Items where Subject is "Institute of Aerodynamics and Flow Technology"

A

Adeli, R. and Longo, J.M.A. and Emunds, H. (2004) Flow field study of a supersonic jet exiting into a supersonic stream. (In Press) Volltext nicht online.

Ahmed, S.R. (2001) Helicopter Main- and Tail Rotor Performance in Presence of Winds. In: CD-Proceedings. 27th European Rotorcraft Forum, Moscow (rus), 11.-14.09.2001. Volltext nicht online.

Ahmed, S.R. (2001) Tutorial on Automobile Aeroacoustics. 8th International Congress on Sound and Vibration, Hongkong (vrc), 02.-06.07.2001. Volltext nicht online.

Ahmed, S.R. (2001) Theoretical And Experimental Approaches to Automobiles Aeroacoustics. SAE 2001 World Congress & Exposition, Detroit (usa), 05.-08.03.2001. Volltext nicht online.

Ahmed, S.R. (2002) Entdeckbarkeit und Lärmcharakteristik von Hubschraubern. In: 13. Arbeitstagung, Anwendungen der Akustik in der Wehrtechnik I. Hochschule der Bundeswehr, Hamburg. 13. Arbeitstagung der wehrtechnischen Dienststelle für Waffen und Munition, Meppen (de), 24.-28.06.2002. Volltext nicht online.

Alder, Marko (2016) Nonlinear Dynamics of Prestressed Panels in Low Supersonic Turbulent Flow. AIAA Journal, 54 (11), pp. 3632-3646. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J054783. ISSN 0001-1452. Volltext nicht frei.

Alrutz, T. (2002) Erzeugung von unstrukturierten Netzen und deren Verfeinerung anhand des Adaptionsmoduls des DLR TAU-Codes. DLR-Interner Bericht. 224-2002 A 10. Diploma. 100 S. Volltext nicht online.

Alrutz, Thomas and Knopp, Tobias (2008) Near-wall grid adaption for turbulent flows. International Journal of Computing Science Mathematics (1), pp. 177-192. Volltext nicht online.

Alrutz, Thomas and Aumann, Petra and Basermann, Achim and Feldhoff, Kim and Gerhold, Thomas and Hunger, Jörg and Jägersküpper, Jens and Kersken, Hans-Peter and Knobloch, Olaf and Kroll, Norbert and Krzikalla, Olaf and Kügeler, Edmund and Müller-Pfefferkorn, Ralph and Puetz, Mathias and Schreiber, Andreas and Simmendinger, Christian and Voigt, Christian and Zscherp, Carsten (2009) HICFD – Hocheffiziente Implementierung von CFD-Codes für HPC-Many-Core-Architekturen. In: PARS-Mitteilungen (ISSN 0177-0454), 26, pp. 27-35. 22. PARS-Workshop, 04.-05. Juni 2009, Parsberg in der Oberpfalz, Deutschland. ISSN ISSN 0177-0454.

Alvarez-Gonzalez, J. (2003) Slat Cove Particle Image Velocity Measurements Data Report. DLR-Interner Bericht. 124-2003/11. 31 S. Volltext nicht online.

Alvarez-Gonzalez, J. (2003) Slat Horn Particle Image Velocity Measurements Data Report. DLR-Interner Bericht. 124-2003/36. 56 S. Volltext nicht online.

Armster, S.Q.; and Delplanque, J.-P.; and Rein, M. and Lavernia, E.J.; (2002) Thermo-fluid mechanisms controlling droplet based materials processes. International Materials Reviews, 47 (6), pp. 265-301. Volltext nicht online.

Arnott, A. and Agocs, J. and Schneider, G. and Sammler, B. and Schroeder, A. (2002) PIV for the EUROLIFT high-lift aerodynamics programme. In: Proceedings, CD-ROM, 7.1-7.2. CEAS Aerospace Aerodynamics Conference, Cambridge, UK, 10 - 12 Juni 2002. Volltext nicht online.

Arnott, A. and Bao, F. and Brunel, E., ONERA, F, and Dieterle, L. and Evrard, J.-P., ONERA,F, and Fatien, C., ONERA, F, and Frahnert, H. and Geiler, C., ONERA, F, and Gilliot, A., ONERA, F, and Klinge, F. and Kompenhans, J. and Lozier, J.-F., ONERA, F, and Mattner, H. and Monnier, J.-C., ONERA, F, and Richard, H. and Sammler, B. and Schneider, G. and Schröder, A. and Simon, P., ONERA, F, and Thibaut, D., ONERA, F, and Vollmers, H. (2003) Test Report of 2D und 3C PIV Measurement on 6 Configurations of LTA and VLTA Models. DLR-Interner Bericht. 224-2003 C 15. Volltext nicht online.

Arnott, A. and Schneider, G. and Neitzke, K.-P. and Agocs, J. and Sammler, B. and Schröder, A. and Kompenhans, J. (2003) Multi-window PIV for high-lift measurements. In: ICIASF 2003 Record, IEEE Catalog Number 03CH37501, pp. 44-53. 20th International Congress on Instrumentation in Aerospace Simulation Facilities, 25-29 Aug 2003, Göttingen, Germany. ISBN 0-7803-8149-1. Volltext nicht online.

Arnott, Alistair and Schneider, Gert and Neitzke, Klaus-Peter and Agocs, Janos and Sammler, Bernd and Schröder, Andreas and Kompenhans, Jürgen (2003) Multi-window PIV for high-lift measurements. In: ICIASF 2003 Record, IEEE Catalog Number 03CH37501, pp. 44-53. 20th International Congress on Instrumentation in Aerospace Simulation Facilities, 2003-08-25 - 2003-08-29, Göttingen. ISBN 0-7803-8149-1. Volltext nicht online.

Augenstein, E. and Leopold, F. and Richard, H. and Raffel, M. (2001) Schlieren Techniques in Comparison: The Background Oriented Method versus Visualization with Holographic Filters. 4th Intern. Symposium on Particle Image Velocimetry, Göttingen, Germany, September 17-18, 2001.. Volltext nicht online.

B

Bachmann, Arne and Kunde, Markus and Litz, Markus and Schreiber, Andreas and Bertsch, Lothar (2009) Automation of Aircraft Pre-design Using a Versatile Data Transfer and Storage Format in a Distributed Computing Environment. IEEE Conference Publications, 1 (1). IEEE. doi: 10.1109/ADVCOMP.2009.22. ISBN 978-1-4244-5082-4.

Bao, F. (2001) Experimental Investigation of Transitional Unsteady Separated Vortex Flows. DLR-Forschungsbericht. 2001-20. Dissertation. 114 S. Volltext nicht online.

Bao, F. (2002) Application of PIV technique in water flows. Nanjing University of Aeronautics and Astronautics, China, 21.10.02. Volltext nicht online.

Bao, F. (2002) Application of PIV technique in water flows. Beijing University of Aeronautics and Astronautics, China , 24.10.02. Volltext nicht online.

Bao, F. and Dallmann, U. (2004) Some physical aspects of separation bibble on a rounded backward-facing step. Aerospace Science and Technology, Vol. 8 (No. 2), pp. 83-91. Volltext nicht online.

Bao, F. and Vollmers, H. (2003) Untersuchungen an Wirbelschleppen im Hinblick auf den Endeffekt in einem Wasserschleppkanal. STAB 2003, DLR, Göttingen , 04.11. - 06.11.2003. Volltext nicht online.

Bao, F. and Vollmers, H. (2004) Wake Vortex Investigation in WSG without / with End-effect. DLR/ONERA - Annex II Meeting, DLR, Köln, 6. -7. April 2004. Volltext nicht online.

Bao, F. and Vollmers, H. (2005) Alleviation of End-effect in Facilities for Far Wake Investigations. In: AIAA Meeting Papers on Disk, pp. 1-11. AIAA Electronic Library. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 10.-13.Jannuary 2005, Reno, Nevada, USA. ISBN CD Code: 666-196461. Volltext nicht online.

Bao, F. and Vollmers, H. (2004) Experimental investigation of wake vortices with respect to wake vortices with respect to „end-effect“ in a water effect“ in a water-towing towing-tank. 14. DGLR- Fach-Symposium der STAB, 16.-18.11.2004, Bremen, Germany. Volltext nicht online.

Bao, F. and Vollmers, H. and Mattner, H. (2003) Experimental Study on Controlling Wake Vortex in Water-Towing-Tank. In: ICIASF 2003 Record, Session 8.3, pp. 214-223. IEEE. ICIASF 2003, Göttingen, Germany, August 25 -29, 2003. ISBN 0-7803-8149-1. Volltext nicht online.

Bao, F. and Vollmers, H. and Schröder, A. (2004) Experimental Study on the Alleviation of Wake Vortices. In: The Proceedings of the Workshop on Applications of Particle Image Velocimetry to Naval and Industrial Hydrodynamics, CD, pp. 1-19. Workshop on Applications of Particle Image Velocimetry to Naval and Industrial Hydrodynamics, Rome, Italy, 05.-06. May 2004. Volltext nicht online.

Barakat, S. and Elsholz, E. (2005) CFD Analysis on Different Wing-tip Devices of Commercial Aircrafts. CEAS/KATnet Conference 2005, 20-22 June, Bremen. Volltext nicht online.

Barakat, S. and Schwamborn, D. (2004) Numerical simulation of the Flow about a Train Model. Aerodynamics of Heavy Vehicles,, Monterey (USA). Volltext nicht online.

Barakat, S. and Schwamborn, D. (2004) Numerical simulation of the Flow about a Train Model. In: The Aerodynamics of Heavy Vehicles: Trucks, Buses, and Trains Springer Verlag. pp. 329-338. ISBN 3-540-22008-7. Volltext nicht online.

Barth, Tarik (2007) Advanced Aerothermodynamic Analysis of SHEFEX I. In: European Air and Space Conference (CEAS). 1st CEAS Berlin, 2007-09-10 - 2007-09-13, Berlin. (Unpublished) Volltext nicht online.

Barth, Tarik (2008) Aerothermodynamic Data Base of SHEFEX-I. DLR-Interner Bericht. DLR-IB 917-2008/919. 7 S. Volltext nicht online.

Barth, Tarik (2008) Aero- and Thermodynamic Analysis of SHEFEX I. Engineering Applications of Computational Fluid Mechanics, 2 (1), pp. 76-84.

Barth, Tarik and Eggers, Thino (2007) SHEFEX - A First Aerodynamic Post-Flight Analysis. In: Springer Verlag.

Beck, Nils and Radespiel, Rolf and Lenfers, Carsten and Friedrichs, Jens and Rezaeian, Alireza (2014) Aerodynamic effects of propeller slipstream on a wing with circulation control by internally blown flap. AIAA SciTech, 52nd Aerospace and Science Meeting, 13.-17. Jan. 2014, USA. Volltext nicht frei.

Behrens, J. and Bozic, O. (2004) Development of Electromagnetic Railgun Technology for the Launch of Payloads into Suborbital and Orbital Altitudes. 55th Congress of International Astronautical Federation, Vancouver (can), 04.-08.10.2004. Volltext nicht online.

Behrens, J. and Lehmann, P. and Longo, J.M.A. and Bozic, O. and Rapp, M. and Conde Reis, A. (2003) Hypersonic and electromagnetic railgun technology as a future alternative for the launch and suborbital payloads. 16th ESA Symposium on Rocket and Balloon Programmes, St. Gallen (ch), 03.-05.06.2003. Volltext nicht online.

Bergmann, Andreas and Hübner, Andreas-René (2007) Integrated Experimental and Numerical Resaerch on the Aerodynamics of Unsteady Aircraft. 3rd International Symosium on Integrating CFD and Experiments in Aerodynamics, 2007-06-20 - 2007-06-21, ASAFA, Colorado. Volltext nicht online.

Bertolotti, F.P. and Hein, S. and Stolte, A. and Koch, W. (2003) Absolute/convective instability investigation of primary and secondary crossflow vortices. In: Recent Results in Laminar-Turbulent Transition - Selected Numerical and Experimental Contributions from the DFG-Verbundsschwerpunkt "Transition" in Germany Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 86. Springer, Heidelberg. ISBN 3-540-40490-2. Volltext nicht online.

Bertsch, Lothar (2007) Stand der Arbeiten zur akustischen Bewertung von Flugzeugkonfigurationen im Projekt QSTOL. DLR-Interner Bericht. Volltext nicht frei.

Bertsch, Lothar and Dobrzynski, Werner and Guerin, Sebastien (2008) Tool development for Low-Noise Aircraft Design. In: 2008 AIAA Meeting Papers, Vol. 13 (Nr. 5 (Aeroacoustics)). 14th AIAA/CEAS Aeroacoustics Conference, 2008-05-05 - 2008-05-07, Vancouver, Canada. ISBN 978-1-56347-939-7. Volltext nicht online.

Bertsch, Lothar and Guerin, Sebastien and Looye, Gertjan and Pott-Polenske, Michael (2011) The Parametric Aircraft Noise Analysis Module - status overview and recent applications. 17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference), 5.-8. June 2011, Portland, Oregon, USA.

Boelen, Okko and Barakos, Georg and Biava, Massimo and Brocklehurst, Alan and Costes, Michel and D’Alascio, Alessandro and Dietz, Markus and Drikakis, Dimitris and Ekaterinaris, John and Humby, Isabel and Khier, Walid and Knutzen, Bjoern and Kok, Johan and LeChuiton, Frederic and Pahlke, KlausDieter and Renaud, Thomas and Schwarz, Thorsten and Steijl, Rene and Sudre, Laurent and van der Ven, H and Vigevano, Luigi and Zhong, Bowen (2007) The blind-test activity of the GOAHEAD project. 33rd European Rotorcraft forum,, 2007-09-13, Kazan, Russia.

Boiko, A.V. (2002) Development of a stationary streak in a local separation bubble. DLR-Interner Bericht. 224-2002 A04. 39 S. Volltext nicht online.

Boiko, A.V. (2002) Development of low-freqency streaks in Blasius boundary layer. DLR-Interner Bericht. 224-2002 A05. 23 S. Volltext nicht online.

Bozic, O. and Longo, J.M.A. and Giese, P. (2003) New European Concept of Single Staged Rocket to launch nano-satellites in Low Earth Orbit (LEO). In: Proceedings of the International Conference on Recent Advances in Space Technologies, pp. 50-55. International Conference on Recent Advances in Space Technologies, Istanbul (tr), 20.-22.11.2003. ISBN 0-7803-8142-4. Volltext nicht online.

Bozic, O. and Longo, J.M.A. and Giese, P. and Behrens, J. (2003) Design of propelled projectiles to provide escape velocity for Nano-Satellites. In: CD ROM. 54th Congress of International Astronautical Federation (IAF), Bremen (de), 29.09.-03.10.2003. Volltext nicht online.

Bozic, O. and Longo, J.M.A. and Giese, P. and Behrens, J. (2004) High-End Concept Based On Hypersonic Two-Stage Rocket and Electromagnetic Railgun To Launch Micro-Satellites Into Low-Earth-Orbit. 5th European Symposium on Aerothermodynamics for Space Vehicles, Köln (de), 08.11.11.2004. Volltext nicht online.

Bozic, O. and Otto, H. (2004) Flow field analysis of a future launcher configuration during start. 5th European Symposium on Aerothermodynamics for Space Vehicles, Köln (de), 08.-11.11.2004. Volltext nicht online.

Bozic, Ognjan and Longo, Jose M. A. and Otto, Hannes (2006) Shock – Wave– Boundary– Layer Interaction (SWBLI) around Open Flaps of Expert Capsule and their Consideration on Heat and Mechanical Loads under Critical Re-entry Flow Conditions. 57th International Astronautical Congress 2006,Space Transportation Symp. (D2.) - Future Space Transportation Systems Technologies (5.), 2006-10-02 - 2006-10-6, Valencia , Spain. Volltext nicht frei.

Bramesfeld, G. and Maughmer, M.D. and Horstmann, K.H. (2004) A Free-Wake, Lifting-Surface Model using Distributed Vorticity Elements. 22nd AIAA Applied Aerodynamics Conference, Providence (usa), 16.-19.08.2004. Volltext nicht online.

Brezillon, J. (2005) Application of the Adjoint Technique with the Optimization Framework Synaps Pointer Pro. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 195-209. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6. Volltext nicht online.

Brezillon, J. and Gauger, N. (2003) 2D and 3D Aerodynamic Shape Optimization using the Adjoint Approach. In: Jahrbuch I & II; Auslegung und Simulation - Geometrie, Strömung, Struktur. DGLR Kongress 2003, München (de), 17.-21.11.2003. ISBN ISSN: 0700-4083. Volltext nicht online.

Brezillon, J. and Gauger, N. (2004) 2D and 3D Aerodynamic Shape Optimization using the Adjoint Approach. Aerospace Science and Technology, 8 (8), pp. 715-727. Volltext nicht online.

Brezillon, Joel and Brodersen, Olaf and Dwight, Richard and Ronzheimer, Arno and Wild, Jochen (2006) Development and Application of a Flexible and Efficient Environment for Aerodynamic Shape Optimisation. In: ODAS Proceedings. ODAS 2006 (ONERA DLR Aerospace Symposium), 2006-10-04 - 2006-10-06, Toulouse. Volltext nicht online.

Brezillon, Joel and Caslav , Ilic and Widhalm, Markus and Mohammad, Abu-Zurayk (2012) Discrete Viscous Adjoint Method for Solving Aerodynamic Shape Optimization Problems. International Workshop on Simulation, Experiments and Optimisation for the Design of a Future Aviation , 22. Februar 2012, Paris, Frankreich. Volltext nicht online.

Brezillon, Joel and Dwight, Richard P. (2011) Applications of a discrete viscous adjoint method for aerodynamic shape optimisation of 3D configurations. CEAS Aeronautical Journal. Springer. doi: 10.1007/s13272-011-0038-0. Volltext nicht online.

Brezillon, Joel and Ilic, Caslav and Abu-Zurayk, Mohammad and Widhalm, Markus (2012) State of the art at DLR in solving aerodynamic shape optimization problems using the discrete viscous adjoint method. Conference on adjoint fluid optimization and FlowHead, Munich.

Brezillon, Joel and Ronzheimer, Arno and Haar, Danil and Abu-Zurayk, Mohammad and Lummer, Markus and Krüger, Wolf-Reiner and Natterer, Franz Josef (2012) Development and application of multi-disciplinary optimization capabilities based on high-fidelity methods. 8th AIAA Multidisciplinary Design Optimization Specialist Conference, 23-26 Apr. 2012, Honolulu, Hawaii. Volltext nicht online.

Brezillon, Joël and Dwight, Richard P. and Widhalm, Markus (2009) Aerodynamic Optimization for Cruise and High-Lift Configurations. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 107. Springer. pp. 249-262. ISBN 978-3-642-04092-4. ISSN 1612-2909. Volltext nicht online.

Brezillon, Joël and Dwight, Richard P. and Wild, Jochen (2009) Numerical Aerodynamic Optimisation of 3D High-Lift Configurations. CEAS 2009 European Air and Space Conference, 26-29 October 2009, Manchester, UK. Volltext nicht online.

Brezillon, Joël and Dwight, Richard P. (2009) Aerodynamic Shape Optimization Using the Discrete Adjoint of the Navier-Stokes Equations: Applications Toward Complex 3D Configutations. KATnet II Conference on Key Aerodynamic Technologies, 12-14 May 2009, Bremen.

Brodersen, O. (2002) Drag Prediction of Engine-Airframe Interference Effects Using Unstructured Navier-Stokes Calculations. AIAA Journal of Aircraft, 39 (6), pp. 927-935. Volltext nicht online.

Brodersen, O. (2003) Numerische Analyse der aerodynamischen Triebwerksinstallationseffekte an Transportflugzeugen. Dissertation, TU Braunschweig. Volltext nicht online.

Brodersen, O. (2005) Computation of Engine-Airframe Installation Drag. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 151-161. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6. Volltext nicht online.

Brodersen, O. and Hain, R. and Geyr, H. von (2004) Hybrid Navier-Stokes Calculations for Transport Aircrafts with Conventional and High-Bypass Engines. New Results in Numerical and Experimental Fluid Mechanics IV, 87, pp. 91-98. Springer Verlag, Berlin, Heidelberg, New York. ISBN 3-540-20258-7. Volltext nicht online.

Brodersen, O. and Hain, R. and von Geyr, H. (2002) Hybrid Navier-Stokes Calculations for Transport Aircrafts with Conventional and High-Bypass Engines. 13. DGLR-Fachsymposium der AG STAB 2002, München (de), 12.-14.11.2002. Volltext nicht online.

Brodersen, O. and Rakowitz, M. and Amant, S. and Larrieu, P. and Destarac, D. and Sutcliffe, M. (2004) Airbus, ONERA, and DLR Results from the Second AIAA Drag Prediction Workshop. 42nd AIAA Aerospace Sciences Meeting, Reno (usa), 05.-08.01.2004. Volltext nicht online.

Brodersen, O. and Rakowitz, M. and Sutcliffe, M. (2003) 2nd AIAA Drag Prediction Workshop: TAU Results. AIAA-Drag Prediction Workshop, Orlando (usa), 20.-26.06.2003. Volltext nicht online.

Brodersen, O. and Taupin, K. and Maury, E. and Spieweg, R. and Lieser, J. and Laban, M. and Godard, J.-L. and Vitagliano, P.L. and Bigot, P. (2005) Aerodynamic Investigations in the European Project ROSAS. 23rd AIAA Applied Aerodynamics Conference, Toronto (can), 06.-09.06.2005. Volltext nicht online.

Brodersen, Olaf (2005) Computation of Engine-Airframe Installation Drag. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 89. Springer. ISBN 3-540-24383-6. ISSN 1612-2909. Volltext nicht online.

Brodersen, Olaf and Eisfeld, Bernhard (2006) DPW-3 DLR F6/F6-FX2B Results. In: AIAA Drag Prediction Workshop Web-Site. AIAA. 3rd AIAA Drag Prediction Workshop, 2006-06-03 - 2006-06-04, San Francisco, CA (USA). Volltext nicht online.

Brodersen, Olaf and Eisfeld, Bernhard and Raddatz, Jochen and Frohnapfel, Petra (2006) DLR Results from the Third AIAA CFD Drag Prediction Workshop (Invited). In: 45th AIAA Aerospace Science Meeting and Exhibit. 45th AIAA Aerospace Science Meeting and Exhibit, 2007-01-08 - 2007-01-11, Reno, NV (USA). (Submitted) Volltext nicht online.

Brodersen, Olaf and Eisfeld, Bernhard and Raddatz, Jochen and Frohnapfel, Petra (2008) DLR Results from the Third AIAA Computational Fluid Dynamics Drag Prediction Workshop. Journal of Aircraft, 45 (3), pp. 823-836. doi: 10.2514/1.30628. ISSN 0021-8669. Volltext nicht online.

Buchholz, H. and Gehlhar, B. and Pott-Pollenske, M. and Spiegel, K.-H. (2003) Noise Assessment for a Laser Reflector Installation (JCAB Global Express). DLR-Interner Bericht. 124-2003/10. 104 S. Volltext nicht online.

Burg, J.W. van der and Cock, K.M.J. de and Berglind, T. and Fritz, W. and Kretzschmar, G. and Kroll, N. and Schwamborn, D. and Sillen, M. (2002) A Joint European Initiative to Develop Hybrid Grid Based CFD-Technology for Inviscid and Viscous Flow Computations Applicable to Geometrically Complex Aircraft Configurations. CEAS Aerospace Aerodynamics Research Conference, 2002-06-10 - 2002-06-12, Cambridge (GB). Volltext nicht online.

Burg van der, Jan Willem and Geyr von, Heiko (2007) Geometrical Model Installation and Deformation Effects in the European Project EUROLIFT II. 25th AIAA Applied Aerodynamics Conference, 2007-06-25 - 2007-06-28, Miami, FL, USA. Volltext nicht online.

Burley, C.L. and Brooks, T.F. and van der Wall, Berend G. and Richard, H. and Raffel, M. and Beaumier, P. and Delrieux, Y. and Lim, J.W. and Yu, Y.H. and Tung, C. and Pengel, K. and Mercker, E. (2002) Rotor Wake Vortex Definition - Initial Evaluation of 3-C PIV Results of the HART-II Study. 28th European Rotorcraft Forum, Bristol (uk), 17-20 September 2002. Volltext nicht online.

Büscher, A. and Radespiel, R. and Streit, T. (2004) Two-Point-Design Of A Non Planar Lifting Configuration Using a Databased Prediction Tool. In: Jahrbuch DGLR 2004, 1, pp. 319-327. DGLR Jahrestagung 2004, Dresden (de), 20.-23.09.2004. ISBN 0070-4083. Volltext nicht online.

Bütefisch, K.-A. (1995) Geschwindigkeitsfeldmessungen mit dem 3D Laser Doppler Anemometer zur Validierung numerischer Verfahren. DGLR - Jahrestagung 1994, Erlangen. Volltext nicht online.

Bütefisch, K.-A. and Kompenhans, J. (2002) Current Status and Prospects for Experimental Aerodynamics. CEAS Aerospace Aerodynamics Research Conference, 10-12 June 2002, Cambridge, United Kingdom. Volltext nicht online.

Bütefisch, K.-A. and Möller, T. and Bippes, H. (1999) Untersuchungen zum Stofflauf. DLR-Interner Bericht. 223-99 C 21. 22 S. Volltext nicht online.

C

Carlier, J. Uni Lille, France, and Kähler, C. and Stanislas, M. (2001) Experimental study of eddy strutures in a turbulent boundary layer using PIV. In: CD ROM Proceedings, Proceedings, 1094-1-1094-7. 4th International Symposium on Particle Image Velocimetry, Göttingen, Germany, September 17-19, 2001. Volltext nicht online.

Chappuis, Johanna and Lummer, Markus (2006) Monopole Diffraction by Generic Plane Geometries. ICAS 2006, 2006-09-03 - 2006-09-08, Hamburg, Germany. Volltext nicht online.

Chow, L.C. and Dobrzynski, W. (2002) Landing Gear Airframe Noise Research Study. 9th International Congress on Sound and Vibration, Orlando (usa), 8.-11.07.2002. Volltext nicht online.

Christou, K. (2004) Schallabstrahlung von turbulenten Freistrahlen I - Standardproblem der Strömungsakustik. Schwingungsphysikalisches Kolloquium, III. Physikalisches Institut, Universität Göttingen, 08.01.2004. Volltext nicht online.

Christou, K. (2004) Messung der Geschwindigkeitsfluktuationen eines turbulenten Unterschall-Freistrahls mit Hilfe der Mehrebenen-Stereo Particle Image Velocimetry als Grundlage für Schallabstrahlungsberechnungen. Diploma, III. Physikalischen Institut der Georg-August-Universität Göttingen. Volltext nicht online.

Ciezki, H. and Rosemann, H. (2001) Tagungsband. 2. DLR-Flugkörper-Workshop. DLR-Interner Bericht. 645-2001/18. 136 S. Volltext nicht online.

Ciobaca, Vlad (2008) Simulation of active flow control on the flap of a 2D high-lift configuration. New Results in Numerical and Experimental Fluid Mechanics VII, 112 (pp. 20). Springer Verlag. ISBN 978-3-642-14242-0. ISSN 1612-2909. Volltext nicht frei.

Ciobaca, Vlad (2013) Parameter study for a slatless 2D high-lift airfoil with active separation control using a URANS approach. In: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 121. Springer-Verlag. pp. 135-142. ISBN 978-3-642-35679-7. ISSN 1612-2909.

Ciobaca, Vlad and Melber-Wilkending, Stefan and Pott-Pollenske, Michael (2009) A CFD process chain for simulating open windtunnel test sections. www.machtwissen.de AG. ISBN 978-3-00-027782-5.

Costes, M. and Kowani, G. (2002) An automatic anti-diffusion method for vortical flows based on Vorticity Confinement. American Helicopter Society Technical Specialists Meeting, San Francisco (usa), 23.-25.01.2002. Volltext nicht online.

Costes, M. and Pahlke, K. and D'Alascio, A. and Castellin, C. and Altmikus, A. (2005) Overview of Results Obtained During the 6-Year French-German CHANCE Project. American Helicopter Society 61st Annual Forum, Grapevine (usa), 01.-03.06.2005. Volltext nicht online.

Coustols, E., ONERA, Toulouse, France, and Stumpf, E. and Jacquin, L., ONERA, Meudon, France, and Moens, F., ONERA Châtillon, France, and Vollmers, H. and Gerz, T. (2003) Minimised Wake: A Collaborative Research Programme on Aircraft Wake Vortice. In: AIAA, pp. 1-15. 41th Aerospace Sciences Meeting & Exhibit, Reno, Nevada, USA, 6.-9. January 2003. Volltext nicht online.

Crippa, Simone and Brodersen, Olaf (2012) DLR Results DPW-V. AIAA CFD Drag Prediction Workshop 5, 23 June - 24 June 2012, New Orleans, LA, USA.

Crippa, Simone and Melber-Wilkending, Stefan and Rudnik, Ralf (2011) DLR Contribution to the First High Lift Prediction Workshop. 49th AIAA Aerospace Sciences Meeting, 4-7 Jan 2011, Orlando, FL, USA.

Cummings, Russel M. and Schütte, Andreas (2009) NUMERICAL SOLUTIONS FOR THE VFE-2 CONFIGURATION ON UNSTRUCTURED GRIDS AT USAFA, UNITED STATES. NATO RTO - Research and Technology Organisation. [Other] Volltext nicht online.

Cummings, Russel M. and Schütte, Andreas (2009) INTRODUCTION TO THE AVT-161 AIR FACET: AN INTEGRATED COMPUTATIONAL/EXPERIMENTAL APPROACH TO UCAV STABILITY AND CONTROL ESTIMATION. NATO RTO - Research and Technology Organisation. [Other] Volltext nicht online.

D

D'Alascio, A. and Berthe, A. and Le Chuiton, F. (2003) Application of CFD to the Fuselage Aerodynamics of the EC-145 Helicopter. Prediction of Unsteady Phenomena and of the Time Averaged Influence of the Main Rotor. 29th European Rotorcraft Forum, 2003-09-16 - 2003-09-18, Friedrichshafen, Germany. Volltext nicht online.

D'Alascio, A. and Castellin, C. and Schöning, B. (2005) Industrial validation of CFD solvers on medium and large helicopter fuselages. European Rotorcraft Forum, Florenz (it), 13.-16.09.2005. Volltext nicht online.

D'Alascio, A. and Pahlke, K. and Castellin, C. and Costes, M. (2001) Aerodynamics of Helicopter. Application of the Navier-Stokes Codes Developped in the Framework of the Joined German/French CFD Research Project CHANCE. 27th European Rotorcraft Forum, Moskau (rus), 10.-15.09.2001. Volltext nicht online.

D'Alascio, A.; Eurocopter Deutschland GmbH and Castellin, C.; Eurocopter and Costes, M.; ONERA and Pahlke, K. (2002) Aerodynamics of Helicopter. Application of the Navier-Stokes Codes developed in the framework of the joined German/French CFD Research Programm Chance. CEAS Aerospace Aerodynamics Research Conference, Cambridge (uk), 10.-12.06.2002. Volltext nicht online.

D'Alascio, A., Eurocopter Deutschland, and Pahlke, K. and Le Chuiton, F. (2004) Application of a structured and an unstructured CFD Method to the Fuselage Aerodynamics of the EC145 Helicopter. Prediction of the time averaged Influence of the Main Rotor. In: CD. ECCOMAS 2004, Jyväskylä (fi), 24.-28.07.2004. Volltext nicht online.

Dankert, C. (2003) Ergebnisse aus der Versuchsanlage V1G zu Werkstoffbelastungen bei bodennahem Hochgeschwindigkeitsflug. DLR-Interner Bericht. 223-2003 C 18. 50 S. Volltext nicht online.

Dankert, C. (2001) Konstruktion, Modifikation und Test einer Anlage zur Simulation der werkstoffbelastungen beim bodennahen Hochgeschwindigkeitsflug. DLR-Interner Bericht. 223-2001 C 15. 20 S. Volltext nicht online.

Dankert, C. (2004) Feasibility Study of Laser Air Data System. DLR-Interner Bericht. 224-2004 C 11. 30 S. Volltext nicht online.

Dankert, C. and Dettleff, G. and Kesting, A. (2003) Plume Characterisation Testing of European Thrusters. Test Report WP3: Investigation of Plume Interaction. DLR-Interner Bericht. 224- 2003 A 09. 62 S. Volltext nicht online.

Dankert, C. and Dettleff, G. and Nazari, B.K. and Rosenhauer, M. (2001) Spectroscopy Measurements in Rarefied Plumes. In: ICIASF 2001 Record, Cleveland Ohio 2001 ICIASF records, I. ISBN 0-7803-7022-8. Volltext nicht online.

Dankert, C. and Mori, H. (2003) Flow Velocity Measurements in Nirogen Plumes Stimulated by REMPI. In: ICIASF 2003, Göttingen, Germany 2003 ICIASF records, I. IEEE. ISBN 0-7803-8149-1. Volltext nicht online.

Dankert, C. and Nazari, B.K. (2001) Spectroscopy Measurements in Rarefied Plumes in the Cryopumped Chamber STG. In: Rarefied Gas Dynamics, 22nd International Symposium, Sydney, Australia,2000 American Institute of Physics, I. AIAA. ISBN unbekannt. Volltext nicht online.

Dargel, G. and Hansen, H. and Wild, J. and Streit, T. and Rosemann, H. and Richter, K. (2002) Aerodynamische Flügelauslegung mit multifunktionalen Steuerflächen. Deutscher Luft- und Raumfahrtkongress 2002, Suttgart, 23. - 26. September 2002. Volltext nicht online.

Das, A. (2001) On the Physics and Kinematics of Vortex Motion in the Downstream of a Long-Span Wing with High-Lift Devices. DLR-Interner Bericht. 129-2001/21. 48 S. Volltext nicht online.

Das, A. and Wichmann, G. (2004) On the physics and kinematics of vortex motion in the downstream of a high aspect ratio wing with high-lift devices. Aerospace Science and Technology, 8 (6), pp. 489-498. Volltext nicht online.

Das, Arabindo and Wichmann, Georg (2008) Some extended analyses concerning the physics and kinematics of wave propagation in moving systems. Zeitschrift für angewandte Mathematik und Physik (ZAMP), 59 (1), pp. 156-180. Birkhäuser Verlag AG, Basel. doi: 10.1007/s00033-007-6107-x. Volltext nicht frei.

Deck, S. and Neitzke, Klaus-Peter and Schröder, Andreas (2005) A combined experimental-numerical investigation of the flow around a high lift wing with deployed slat and flap. PivNet2/EWA Workshop, 2005-05-10 - 2005-05-11, Göttingen (Germany). Volltext nicht online.

Delfs, J. and Heller, H. (1997) Aeroacoustic Research in Europe - 1996 Highlights: A Summary of Last Year's Activities in the Six CEAS Coutries. In: Journal of Sound and Vibration, 204 (4), pp. 609-622. Academic Press Limited. Volltext nicht online.

Delfs, Jan and Dobrzynski, Werner and Heller, H and Isermann, Ullrich and Michel, U. and Obermeier, F. and Splettstösser, W. (2004) Fluglärm. In: Taschenbuch der Technischen Akustik, 3. Auflage Springer Verlag. pp. 585-638. ISBN 3-540-41242-5. Volltext nicht online.

Delfs, Jan / W. and Faßmann, Benjamin and Lippitz, Nicolas and Mößner, Michael and Müller, Lars and Rurkowska, Katharina and Uphoff, Sonja (2014) SFB 880: aeroacoustic research for low noise take-off and landing. CEAS Aeronautical Journal, 5 (4), pp. 403-417. Springer. doi: 10.1007/s13272-014-0115-2. ISSN 1869-5582.

Dennis, B.H. and Egorov, I. N. and Sobieczky, H. and Dulikravich, G.S. and Yoshimura, S. (2003) Parallel Thermoelasticity Optimization of 3-D Serpentine Cooling Passages in. ASME Turbo Expo 2003, Atlanta, GA, June 16-19, 2003. Volltext nicht online.

Dettleff, G. (2004) Plume Characterisation Testing of European Thrusters, Test Report. DLR-Interner Bericht. 224-2004 A 01. 108 S. Volltext nicht online.

Dettleff, G. (2004) Plume Characterisation Testing of European Thrusters, Executive Summary. DLR-Interner Bericht. 224-2004 A 03. 103 S. Volltext nicht online.

Dhondt, Guido and Nagel, Marc and Gauger, Nicolas (2005) Calculation of the eigenfrequeny sensitivity of aircraft engine structures. In: Proceedings of EUROGEN 2005. EUROGEN 2005, Munich. Volltext nicht online.

Dierke, Jürgen and Appel, Christina and Jona, Siebert and Bauer, Marcus and Siefert, Malte and Ewert, Roland (2011) 3D Computation of Broadband Slat Noise from Swept and Unswept High-Lift Wing Sections. 17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference), 05 - 08 June 2011, Portland, Oregon.

Dillmann, A. (2003) On the analytical solution for the cylindrical supersonic free jet. Institutsseminar, Erlangen-Nürnberg, 14.11.2003. Volltext nicht online.

Dillmann, Andreas (2005) Johanna Vogel-Prandtl: Ludwig Prandtl, Ein Lebensbild, Erinnerungen, Dokumente. Göttinger Klassiker der Strömungsmechanik, Band 1. Universitätsverlag Göttingen. 223 S. ISBN 3-938616-34-2. Volltext nicht online.

Dillmann, Andreas (2005) Karl Wieghardt: Theoretische Strömungslehre. Göttinger Klassiker der Strömungsmechanik, Band 2. Universitätsverlag Göttingen. 237 S. ISBN 3-938616-33-4. Volltext nicht online.

Dillmann, Andreas (2011) Flugschau für die Wissenschaft. [Other] Volltext nicht online.

Dillmann, Andreas and Richard, Hugues and Kowalski, Thomas and Loose, Sigfried (2007) The Use of Aeronautical Experimental Facilities and Measurement Techniques for the Aerodynamic Investigation of High Speed Trains. 2007, Conference: The Aerodynamics of Heavy Vehicles II: Trucks, Buses and Trains., 2007, August 26-31., Lake Tahoe, Reno/California (USA). (Unpublished) Volltext nicht online.

Dobrzynski, W. (2001) Stand der Fluglärmforschung - Nationale und Internationale Forschungsvorhaben. In: CD-Proceedings. DGLR-Workshop der Fachgruppe SG2: Infrastruktur des Luftverkehrs "Reduzierung des Fluglärms- Wo liegen die Ziele und Grenzen der Machbarkeit?, Frankfurt/Main (de), 30.11.2001. Volltext nicht online.

Dobrzynski, W. (2001) Results of consultations towards a low airframe noise design of the Dornier 728 Aircraft. DLR-Interner Bericht. 129-01/2. 23 S. Volltext nicht online.

Dobrzynski, W. (2002) Lärmminderung an der Quelle - Techn. Entwicklungen. In: Umweltprobleme des Luftverkehrs. Nomos Verlagsgesellschaft, Baden-Baden. Seminar Umweltrecht, Hamburg (de), 10.06.2002. ISBN 3-8329-0058-6. Volltext nicht online.

Dobrzynski, W. (2002) "Fluglärmforschung im Windkanal - Beispiele aus der Praxis". Aeroakustik-Tagung Nr. E-H030-12-119-2, Ingolstadt (de), 11.-12.12.2002. Volltext nicht online.

Dobrzynski, W. (2003) Assessment of slat and flap side-edge noise reduction potential from far field noise measurements. DLR-Interner Bericht. 124-2003/40. 163 S. Volltext nicht online.

Dobrzynski, W. (2003) Vereinfachtes Prognosemodell für den Hochauftriebslärm. DLR-Interner Bericht. 124-2003/25. 24 S. Volltext nicht online.

Dobrzynski, W. (2003) Umströmungslärm bei Fahrzeugen. Workshop Verkehrslärm im Forschungsverbund "Leiser Verkehr", Bonn (de), 10.04.2003. Volltext nicht online.

Dobrzynski, W. (2004) A380 farfield noise data analysis from measurements in the open Test section of DNW-LLF. Project Report, DLR-Interner Bericht. 124-04/4. 19 S. Volltext nicht online.

Dobrzynski, W. (2004) Quantified noise characteristics of the aircraft with control devices. Project Report, DLR-Interner Bericht. 124-04/11. 28 S. Volltext nicht online.

Dobrzynski, W. and Chow, L.C. and Guion, P. and Shiells, D. (2002) Research into Landing Gear Airframe Noise Reduction. 8th AIAA/CEAS Aeroacoustics Conference, Breckenridge (usa), 17.-19.06.2002. Volltext nicht online.

Dobrzynski, W. and Gehlhar, B. and Buchholz, H. (2001) Model and full scale high lift wing wind tunnel experiments dedicated to airframe noise reduction. Aerospace Science & Technology, 5 (1), pp. 27-33. Volltext nicht online.

Dobrzynski, W. and Gehlhar, B. and Buchholz, H. (2001) RAIN Task 3.2: High Lift Devices Noise Reduction Study - A320 Full-scale Wing in DNW-LLF. DLR-Interner Bericht. 129-01/18. 529 S. Volltext nicht online.

Dobrzynski, W. and Holthusen, H. (2004) Advanced landing gear noise reduction - Test data analysis and assessment of results. DLR-Interner Bericht. 124-04/902. 115 S. Volltext nicht online.

Dobrzynski, W. and Pott-Pollenske, M. and Foot, D. and Goodwin, M. (2004) Landing gears aerodynamic interaction noise. ECCOMAS, Jyväskylä (fi), 24.-28.07.2004. Volltext nicht online.

Dobrzynski, W. and Pott-Pollenske, M. and Gehlhar, B. and Stechow, L. and Herr, M. and Alvarez-Gonzalez, J. (2004) Airframe noise experiments in DLR's project "Quiet Air Traffic". 4th Aeroacoustics Workshop, Aachen (de), 26.-27.02.2004. Volltext nicht online.

Dobrzynski, W. and Stöcker, U. (2001) Regulation for Noise Abatement Around Small Airfields in Germany - A Challenge for the General Aviation Aircraft Industry? International Congress and Exhibition on Noise Control Engineering (inter noise) 2001, The Hague (nl), 27.-30. August 2001. Volltext nicht online.

Dobrzynski, Werner and Ewert, Roland and Pott-Pollenske, Michael and Herr, Michaela and Delfs, Jan (2007) Research at DLR towards airframe noise prediction and reduction. Aerospace Science and Technology, pp. 80-90. doi: 10.1016/j.ast.2007.10.014. Volltext nicht online.

Dobrzynski, Werner and Pott-Pollenske, Michael (2001) Slat Noise Source Studies for Farfield Noise Prediction. In: CD-Proceedings. 7th AIAA/CEAS Aeroacoustics Conference, Maastricht (nl), 28.-30.05.2001, Maastricht (NL). Volltext nicht online.

Dujardin, A. and Gülhan, A. and Longo, J.M.A. and Mack, A. (2001) Numerical/Experimental Investigation of a Wedge-Compression Corner with Gap-Flow under Cold-Hypersonic Gas Conditions. 4th Symposium on Aerothermodynamics for Space Vehicles, Capua (it), 14.-18.10.2001. Volltext nicht online.

Dumont, Etienne and Bussler, Leonid and Karl, Sebastian and Porrmann, Dennis and Manfletti, C. and Krause, Daniel and Klevanski, J. and Clark, Vanessa and Bozic, Ognjan and Poppe, Georg (2016) Analysis of the Ariane 62/64 and Vega-C launcher family. DLR-Interner Bericht. DLR-IB-RY-HB-2016-63. DLR. 199 S. (Unpublished) Volltext nicht online.

Dwight, Richard and Han, Zhong-Hua (2009) Efficient Uncertainty Quantification using Gradient-Enhanced Kriging. 11th AIAA Non-Deterministic Approaches Conference, 4-7 May 2009, Palm Springs, Kalifornien, USA.

Döring, F. (2004) Synthese von Pyrenfarbstoffen und Untersuchung ihrer O2-druckabhängigen Lumineszenz für die Anwendung als Pressure Sensitive Paint. DLR-Forschungsbericht. 18. Dissertation. 239 S. Volltext nicht online.

E

Egami, Yasuhiro and Fey, Uwe and Engler, Rolf (2005) Application of TSP/PSP in a High Speed Cryogenic Wind Tunnel. CEAS/KATnet Conference on Key Aerodynamic Technologies, 2005-06-06 - 2005-06-08, Bremen. Volltext nicht online.

Eggers, T. (2002) Design Specification of the 1:22 EPISTLE SCT Wind Tunnel Model. DLR-Interner Bericht. 129-2002/3. 25 S. Volltext nicht online.

Eggers, T. (2002) Aerodynamic Design of an Ariane 5 Liquid Fly-Back Booster. Volltext nicht online.

Eggers, T. (2002) Input Data Description of the HOTSOSE Code. DLR-Interner Bericht. IB 124-2002/22. Volltext nicht online.

Eggers, T. (2003) Longitudinal Stability and Trim of an Ariane 5 Fly-Back Booster. In: AIAA Online Proceedings. AIAA 12st Space Planes and Hypersonic Systems and Technologies Conference, Norfolk (usa), 15.-19.12.2003. Volltext nicht online.

Eggers, T. (2003) Aerodynamic behaviour of a liquid fly-back booster in transonic cruise flight. In: AIAA Conference Proceedings (CD). AIAA 21st Applied Aerodynamics Conference, Orlando (usa), 23.-26.06.2003. Volltext nicht online.

Eggers, T. (2004) Studies for the Design of an Ariane 5 Liquid Fly-Back Booster. DLR-Interner Bericht. 124-2004/29. 55 S. Volltext nicht online.

Eggers, T. (2004) Aerodynamic Design of an Ariane 5 Reusable Booster Stage. 5th European Symposium on Aerothermodynamics for Space Vehicles, Köln (de), 08.-11.11.2004. Volltext nicht online.

Eggers, T. (2004) Aerodynamic and Aerothermodynamic Layout of the Hypersonic Flight Experiment SHEFEX. 5th European Symposium on Aerothermodynamics for Space Vehicles, Köln (de), 08.-11.11.2004. Volltext nicht online.

Eggers, T. and Bozic, O. (2002) Aerodynamic Design and Analysis of an ARIANE 5 Liquid Fly-Back Booster. 11th AIAA/AAAF Space Planes and Hypersonic Systems Conference, Orleans (fr), 29.9.-04.10.2002. Volltext nicht online.

Eggers, T. and Gülhan, A. and Hannemann, K. and Longo, J.M.A. (2003) Aerothermodynamic Design of Space Vehicles: Experiment and CFD. International Conference on Recent Advances in Space Technologies, RAST 2003, IEEE, Istanbul (tr), 19.-23.11.2003. Volltext nicht online.

Eggers, T. and Novelli, P. and Haupt, M. (2001) Design Studies of the JAPHAR Experimental Vehicle for Dual Mode Ramjet Demonstration. 10th International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto (ja), 24.-27.04.2001. Volltext nicht online.

Ehrenfried, Klaus (2006) Schallausbreitung in gescherten Strömungen: Vergleich zwischen der vereinfachten Möhring-Gleichung und den linearisierten Euler-Gleichungen. DLR-Forschungsbericht. DLR-FB--2006-08. 37 S. Volltext nicht online.

Ehrenfried, Klaus and Koop, Lars (2006) A comparison of iterative deconvolution algorithms for the mapping of acoustic sources. AIAA Journal, 45 (7), pp. 1584-1595. doi: 10.2514/1.26320. Volltext nicht online.

Ehrenfried, Klaus (2006) Noise sources from moving surfaces - Theoretical background. In: VKI Lecture Series. Experimental Aeroacoustics, 2006-11-13 - 2006-11-17, Brüssel.

Einarsson, G. and Neumann, J. (2005) Multidisciplinary Simulation of a Generic Delta Wing: Aerodynamic, Flight-Dynamic and Structure-Mechanic Coupling. In: Computational Methods for Coupled Problems in Science and Engineering, 1st. Edition, pp. 163-182. CIMNE, Barcelona (Spain). Coupled Problems 2005, Santorini Island (gr), 25.-27.05.2005. ISBN 84-95999-71-4. Volltext nicht online.

Eisfeld, B. (2003) Die Eigenwerte des Systems aus RANS- und Reynolds-Spannungsgleichungen. DLR-Interner Bericht. IB 124-2003/1. 154 S. Volltext nicht online.

Eisfeld, B. (2003) Implementation and validation of the Hellsten k-w EARSM. DLR-Interner Bericht. IB 124-2003/33. 34 S. Volltext nicht online.

Eisfeld, B. (2004) Implementation of Reynolds stress models into the DLR-FLOWer code. DLR-Interner Bericht. 124-2004/31. 67 S. Volltext nicht online.

Eisfeld, B. (2005) Turbulence Models in FLOWer. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 63-77. Springer Verlag. Closing Presentation DLR project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6. Volltext nicht online.

Eisfeld, B. and Brodersen, O. (2005) Advanced Turbulence Modelling and Stress Analysis for the DLR-F6 Configuration. 23rd AIAA Applied Aerodynamics Conference, Toronto (can), 06.-09.06.2005. Volltext nicht online.

Eisfeld, B. and Schnitzlein, K. (2001) The influence of confining walls on the pressure drop in packed beds. Chemical Engineering Science, 56, pp. 4321-4329. Volltext nicht online.

Eisfeld, B. and Schnitzlein, K. (2005) A new pseudo-continuous model for the fluid flow in packed beds. Chemical Engineering Science, 60, pp. 4105-4117. Volltext nicht online.

Eisfeld, Bernhard (2006) Computation of Complex Compressible Aerodynamic Flows with a Reynolds Stress Turbulence Model. In: Proceedings of the International Conference on Boundary and Interior Layers (BAIL), Göttingen, 2006. International Conference on Boundary and Interior Layers (BAIL) 2006, 2006-07-24 - 2006-07-28, Göttingen. Volltext nicht online.

Eisfeld, Bernhard (2007) Numerical Simulation of Aerodynamic Problems with the SSG/LRR-ω Reynolds Stress Turbulence Model Using the Unstructured TAU Code. In: New Results in Numerical and Experimental Fluid Mechanics VI, 96, pp. 356-363. Springer-Verlag. 15. DGLR/STAB-Symposium, 2006-11-29 - 2006-12-01, Darmstadt. ISBN 3-540-74458-4. Volltext nicht online.

Eisfeld, Bernhard (2008) Non-dimensionalisation of the governing equations and parameter specification for numerical simulations with the DLR TAU code. DLR-Interner Bericht. DLR-IB 124-2008/2. 45 S. Volltext nicht online.

Emunds, H. and Frieß, M. and Göring, J. and Kemptner, E. and Otto, H. and Dankert, C. (2004) Untersuchungen an den vom DLR neu entwickelten Materialien für Suchkopfabdeckungen. Wirkung und Schutz, Explosivstoffe, Mannheim, 8-10.11.2004. Volltext nicht online.

Emunds, H. and Otto, H. and Göring, J. and Frieß, M. (2003) Untersuchungen von aerothermodynamischen Lasten bei Suchkopfabdeckungen. 3. DLR - Flugkörper-Workshop, Köln, 6 November 2003. Volltext nicht online.

Engler, R. (2004) Application of PSP up to Mach 4. DLR/ONERA - Annex II Meeting, DLR, Köln, 6. - 7. April 2004. Volltext nicht online.

Engler, R. (2004) Pressure Sensitive Paints in Quantitative Wind Tunnel Studies. In: ISFV11 2004 Flow Visualization, pp. 1-11. 11th International Symposium on Flow Visualization, University of Notre Dame, Notre Dame, Indiana, USA. ISBN 0-9533991-5. Volltext nicht online.

Engler, R. (2003) Pressure Sensitive Paints (PSP) - ein flächenhaftes, optisches Meßverfahren zur Ermittlung von Druckverteilungen auf Modelloberflächen in Windkanälen. Seminarvortrag im Wintersemester 2003/2004, Forschungszentrum Karlsruhe, IRS, Karlsruhe, 20.11.2003. Volltext nicht online.

Engler, R. (2003) Entwicklungsstand der DLR PSP-Technik. 11. Fortschritts-Präsentation, Koblenz, 28.01.2003. Volltext nicht online.

Engler, R. (2004) Messungen flächiger Druckverteilungen auf Windkanalmodellen mittels Pressure Sensitive Paint (PSP). 8. Tagung Fahrzeug-Aerodynamik, Haus der Technik, Essen, 27.-28.10.2004. Volltext nicht online.

Engler, R. (2005) Pressure sensitive Paints in quantitative Wind Tunnel Studies. CEAS/KATnet Conference on Key Aerodynamic Technologies, Bremen, Germany, 06. - 08. June 2005, Bremen. Volltext nicht online.

Enk, S. (2003) Implementierung und Validierung eines DES-Modells in den numerischen Strömungslöser FLOWer. DLR-Interner Bericht. IB 124-2003/21. Volltext nicht online.

Enk, S. (2004) DES Rechnung mit Strömungslöser FLOWer am Aerospatiale A-Profil. DLR-Interner Bericht. 124-2004/7. 25 S. Volltext nicht online.

Erdi-Betchi, A. and Klinkov, K. V. and Rein, M. (2002) Kaltgasspritzen: Untersuchungen zur Geschwindigkeitsverteilung der Partikel im Spray. In: Spray 2002: 7. Workshop über Techniken der Fluidzerstäubung und Untersuchung von Sprühvorgängen, A 870, pp. 193-202. Spray 2002 -- 7. Workshop über Techniken der Fluidzerstäubung und Untersuchungen von Sprühvorgängen, Freiberg, 21.-22. Nov. 2002. ISBN 3-86012-185-5. Volltext nicht online.

Erdi-Betchi, A. and Klinkov, K.V. and Rein, M. (2003) Düsenexpansion und Wechselwirkung des Überschallfreistrahls mit einer Wand. STAB-Workshop, DLR, Göttingen, 04.-06.11.2003. Volltext nicht online.

Erdi-Betchi, A. and Rein, M. (2001) Strahlplattieren - ein kaltes Verfahren zur Oberflächenbeschichtung. 10. STAB-Workshop, DLR, Göttingen, 14.-16. Nov. 2001. Volltext nicht online.

Esquieu, Sebastien and Meheut, Michael and Geyr, Frhr. Heiko von and Brodersen, Olaf (2006) Far-Field Drag Extraction fromNumerical Solutions and Wake Surveys. In: ODAS Proceedings. ODAS 2006 (ONERA DLR Aerospace Symposium), 2006-10-04 - 2006-10-06, Toulouse (France). Volltext nicht online.

Esser, B. and Gülhan, A. and Schäfer, R. and Mack, A. (2003) Experimental investigation of thermomechanical fluid structure interaction in high-enthalpy flow. ICTS 5th Congress on Thermal Stresses and related Topics, Blacksburg (usa), 09.-11.06.2003. Volltext nicht online.

Esser, B. and Gülhan, A. and Schäfer, R. and Mack, A. (2003) Experimental investigation of thermomechanical fluid-structure interaction in high-enthalpy flow. 5th Congress on Thermal Stresses and related topics, Blacksburg, Virginia, USA 5. - 8. June 2003. Volltext nicht online.

Esser, Burkard and Gülhan, Ali (2006) Thermal Fluid-Structure Interaction in Different Atmospheres. 5th European Workshop on Thermal Protection Systems and Hot Structures, SP-631. Volltext nicht online.

Esser, Burkard and Gülhan, Ali and Kuhn, Markus (2007) Thermal qualification of transpiration cooling for atmospheric entry. In: Proceedings of the 1st CEAS European Air and Space Conference, pp. 3205-3210. 1st CEAS European Air and Space Conference, 2007-09-10 - 2007-09-13, Berlin (Germany). Volltext nicht online.

Ewert, R. (2004) Computation of trailing edge noise applying acoustic perturbation equations. Abhandlungen aus dem Aerodynamischen Institut, 1 (34), pp. 365-398. ISSN 0172-3898. Volltext nicht online.

Ewert, R. and Bauer, M. (2004) Towards the prediction of broadband trailing edge noise. 10th AIAA/CEAS Aeroacoustics Conference, Manchester (uk), 10.-12.05.2004. Volltext nicht online.

Ewert, R. and Delfs, J.W. and Lummer, M. (2003) Perturbation Approaches to the Simulation of Airframe Noise. EUROMECH Kolloquium 449, Chamonix (fr), 09.-12.12.2003. Volltext nicht online.

Ewert, R. and Delfs, J.W. and Lummer, M. and Bauer, M. (2004) The Simulation of Airframe Noise Applying Euler-Perturbation and Acoustic Analogy Approaches. In: ECCOMAS 2004, 4th European Congress on Computational Methods in Applied Sciences and Engineering, CD-ROM. ECCOMAS 2004, Jyväskylä (fi), 24.-28.07.2004. ISBN 951-39-1869-6. Volltext nicht online.

Ewert, R. and Schröder, W. (2004) On the simulation of trailing edge noise with a hybrid LES/APE method. Journal of Sound and Vibration, 270 (1), pp. 509-524. Volltext nicht online.

Ewert, R. and Yin, J. and Delfs, J. (2003) Simulation of Multi-Geometry Scattering Problems and the Radiation and Refraction of Acoustic Waves Through a Shear Layer with Instability Waves Suppressed. 4th Computational Aeroacoustics (CAA) Workshop on Benchmark Problems, Brook Park/Cleveland (usa), 08.-10.10.2003. Volltext nicht online.

Ewert, R. and Yin, J. and Delfs, J.W. (2004) Simulation Of Multigeometry Scattering Problems And The Radiation And Refraction of Acoustic Waves Through A Shear Layer With Instability Waves Suppressed. 4th Computational Aeroacoustics (CAA) Workshop on Benchmark Problems, Brook Park/Ohio (usa), 20.-22.10.2003. Volltext nicht online.

Ewert, R. and Zhang, Q. and Schröder, W. and Delfs, J.W. (2003) Computation of Trailing Edge Noise of a 3D Lifting Airfoil in Turbulent Subsonic Flow. 9th AIAA/CEAS Aeroacoustics Conference, Hilton Head (usa), 12.-14.05.2003. Volltext nicht online.

Ewert, Roland (2007) CAA prediction of slat cove filler effect on broadband slat noise sound generation and radiation. Journal of Sound and Vibration, 304, pp. 421-449. Elsevier. Volltext nicht online.

Ewert, Roland and Hartmann, R. and Held, J. and Leicht, T. and Bauer, M. and Ashcroft, G. and Weckmüller, C. and Guerin, S. and Schady, A. and Heimann, D. and Siefert, M. and Heintze, O. and Unruh, O. and Mühlbauer, Bernd and Noll, Berthold (2010) Advanced Numerical Tools Graduation for Aeronautical Research and Development. Project Report. 160 S. Volltext nicht online.

Ewert, Roland and Manoha, Eric (2007) Trailing edge noise. In: Large-Eddy Simulation for Acoustics Cambridge University Press. pp. 293-333. ISBN 978-0-521-87144-0. Volltext nicht online.

Ewert, R. and Appel, C. and Dierke, J. and Herr, M. (2009) RANS / CAA based prediction of NACA0012 broadband trailing edge noise and experimental validation. In: AIAA Paper 2009-3369. 15th AIAA/CEAS Aeroacoustics Conference, 11 - 13 May 2009, Miami, Florida. Volltext nicht frei.

Ewert, Roland (2007) RPM - the fast Random Particle-Mesh method to realize unsteady turbulent sound sources and velocity fields for CAA applications. In: AIAA Pap. 2007-3506. 13th AIAA/CEAS Aeroacoustics Conference, 2007-05-21 - 2007-05-23, Rome, Italy.

F

Fassbender, J.K. (2004) Improved Robustness for Numerical Simulation of Turbulent Flows around Civil Aircraft at Flight Reynolds Numbers. DLR-Forschungsbericht. 2003-09. Dissertation. 266 S. Volltext nicht online.

Fazzolari, A. and Gauger, N.R. and Brezillon, J. (2004) Sensitivity Evaluation For Efficient Aerodynamic Shape Optimization With Aeroelastic Constraints. In: CD. ECCOMAS 2004, Jyväskylä (fi), 24.-28.07.2004. Volltext nicht online.

Fazzolari, Antonio and Gauger, Nicolas and Brezillon, Joel (2005) An aero-structure adjoint formulation for efficient multidisciplinary wing optimization. In: Proceedings of EUROGEN 2005. EUROGEN 2005, Munich. Volltext nicht online.

Fazzolari, Antonio and Gauger, Nicolas and Brezillon, Joel (2007) Efficient aerodynamic shape optimization in MDO context. Journal of Computational and Applied Mathematics, 203, pp. 548-560. Volltext nicht online.

Fazzolari, Antonio and Gauger, Nicolas and Brezillon, Joel (2005) Efficient aerodynamic shape optimization in MDO context. In: Proc. Appl. Math. Mech., 5, pp. 739-740. GAMM 2005, Luxemburg. Volltext nicht online.

Faßbender, J. and Heinrich, R. and Kroll, N. and Le Chuiton, F. (2002) Machbarkeitsstudie zur Integration spezifischer Funktionalitäten von EUVISC in FLOWer. DLR-Interner Bericht. 124-2002/33. 24 S. Volltext nicht online.

Fedorova, N.N. and Fedorchenko, I.A. and Schülein, E. (2001) Investigation and Numerical Simulation of the Impinging Oblique Shock Wave /Turbulent Boundary Layer Interaction at M = 5. In: Short Communications in Mathematics and Mechanics, ZAMM, Vol. 81, Suppl. 3, pp. 773-774. GAMM – Göttingen, Germany, April 2-7, 2000. ISBN 0946-8463. Volltext nicht online.

Fedorova, N.N. and Fedorchenko, I.A. and Schülein, E. (2000) Impinging shock wave / flat plate turbulent boundary layer interaction at M=5 (experiments and computations). In: International Conference on Methods of Aerophysical Research, Part 1, pp. 71-77. Publishing House of S B RAS. X International Conference on Methods of Aerophysical Research 9 – 16 July 2000, Novosibirsk, Russia. Volltext nicht online.

Fedorova, N.N. and Fedorchenko, I.A. and Schülein, E. (2001) Experimental and numerical study of oblique shock wave / turbulent boundary layer interaction at M=5. 7th Russian-Japanese CFD Workshop at Moscow State University, July 31-August 4, 2001. ISBN 0918-6654. Volltext nicht online.

Fedorova, N.N. and Fedorchenko, I.A. and Schülein, E. (2003) Impinging shock wave / flat plate turbulent boundary layer interaction at M=5 (experiments and computations). 3rd International Symposium ATMOSPHERIC REENTRY VEHICLE AND SYSTEMS, ARCACHON (France), 24-27 March, 2003. Volltext nicht online.

Frahnert, H. (2003) Optische Messtechnik in der Lärmimmissionsforschung. Presseverteiler der Öffentlichkeitsarbeit, Nr. 202 - 35. Woche (Göttinger Tageblatt), Seite:WissenschaftundWetter-. Volltext nicht online.

Frahnert, H. (2004) Some Review on Reynolds Averaging. 17th Annual Liepmann-Ludwieg Seminar, California Institute of Technology, Guggenheim, CA, USA, 22. June 2004. Volltext nicht online.

Frahnert, H. (2004) Measurement of model location and model deformation in wind tunnels. European Windtunnel Association Initial Joint Workshop, Toulouse, October18-20,2004. Volltext nicht online.

Frahnert, H.,, and Dallmann, Uwe Ch. (2002) Examination of the eddy-viscosity concept regarding its physical justification. In: New Results in Numerical and Experimental Fluid Mechanics III., Vol. 77, pp. 255-262. Springer. 12. AG STAB / DGLR -Symposium, Stuttgart, 15.-17. Nov. 2000. Volltext nicht online.

Fricke, D. (2002) Implementierung einer allgemeinen Transformationsvorschrift in den Navier-Stokes-Löser FLOWer für die einfache Vorgabe von Drehachsen und Gelenkpositionen zur Strömungssimulation um Hubschrauber. DLR-Interner Bericht. IB 124-2002/6. Diploma. 87 S. Volltext nicht online.

Fricke, Sebastian and Grossrubatscher, Michael (2014) Certification and Performance Determination of a Research Aircraft with External Installations. RAeS Research Aircraft Operations Conference, 03.-05. Nov. 2014, London, Vereinigtes Königreich. Volltext nicht online.

G

Ganzevles, F.L.A. and de Bruin, A.C. and Puffert-Meißner, W. (2002) A quantitative analysis of viscous and lift-induced drag components from detailed wake measurements behind a half model. CEAS Aerospace Aerodynamics Research Conference, Cambridge (uk), 10.-12.06.2002. Volltext nicht online.

Gatlin, Greg and Rivers, Melissa, B. and Goodliff, Scott, l. and Rudnik, Ralf and Sitzmann, Martin (2008) Experimental Investigation of the DLR-F6 Transport Configuration in the National Transonic Facility. In: AIAA 2008-6917. 26th AIAA Applied Aerodynamics Conference, 2008-08-18, Honululu, HI, USA. Volltext nicht online.

Gauger, N. (2001) Vergleich der diskreten und der kontinuierlichen Adjungierten und letztere in der Anwendung der aerodynamischen Optimierung. Forschungsseminar 'Adjunktorensysteme', Dresden (de), 12.06.2001. Volltext nicht online.

Gauger, N. (2001) Hand-coded Adjoints in Aerodynamic Applications. Minisymposium 'Automatic Differentiation and Partial Differential Equations' at the SIAM Annual Meeting 2001, San Diego (USA), 9.-13.7.2001. Volltext nicht online.

Gauger, N. (2001) Aerodynamic Shape Optimization using the Adjoint Euler Equations. In: Discrete Modelling and Discrete Algorithms in Continuum Mechanics, pp. 87-96. Logos Verlag, Berlin (de). Workshop on 'Discrete Modelling and discrete Algorithms in Continuum Mechanics', Braunschweig (de), 24.-25.11.2000. ISBN 3-89722-683-9. Volltext nicht online.

Gauger, N. (2001) Aerodynamic Shape Optimization using Adjoint Method. Minisymposium 'Numerical Methods in Shape Optimization' at the SIAM-EMS Conference 2001, Berlin (de), 02.-06.09.2001. Volltext nicht online.

Gauger, N. (2001) Aerodynamic Shape Optimization using Adjoint Method. 4th Annual CFD Symposium, Bangalore (india), 10.-11.08.2001. Volltext nicht online.

Gauger, N. (2002) Das Adjungiertenverfahren in der aerodynamischen Formoptimierung. Graduiertenkolleg 'Wechselwirkung von Struktur und Fluid', TU Braunschweig, Braunschweig (de), 27.06.2002. Volltext nicht online.

Gauger, N. (2003) Das Adjungiertenverfahren in der aerodynamischen Formoptimierung. DLR-Forschungsbericht. 2003-05. Dissertation. 102 S. Volltext nicht online.

Gauger, N. (2004) Aerodynamische Formoptimierung mit dem Adjungiertenverfahren im MDO-Kontext. Gastvortrag am SFB568 der TU Darmstadt, Darmstadt (de), 13.12.2004. Volltext nicht online.

Gauger, N. and Brezillon, J. (2002) DLR's Technical Annex to the 2nd Year Progress Report of the European Project AEROSHAPE. DLR-Interner Bericht. 124-2002/13. Volltext nicht online.

Gauger, N. and Brezillon, J. (2005) The Continous Adjoint Approach in Aerodynamic Shape Optimization. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 181-193. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6. Volltext nicht online.

Gauger, N. and Mauß, M. (2001) Das Adjungiertenverfahren in der aerodynamischen Optimierung von Turbomaschinen. DLR-Interner Bericht. 129-2001/22. 22 S. Volltext nicht online.

Gauger, N.R. (2004) Adjoint Formulations for the Structural Shape Optimization of Turbine Blades. DLR-Interner Bericht. 124-2004/901. 7 S. Volltext nicht online.

Gauger, N.R. (2003) Adjoint Methods. ERCOFTAC, Garching/München (de), 01.-03.04.2003. Volltext nicht online.

Gauger, N.R. (2004) Ongoing activities in shape optimization within the German project MEGADESIGN. EUCCO2004, Dresden (de), 29.-31.03.2004. Volltext nicht online.

Gauger, N.R. (2004) Efficient Aerodynamic Shape Optimization in MDO Context. PDE, Scientific Computing and Optimization in Applications, Trier (de), 08.-10.09.2004. Volltext nicht online.

Gauger, N.R. (2003) Potential von Adjungiertenverfahren in der Optimierung von Hochauftriebssystemen. Kolloquium zur Verabschiedung von Prof. H. Körner, Braunschweig (de), 13.02.2003. Volltext nicht online.

Gauger, N.R. (2004) Adjungiertenverfahren. Seminar der Konzernforschung der Volkswagen AG, Wolfsburg (de), 13.07.2004. Volltext nicht online.

Gauger, N.R. (2003) Aero-Struktur-Optimierung mit dem Adjungiertenverfahren. Gastvortrag am SFB401 der RWTH Aachen, Aachen (de), 07.02.2003. Volltext nicht online.

Gauger, N.R. and Brezillon, J. (2002) Aerodynamic Shape Optimization Using Adjoint Method. Journal of the Aeronautical Society of India, 54 (3), pp. 247-254. Volltext nicht online.

Gauger, N.R. and Kroll, N. and Brezillon, J. (2003) Aerodynamic Shape Optimization Based on Adjoint Formulations of the Compressible Euler/Navier-Stokes Equations for Complex Applications. In: Numerical Techniques for Optimization Problems with PDE Constraints. Numerical Techniques for Optimization Problems with PDE Constraints, Oberwolfach (de), 16.-22.02.2003. Volltext nicht online.

Gauger, Nicolas (2006) Adjoint approaches in aerodynamic shape optimization and MDO context. In: Proceedings of ECCOMAS CFD 2006. ECCOMAS CFD 2006, Egmond an Zee. ISBN 90-9020970-0. Volltext nicht online.

Gauger, Nicolas (2005) Adjoint flow solvers for aerodynamic shape optimization. ERCOFTAC Bulletin, 66, pp. 9-11. Volltext nicht online.

Gauger, Nicolas and Fazzolari, Antonio (2009) Adjoint Methods for Coupled CFD-CSM Optimization. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 107. Springer. pp. 237-246. ISBN 9783642040924. ISSN 16122909. Volltext nicht online.

Gauger, Nicolas and Griewank, Andreas and Riehme, Jan (2008) Extension of fixed point PDE solvers for optimal design by one-shot method - With first applications to aerodynamic shape optimization. European Journal of Computational Mechanics (REMN), 17, pp. 87-102. Volltext nicht online.

Gauger, Nicolas and Walther, Andrea and Moldenhauer, Carsten and Widhalm, Markus (2007) Automatic differentiation of an entire design chain for aerodynamic shape optimization. Springer. STAB 2006, Darmstadt. Volltext nicht online.

Gehlhar, B. and Pott-Pollenske, M. and Buchholz, H. and Dobrzynski, W. (2002) Lärmmessung an einer MD-11 zur Ermittlung lärmminimaler Landeverfahren. DLR-Interner Bericht. IB 124-2002/45. 27 S. Volltext nicht online.

Geissler, Wolfgang and Dietz, Guido and Mai, Holger and Bosbach, Johannes and Richard, Hugues (2005) Dynamic Stall and its Passive Control Investigations on the OA209 Airfoil Section. In: Proceedings - 31th European Rotorcraft Forum. 31th European Rotorcraft Forum, 2005-09-13 - 2005-09-16, Florence, Italy (Europe). Volltext nicht online.

Geißler, W. (2003) Dynamic Stall Control by Static Flap Deflection. DLR-Interner Bericht. 224 - 2002 C 07. 48 S. Volltext nicht online.

Geißler, W. (2003) Dynamic Stall Control by Static Flap Deflection. DLR-Interner Bericht. 224 - 2002 A 17. 11 S. Volltext nicht online.

Geißler, W. (2004) Dynamic Stall. DLR-Interner Bericht. 224 - 2004 A 04. 43 S. Volltext nicht online.

Geißler, W. (2005) Dynamic Stall. DLR-Interner Bericht. 224 - 2005 A 04. 24 S. Volltext nicht online.

Geißler, W. and Dietz, G. and Mai, H. (2003) Dynamic Stall on a Supercritical Airfoil. 29th European Rotorcraft Forum, Friedrichshafen, 16-18 September 2003. Volltext nicht online.

Gerhold, Thomas and Evans, John (1999) Efficient Computation of 3D-Flows for Complex Configurations with the DLR-TAU Code. In: New Results in Numerical and Experimental Fluid Mechanics, 72, pp. 178-185. Vieweg. AG STAB Symposium, 1998-11-10 - 1998-11-12, Berlin. ISBN 3-528-03122-0. Volltext nicht online.

Gerhold, Thomas and Kroll, Norbert (2008) Parallel Computimg in Aircraft Design - Strategies, Methods and Applications. PARCFD 2008, 2008.19.5 - 2008.22.5, Lyon, France. (Unpublished) Volltext nicht online.

Gerhold, Thomas and Neumann, Jens (2007) The parallel mesh deformation of the DLR TAU-Code. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 96. Springer-Verlag Berlin Heidelberg 2007. pp. 162-169. ISBN 3-540-74458-4. Volltext nicht online.

Gerhold, Thomas and Neumann, Jens (2006) The parallel mesh deformation of the DLR TAU-Code. 15. DGLR-Fach-Symposium der STAB, 2006-11-29-2006-12-01, Darmstadt (Germany). (Submitted) Volltext nicht frei.

Geyr, H. von (2003) Effects of external Flow Speed on the Thrust Determination of Jet Powered Configurations in the Wind Tunnel using the Static Calibration Procedure. RTO-Symposium AVT-100, Warschau (pl), 07.-09.10.2003. Volltext nicht online.

Geyr, H. von and Hoheisel, H. and Rossow, C.-C. (2002) Numerical and Experimental Study of Engine/Airframe Interference Effects for Engines with Different Bypass Ratios. CEAS Aerospace Aerodynamics Research Conference, Cambridge (uk), 10.-12.06.2002. Volltext nicht online.

Geyr, H. von and Rossow, C.-C. and Hoheisel, H. (2004) Influence of Transonic Flow on the Thrust Determination of TPS during Wind Tunnel measurements. In: New Results in Numerical and Experimental Fluid Mechanics IV, 87, pp. 475-482. Springer Verlag, Berlin, Heidelberg, New York. 13th STAB/DGLR Symposium, München (de), 12.-14.11.2002. ISBN 3-540-20258-7. Volltext nicht online.

Geyr, H. von and Rossow, C.-C. and Hoheisel, H. (2002) Influence of transonic Flow on the Thrust Determination of TPS during Wind Tunnel measurements. 13. DGLR-Fachsymposium der AG STAB, München (de), 12.-14.11.2002. Volltext nicht frei.

Geyr von, Heiko and Schade, Niko (2007) Prediction Capabilities of Maximum Lift Effects for Realistic High-Lift-Commercial Aircraft-Configurations within the European Project EUROLIFT II. First CEAS European Air and Space Conference, 2007-09-10 - 2007-09-13, Berlin. Volltext nicht online.

Geyr von, Heiko and Schade, Niko and Burg van der, Jan Willem and Eliasson, Peter and Esquieu, Sebastien (2007) CFD-Prediction of Maximum-Lift-Effects on Realistic High-Lift-Commercial-Aircraft-Configurations within the European Project EUROLIFT II. 25th AIAA Applied Aerodynamics Conference, 2007-06-25 - 2007-06-28, Miami, FL, USA. Volltext nicht online.

Goldhahn, E. and Klinge, F. (2003) Weiterentwicklung der experimentellen Hintergrund Schlieren Methode zu einem universell einsetzbaren, quantitativ messenden Dichtemessverfahren. 11. STAB Workshop, DLR Göttingen, 04.11.-06.11.2003. Volltext nicht online.

Goldhahn, Erik (2005) The Background Oriented Schlieren method (BOS) for quantitative evaluation of three dimensional density distributions. BUAA, 2005-06-15, Peking (China). Volltext nicht online.

Goldhahn, E., TU-Hannover, (2004) Weiterentwicklung von BOS (Background Oriented Schlieren) zu einem universellen 3D Dichtefeldmessverfahren. DFG-Jahreskolloquium, Rostock, 04.11.-06.11.2004. Volltext nicht online.

Goldhahn, E., TU-Hannover, and Klinge, F. (2004) The BOS (Backround Oriented Schlieren) method for measurement of density gradients. EWA-Meeting, ONERA, Tolouse, France18.10.-20.10.2004. Volltext nicht online.

Grogger, H.A. and Lummer, M. and Lauke, T. (2001) Simulating the Interaction of a Three-Dimensional Vortex with Airfoils Using CAA. In: CD-Proceedings. 7th AIAA/CEAS Aeroacoustics Conference, Maastricht (nl), 28.-30.05.2001. Volltext nicht online.

Groot, K. de (2002) Druckmessung in der aerodynamischen Meßtechnik. Vorlesung in der Berufsakademie Mannheim, Mannheim (de), 16.05.2002. Volltext nicht online.

Grosche, F.-R. and Lu, M. and Kreplin, H.-P. (2002) Strömungsbeeinflussung bei stumpfen Körpern durch passive Ventilation des Nachlaufs. Springer. 13. DGLR-Fach-Symposium der STAB, München, 12.-14. Nov. 2002 (Vortrag). Volltext nicht online.

Grosche, F.-R. and Meier, G.E.A. (2001) Research at DLR Göttingen on bluff body aerodynamics, drag reduction by wake ventilation and active flow control. Journal of Wind Engineering and Industrial Aerodynamics, 89 (14/15), pp. 1201-1218. Volltext nicht online.

Grosche, Friedrich-Reinhard and Lu, Mei and Kreplin, Hans-Peter (2003) Control of flow around bluff bodies by passive wake ventilation. In: New results in numerical and experimental fluid mechanics IV Notes on numerical fluid mechanics and multidisciplinary design, 87. Springer Verlag. pp. 140-147. ISBN 3-540-20258-7. Volltext nicht online.

Gruhn, Patrick (2006) Inviscid design of the inlet for the LAPCAT Mach 8 configuration. DLR-Interner Bericht. DLR-IB 32418-2006A28. 24 S. Volltext nicht online.

Gölling, B. (2001) Experimentelle Untersuchungen des laminar-turbulenten Überganges der Zylindergrenzschichtströmung. DLR-Forschungsbericht. 2001-14. Dissertation. 148 S. Volltext nicht online.

Göring, J. and Kemptner, E. and Emunds, H. and Frieß, M. (2003) Oxidkeramische Verbundwerkstoffe für Suchkopfabdeckungen hochagiler Flugkörper. 3. DLR - Flugkörper-Workshop, Köln, 6 November 2003. Volltext nicht online.

Gülhan, Ali and Esser, Burkard and Koch, Uwe and Siebe, Frank and Riehmer, Johannes and Giordano, Domenico and Konigorski, Detlev (2009) Experimental Verification of Heat-Flux Mitigation by Electromagnetic Fields in Partially-Ionized-Argon Flows. Journal of Spacecraft and Rockets, 46 (2), pp. 274-283. American Institute of Aeronautics and Astronautics (AIAA). ISSN 0022-4650. Volltext nicht online.

Günther, G. (2002) Instationäre aeroelastische Simulation mir dem TAU-Code. Institutskolloquium, DLR Braunschweig, 29.04.2002. Volltext nicht online.

Génin, C. and Stark, Ralf and Jack, Sebastian (2013) Flow Separation in Out-of-Round Nozzles, a Numerical and Experimental Study. In: Proceedings 5th EUCASS. 5th European Conference for Aeronautics and Space Sciences EUCASS 2013, 1. - 5. Jul. 2013, München, Germany. ISBN 978-84-941531-0-5. Volltext nicht online.

Génin, C. and Stark, Ralf and Jack, Sebastian (2015) Flow separation in out-of-round nozzles, a numerical and experimental study. In: Progress in Flight Physics pp. 269-282. doi: 10.1051/eucass/201507269. Volltext nicht online.

Görtz, Stefan (2014) Proceedings of the 2nd NPU-DLR Workshop on Aerodynamics. DLR-Interner Bericht. DLR-IB 124-2014/5. Other. DLR. 373 S. Volltext nicht online.

Gülhan, Ali (2006) The Sharp Edge Hypersonic Flight Experiment SHEFEX. In: DFG Summer-School. DFG Summer-School, 2006-07-12 - 2006-07-13, Aachen (Deutschland). Volltext nicht online.

Gülhan, Ali (2006) Integrated Multi-Disciplinary Design of Hot Structures. In: DFG Summer-School. DFG Summer-School, 2006-07-12 - 2006-07-13, Aachen (Deutschland). Volltext nicht online.

Gülhan, Ali and Gruhn, Patrick (2007) Shock wave boundary layer interaction at high flap angles and high incidence of space vehicles in hypersonic flow. AIAA. 25th AIAA Applied Aerodynamics Conference, 2007-06-25 - 2007-06-28, Miami, FL (USA). Volltext nicht online.

Gülhan, Ali and Schütte, Gerrit and Stahl, Bernhard (2008) An Experimental Study on Aerothermal Heating Caused by Jet-Hypersonic Cross Flow Interaction. Journal of Spacecraft and Rockets, 45 (5). AIAA. Volltext nicht online.

Gülhan, Ali and Thiele, Thomas and Siebe, Frank and Häberle, Jürgen (2008) EXPERT Open Flap Instrumentation and its Ground Qualification. In: Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles, SP-659. 6th European Symposium on Aerothermodynamics for Space Vehicles, 2008-11-03 - 2008-11-06, Versailles, Frankreich. Volltext nicht online.

H

Haas, S. (2004) Steuerung einer 3-Achsen Scheimpflugadapters mit Servomotoren. Diploma, Universität Hannover. Volltext nicht online.

Haidn, Oskar and Ciezki, Helmut and Hannemann, Klaus and Karl, S. (2007) Selected Supersonic Combustion Activities at DLR within the European LAPCAT Project. 2nd European Conference for Aerospace Sciences (EUCASS2007), 2007-07-01 - 2007-07-06, Brussels (Belgium). Volltext nicht online.

Han, Zhong-Hua and Görtz, Stefan and Hain, Rainer (2008) A Variable-Fidelity Modeling Method for Aero-Loads Prediction. AG STAB Symposium 2008, 3-4 Nov, 2008, Aachen.

Han, Zhong-Hua and Görtz, Stefan and Zimmermann, Ralf (2009) On Improving Efficiency and Accuracy of Variable-Fidelity Surrogate Modeling in Aero-data for Loads Context. CEAS 2009 European Air and Space conference, 26-29 Oct. 2009, Manchester, UK.

Hannemann, K. and Ciezki, H. and Haidn, O. and von Wolfersdorf, J. and Rocci Denis, S. (2007) German Test Facilities for High Speed Air Breathing Propulsion. 2nd European Conference for Aerospace Sciences (EUCASS2007), 2007-07-01 - 2007-07-06, Brussels (Belgium). Volltext nicht online.

Hannemann, K. and Schramm, J.M. and Brück, S. and Longo, J.M.A. (2001) High Enthalpy Testing and CFD Rebuilding of X-38 in HEG. 4th Symposium on Aerothermodynamics for Space Vehicles, Capua (it), 14.-18.10.2001. Volltext nicht online.

Hannemann, K. and Schramm, J.M. and Brück, S. and Longo, J.M.A. (2001) High Enthalpy Testing and CFD Rebuilding of X-38 in HEG. 23rd Int. Symposium on Shock Waves, Arlington (usa), 22.-27.07.2001. Volltext nicht online.

Hannemann, Klaus (2009) Combustion Experiments Performed Within the LAPCAT I Project – An Overview. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 19. Okt - 22. Okt. 2009, Bremen. Volltext nicht online.

Hartmann, R. (2005) The role of the Jacobian in the adaptive discontinuous Galerkin method for the compressible Euler equations. In: Analysis and Numerics for Conservation Laws 1, 1. Springer Heidelberg, Berlin. ISBN 10-3-540-24834-X. Volltext nicht online.

Hartmann, R. and Houston, P., University Leichester, (2004) Adaptive Discontinuous Galerkin Finite Element Methods with Interior Penalty for the Compressible Navier-Stokes Equations. In: Numerical Mathematics and Advanced Applications, ENUMATH 2003 Springer Verlag. ISBN 3-540-21460-7. Volltext nicht online.

Hazra, S.B.; Universität Trier and Schulz, V.; Universität Trier and Brezillon, J. and Gauger, N.R. (2004) Aerodynamic Shape Optimization using Simultaneous Pseudo-Timestepping. Other. 04-2. Universität Trier, Fachbereich IV - Mathematik/Informatik. Volltext nicht online.

Hazra, Subhendu and Gauger, Nicolas (2005) Simultaneous pseudo-timestepping for aerodynamic shape optimization. In: Proc. Appl. Math. Mech., 5, pp. 743-744. GAMM 2005, Luxemburg. Volltext nicht online.

Hazra, S.B., Universität Trier, and Schulz, V., Universität Trier, and Brezillon, J. and Gauger, N.R. (2005) Aerodynamic shape optimization using simultaneous pseudo-timestepping. Journal of Computational Physics, 204 (1), pp. 46-64. Volltext nicht online.

Heddergott, A. and Psolla-Bress, H. and Haselmeyer, H. and Höhler, G. and Jacobs, M. (2001) Kraft-und Druckverteilungsmessungen am rollenden Deltaflügel im transsonischen Geschwindigkeitsbereich. 10. AG STAB-WORKSHOP, Göttingen, 14.-15. Nov. 2001. Volltext nicht online.

Heider, A. (2004) Schallabstrahlung von turbulenten Freistrahlen II – Ein neuer Zugang durch Mehrebenen-Stereo-PIV. Schwingungsphysikalisches Kolloquium III. Physikalisches Institut, Universität Göttingen, 15.01.2004. Volltext nicht online.

Heider, A. (2004) Turbulente Geschwindigkeitsfluktuationen im Freistrahl - Studie zur Bestimmbarkeit der räumlich-zeitlichen Korrelationen mittels Mehrebenen-Stereo-Particle-Image-Velocimetry. Diploma, III Physikalisches Institut der Georg-August-Universität Göttingen. Volltext nicht online.

Heider, A. and Christou, K. (2003) Rekonstruktion der Schallabstrahlung am turbulenten Düsenfreistrahl mittels Mehrebenen-Stereo-PIV. 11. STAB Workshop, DLR Göttingen, 04.11.-06.11.2003. Volltext nicht online.

Heider, A. and Christou, K. (2004) Optical noise source detection in a turbulent jet flow using Multiplane Stereo PIV. DLR/ONERA - Annex II Meeting, DLR, Köln; 6.-7.04.2004. Volltext nicht online.

Hein, S. (2002) Nonlinear Nonlocal Transition Analysis - Code Development and Results -. Abschluss-Kolloquium im DFG-Verbundschwerpunktprogramm 'Transition', Stuttgart, 22.-24. April 2002 (Vortrag).. Volltext nicht online.

Hein, S. (2003) Nonlinear nonlocal transition analysis - code development and results. In: Recent Results in Laminar-Turbulent Transition - Selected numerical and experimental contributions from the DFG priority programme "Transition" in Germany Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 86. Springer, Heidelberg. ISBN 3-540-40490-2. Volltext nicht online.

Hein, S. (2005) Nonlinear Nonlocal Transition Analysis. DLR-Forschungsbericht. 2005-10. Dissertation. 154 S. Volltext nicht online.

Hein, S. and Hohage, T. and Koch, W. (2003) Numerical computation of acoustic resonamces in open systems. Aeroacoustics research in Europe: the CEAS-ASC report on 2002 highlights, Vol. 268, pp. 822-823. Volltext nicht online.

Hein, S. and Hohage, T. and Koch, W. (2004) On resonances in open systems. Journal of Fluid Mechanics, Vol. 506, pp. 255-284. Volltext nicht online.

Hein, S. and Koch, W. (2003) Secondary Instability Theory Applied to the Fokker 100 Flight Experiment. Project Report, DLR-Interner Bericht. 224-2003 C 09. 23 S. Volltext nicht online.

Hein, S. and Koch, W. and Schöberl, J. (2005) Acoustic Resonances in a 2D High Lift Configuration and 3D Open Cavity. In: AIAA Paper 2005-2867, pp. 1-15. 11th AIAA/CEAS Aeroacoustics Conference, Monterey/CA, 23.-25.5.2005. Volltext nicht online.

Hein, S. and Koch, W. and Schöberl, J. (2005) Akustische Resonanzen in einem Hochauftriebssystem. DGLR Fachausschusssitzung T 2.3, DLR, Braunschweig, 4.2.2005. Volltext nicht online.

Hein, S. and Theofilis, V. (2001) Instability Analysis of Three-Dimensional Vortical Flows. First Symposium on Global Flow Instability and Control, Crete, Greece, 23-25 Sept. 2001. Volltext nicht online.

Hein, S. and Theofilis, V. (2001) Instability Analysis of Three-Dimensional Vortical Flows. 10. STAB-Workshop, Göttingen, 14.-15. Nov. 2001 (Vortrag). Volltext nicht online.

Hein, S. and Theofilis, V. (2002) On instability characteristics of isolated vortices and models of trailing-vortex systems. Vortrag: AMIF 2002 - Applied Mathematics for Industrial Flow Problems -, Lisbon-Portugal, April 17-20, 2002. Volltext nicht online.

Heinrich, R. (2002) Viskose und reibungsfreie, instationäre FLOWer Rechnungen - Nickwinkelschwingungen am LANN- und A340 Flügel. DLR-Interner Bericht. IB 124-2002/34. 32 S. Volltext nicht online.

Heinrich, R. and Ahrem, R. and Günther, G. and Krüger, W. and Neumann, J. (2002) Aeroelastische Simulationen unter Verwendung des AMANDA Simulationssystems. In: Fluid-Struktur-Wechselwirkung, pp. 443-458. VDI-Tagung "Fluid-Struktur-Wechselwirkung", Wiesloch (de), 11.-12.06.2002. ISBN ISBN: 3-18-091682-6; ISSN: 0083-5560. Volltext nicht online.

Heinrich, R. and Dwight, R. and Widhalm, M. and Raichle, A. (2005) Algorithmic Developments in TAU. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 93-108. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, 2002-12-10 - 2002-12-11, Braunschweig (DE). ISBN 3-540-24383-6. Volltext nicht online.

Heinrich, Ralf and Reimer, Lars and Michler, Andreas K. (2014) Multidisziplinäre Simulation des Wirbelschleppen Durchfluges eines Flugzeuges mit dem DLR TAU-Code. 19. DGLR-Fach-Symposium der STAB, 04.-05. Dez. 2014, München.

Heister, C. C. (2012) Semi-/empirical transition prediction and application to an isolated rotor in hover. International Journal of Engineering Systems Modelling and Simulation, 4 (1/2), pp. 69-78. Inderscience Enterprises Ltd. Volltext nicht frei.

Heister, C. C. and Raddatz, J. and Klein, A. (2010) Accurate Numerical Flow Simulation of Hovering Rotors using different Transition Prediction Methods. 36th ERF 2010, 06.-09.Sep., Paris. Volltext nicht frei.

Heller, G. and Dirmeier, S. and Kreuzer, P. and Streit, T. (2001) Aerodynamische Leistungssteigerung durch Flügelspitzenmodifikation am Beispiel der Envoy 7. DGLR Jahrestagung, Hamburg (de), 17.-20.09.2001. Volltext nicht online.

Heller, H. (2001) Entstehung und Minderung des Lärms von Hubschrauberrotoren. 51. Jahrestagung der Österreichischen Physikalischen Gesellschaft (ÖPG), Technische Universität Wien, Wien (a), 17.-21.09.2001. Volltext nicht online.

Heller, H. (2001) Himmlische Störenfriede. Spektrum der Wissenschaft, Ausgabe 12, pp. 64-68. Volltext nicht online.

Heller, H. and Dobrzynski, W. (2001) The Challenge To Break The Ultimate Noise Barrier: Sources and Control of Airframe Noise. 8th International Congress on Sound and Vibration, Hong Kong (vrc), 02.-06.07.2001. Volltext nicht online.

Heller, H. and Schultz, K.-J. (2001) Definition für erhöhte Schallschutzanforderungen für Hubschrauber auf der Basis der Lärmzertifikation und Erarbeitung von Schutzkriterien für lärmsensible Zeiten. DLR-Interner Bericht. 129-2001/20. 125 S. Volltext nicht online.

Heller, Hanno H. and Yin, Jianping (2007) Chapter 91. Helicopter Rotor Noise: Generation, Prediction, and Control. In: Handbook of Noise and Vibration Control (Editor: Malcolm J. Crocker) Wiley Verlag. pp. 1120-1132. ISBN 978-0-471-39599-7. Volltext nicht online.

Henckels, Andreas and Gruhn, Patrick and Gülhan, Ali (2008) Design and Experimental Verification of a Scram-Jet Inlet in Frame of ESA's LAPCAT Program. In: Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles, SP-659. 6th European Symposium on Aerothermodynamics for Space Vehicles, 2008-11-03 - 2008-11-06, Versailles, Frankreich. Volltext nicht online.

Henckels, Andreas and Gülhan, Ali and Neeb, Dominik (2007) An Experimental Study on the Base Flow Plume Interaction of Booster Configurations. In: European Air and Space Conference. DGLR. 1st CEAS European Air and Space Conference, 2007-09-10 - 2007-09-13, Berlin (Germany). ISSN 0700-408. Volltext nicht online.

Hepperle, M. (2001) The Sonic Cruiser. 10. STAB Workshop, Göttingen (de), 14.-15.11.2001. Volltext nicht online.

Hepperle, M. (2001) Nurflügel-Transportflugzeuge, Aerodynamik und Flugmechanik. Euroavia Design Workshop 2001: Blended Wing Body", Stuttgart (de), 15.-26.10.2001. Volltext nicht online.

Hepperle, M. (2002) The Sonic Cruiser - A Concept Analysis. ASTEC 2002 Symposium "Aviation Technologies of the 21st Century, Berlin (de), 07.-08.05.2002. Volltext nicht online.

Hepperle, M. (2002) Environmental Friendly Transport Aircraft. 13. DGLR-Fachsymposium der AG STAB 2002, München (de), 12.-14.11.2002. Volltext nicht online.

Hepperle, M. (2003) Strato 2C - Ein Rückblick. DFG-Abschlusskolloquium Forschergruppe "Leichter als Luft", Stuttgart (de), 29.07.2003. Volltext nicht online.

Hepperle, M. (2004) Environmental Friendly Transport Aircraft. In: New Results in Numerical and Experimental Fluid Mechanics IV, Vol. 87, pp. 26-33. Springer Verlag, Berlin, Heidelberg, New York. 13th STAB/DGLR Symposium, München (de), 12.-14.11.2002, München (DE). ISBN 3-540-20258-7. Volltext nicht online.

Hepperle, M. and Heinze, W. (2003) Future Global Range Aircraft. RTO-Symposium "Novel Vehicle Concepts and Emerging Technologies", Brüssel (bel),07.-10.04.2003. Volltext nicht online.

Hepperle, Martin and Ruiz-Leon, Alba and Runge, Hartmut and Horwath, Joachim (2007) HALE Platforms - A Feasibility Study. DLR-Interner Bericht. DLR-IB-129-2007/11. 81 S.

Herr, M. (2004) Experimental Study On Noise Reduction Through Trailing Edge Brushes. Springer Verlag. (In Press) Volltext nicht online.

Herr, M. and Dobrzynski, W. (2004) Experimental Investigations In Low Noise Trailing Edge Design. 10th AIAA/CEAS Aeroacoustics Conference, Manchester (uk), 10.-12.05.2004. Volltext nicht online.

Herr, M. and Dobrzynski, W. (2005) Experimental Investigations In Low-Noise Trailing-Edge Design. AIAA-Journal, 43 (6), pp. 1167-1175. Volltext nicht online.

Herrmann, Dirk and Triesch, Klaus (2006) Experimental investigation of isolated inlets for high agile missiles. Aerospace Science and Technology, 10, pp. 659-667. Volltext nicht online.

Herrmann, Dirk and Triesch, Klaus and Gülhan, Ali (2007) An Experimental Study of Chin-Intakes for Airbreathing Missiles with High Agility. Journal of Propulsion and Power, 24 (2), pp. 236-244. AIAA. Volltext nicht online.

Herrmann, U. (2001) Analysis of numerical prediction capabilities for SCT low-speed high-lift flows. DLR-Interner Bericht. 129-2001/16. 90 S. Volltext nicht online.

Herrmann, U. (2002) Specification of the EPISTLE wind tunnel model extension for use in the DNW NWB. DLR-Interner Bericht. IB 124-2002/46. 10 S. Volltext nicht online.

Herrmann, U. (2003) Effizientes Hochauftriebssystem für das Überschallverkehrsflugzeug. Kolloquium zur Verabschiedung von Prof. Dr. H. Körner, Braunschweig (de), 13.02.2003. Volltext nicht online.

Herrmann, U. (2003) Das Windkanalmodell des EPISTLE-Projektes. Veranstaltung 2 Jahre Modellbauzentrum DLR, Braunschweig (de), 21.03.2003. Volltext nicht online.

Herrmann, U. (2003) CISAP Cruise Speed Impact on Supersonic Aircraft Planform. 2nd KATnet Workshop on high speed aerodynamics, Bath (uk), 02.-05.09.2003. Volltext nicht online.

Herrmann, U. (2003) CISAP Cruise Speed Impact on Supersonic Aircraft Planform. DLR-Interner Bericht. IB 124-2003/35. Volltext nicht online.

Herrmann, U. (2004) Optimierender Flügelentwurf für Überschallflugzeuge: maximale Reichweite für Flugmissionen bei M=2, 1.6 & 1.3. First MEGADESIGN Workshop Braunschweig (de), 4.-5.11.2004. Volltext nicht online.

Herrmann, U. (2004) Numerical Design of a Low-Noise High-Lift System for a Supersonic Aircraft. 14th DGLR/STAB Symposium, Bremen (de), 16.-18.11.2004. Volltext nicht online.

Herrmann, U. (2004) CISAP: Cruise Speed Impact on Supersonic Aircraft Planform; a Project Overview. 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany/New York (usa), 30.08.-01.09.2004. Volltext nicht online.

Herrmann, U. (2004) Low-Speed High-Lift Performance Improvements obtained and validated by the EC-project EPISTLE. 24th ICAS Conference, Yokohama (ja), 29.08.-03.09.2004. Volltext nicht online.

Herrmann, U. (2004) High Performance High-Lift System Design for SCT in the EC-project EPISTLE. ECCOMAS 2004, Jyväskylä (fi), 24.-28.07.2004. Volltext nicht online.

Herrmann, U. (2004) Analysis of the aerodynamic off-design characteristics of the multidiscipline optimized M=1.6 CISAP configuration. DLR-Interner Bericht. 124-2004/23. 49 S. Volltext nicht online.

Herrmann, U. (2004) Low-drag high-lift system design using a viscous flow solution based manual design procedure. DLR-Interner Bericht. 124-2004/903. 67 S. Volltext nicht online.

Herrmann, U. and Geyr, H. von (2003) Preparing for SCT MDO design work. 41st AIAA Aerospace Sciences Meeting & Exhibit, Reno (usa), 06.-09.01.2003. Volltext nicht online.

Herrmann, U. and Press, A. and Newbold, C. and Kaurinkoski, P. and Artiles, C. and Muijden, J.V. and Carrier, G. (2001) Validation of European CFD Codes for SCT low-speed high-lift Computations. 19th AIAA Applied Aerodynamics Conference, Anaheim (usa), 11.-14.06.2001. Volltext nicht online.

Himisch, Jan and Melber, Stefan and Horstmann, Karl-Heinz (2006) Numerical Investigation in the Aerodynamics of Thermaling for a Glider. In: 28th OSTIV Congress / Eskilstuna 2006. 28th OSTIV Congress, Eskilstuna, Schweden. Volltext nicht online.

Hirschen, Christian and Gruhn, Patrick and Gülhan, Ali (2006) Influence of Heat Capacity Ratio on the Interaction between the External Flow and Nozzle Flow of a Scramjet. In: 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference (AIAA-2006-8095). 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference, 2006-11-06 - 2006-11-09, Canberra (Australien). Volltext nicht online.

Hirschen, Christian and Gülhan, Ali (2007) Experimental Study of the Single Expansion Ramp Nozzle Flow Properties and its Interaction with the External Flow. In: Conference Proceedings 1st Gas Air and Space Conference. 1st Gas Air and Space Conference, 2007-09-10 - 2007-09-13, Berlin (Germany). ISSN 0070-4083. Volltext nicht online.

Hirschen, Christian Mark and Gülhan, Ali (2009) Influence of Heat Capacity Ratio on Pressure and Nozzle Flow of Scramjets. Journal of Propulsion and Power, 25 (2), pp. 303-311. American Institute of Aeronautics and Astronautics (AIAA). ISSN 0748-4658. Volltext nicht online.

Hoffmann, E. and Wagner, M. (2003) Design of a Management Tool for Scientific Data at the DLR-Institute of Aerodynamics and Flow Technology: DataFinder. Integration of Numerical Simulation into the Development Process, NAFEMS2003, Wiesbaden (de), 17.-18.11.2003. Volltext nicht online.

Hohage, T. and Koch, W. and Schmidt, F. and Zschiedrich, L. (2005) Transparent Boundary Conditions for Computing Resonances. In: Proceedings of the 7th International Conference on Mathematical and Numerical Aspects of Wave Propagation, pp. 68-70. WAVES 2005, Providence, RI/USA, 20.-24.6.2005. Volltext nicht online.

Horstmann, K.H. (2001) The new ALTTA HLF fin design. European Drag Reduction Workshop, Bedford (gb), 25.-26.06.2001. Volltext nicht online.

Horstmann, K.H. and Boermans, L.M.M. (2003) Evolution of Airfoils for Sailplanes. AIAA/ICAS International Air & Space Symposium and Exposition, Dayton (usa), 14.-17.07.2003. Volltext nicht online.

Horstmann, K.H. and Meyer, J. and Rohardt, C.H. and Kommallein, S. (2003) HYLTEC Laminar Flow Systems Flight Tests: Flight Testing of Anti-Icing and Anti-Contamination Systems on the DLR Do228 Test Vehicle. CEAS 2003 Conference, London (uk), 10.-12.06.2003. Volltext nicht online.

Horstmann, K.H. and Meyer, J.B. (2004) Flight Testing of Anti-Icing and Anti-Contamination Systems for HLFC Surfaces. KATnet Flow Control Workshop, Poitiers (fr), 12.-13.10.2004. Volltext nicht online.

Horstmann, K.H. and Schrauf, G.; Airbus Deutschland and Sawyers, D.M.; Airbus UK and Sturm, H.; AOA (2002) A Simplified Suction System for an HLFC Leading Edge Box of an A320 Fin. CEAS Aerospace Aerodynamics Research Conference, Cambridge (uk), 10.-13.06.2002. Volltext nicht online.

Horstmann, K.H. and Schröder, W. (2001) Ein einfaches System zur Hybridlaminarhaltung am Seitenleitwerk des Airbus A320. 10. STAB-Workshop, Göttingen (de), 14.-15.11.2001. Volltext nicht online.

Huber, Kerstin Claudie and Loeser, Thomas and Looye, Gertjan and Liersch, Carsten M. and Lindermeir, Erwin and Kemptner, Erich and Klimmek, Thomas and Koch, Stefan and Kuchar, Richard and Nauroz, Mobin and Paul, Michael and Rein, Martin and Rode, Gerald and Rohlf, Detlef and Rütten, Markus and Schütte, Andreas and Schwithal, Jana and Siggel, Martin and Voss, Arne and Zimper, Dirk (2015) Bewertung und Entwurf von agilen und hoch gepfeilten Flugzeugkonfigurationen. DLR-Interner Bericht. DLR-IB 124-2015/913. 120 S. Volltext nicht online.

Hummel, D. and Redeker, G. (2001) A new vortex flow experiment for computer code validation. RTO-AVT Symposium on Vortex Flow and High Angle of Attack, Loen (no), 07.-11.05.2001. Volltext nicht online.

Häberle, Jürgen and Gülhan, Ali (2006) Investigation of the Performance of a Scramjet Inlet at Mach 6 with Boundary Layer Bleed. 14th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference, 2006-11-06 - 2006-11-09, Canberra (Australien). Volltext nicht online.

Hübner, A.-R. (2001) Bestimmung der dynamischen Dämpfungsderivativa von Verkehrsflugzeugen mit dem numerischen Verfahren VSAERO. DLR-Interner Bericht. 129-2001/1. Volltext nicht online.

Hübner, A.-R. (2004) Numerical determination of dynamic derivatives for transport aircraft. 14th DGLR STAB Symposium, Bremen (de), 16.-18.11.2004. Volltext nicht online.

Hübner, A.-R. and Scholz, P. (2002) Influences of the skinwaviness on the pressure distribution around the static port of the Falcon 10. DLR-Interner Bericht. IB 124-2002/42. 77 S. Volltext nicht online.

Hüttl, T. J. and Chaudhuri, M. and Wagner, Claus and Friedrich, R. (2004) Reynolds-stress balance equations in orthogonal helical coordinates and application. Zeitschrift für Angewandte Mathematik und Mechanik, 84 (6), pp. 403-416. Volltext nicht online.

Häberle, Jürgen (2006) Experimentelle Untersuchung der Innenströmung des modifizierten Hyperschalleinlaufs SCR-02 im H2K bei Mach 6. DLR-Interner Bericht. DLR IB-32418-2006A33. 77 S. Volltext nicht online.

Häberle, Jürgen and Gülhan, Ali (2007) Internal flowfield investigation of a hypersonic inlet at Mach 6 with bleed. Journal of Propulsion and Power, 23 (5). Volltext nicht online.

Häberle, Jürgen and Gülhan, Ali (2007) Investigation of the Flow Field of a 2D SCRAM-Jet Inlet at Mach 7 with optional Boundary Layer Bleed. AIAA. 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2007-07-08 - 2007-07-11, Cincinnati, OH (USA). Volltext nicht online.

Häberle, Jürgen and Gülhan, Ali (2007) Investigation of a two dimensional Scramjet Inlet Flow Field at Mach 7. Journal of Propulsion and Power. AIAA. Volltext nicht online.

Häberle, Jürgen and Gülhan, Ali (2008) Experimental Investigation of a Two-Dimensional and a Three-Dimensional Scramjet Inlet at Mach 7. Journal of Propulsion and Power, 24 (5), pp. 1023-1034. Volltext nicht online.

Häberle, Jürgen and Gülhan, Ali (2008) Investigation of Two-Dimensional Scramjet Inlet Flowfield at Mach 7. Journal of Propulsion and Power, 24 (3). Volltext nicht online.

Hübner, Andreas-René (2006) Experimental and numerical determination of dynamic derivatives of aircraft configuration. ONERA-DLR Aerospace Symposium, 2006-10-04 - 2006-10-06, Toulouse. Volltext nicht online.

Hübner, Andreas-René (2007) Experimental and numerical investigations of unsteady aerodynamic derivatives for transport aircraft configurations. In: AIAA Technical Conference. AIAA, 2007-01-09 - 2007-01-12, Reno, Nevada. Volltext nicht online.

Hübner, Andreas-René (2004) Determination of dynamic derivatives for transport aircraft. 17th Liepmann Ludwig Seminar, 2004-06-22, Caltech, Pasadena, Californien. Volltext nicht online.

Hübner, Andreas-René and Löser, Thomas (2005) Methods for determination of the unsteady aerodynamic derivatives for transport aircraft configurations. RTO-AVT-123, 2005-04-25 - 2005-04-29, Budapest. Volltext nicht online.

I

Ilic, Caslav and Widhalm, Markus and Brezillon, Joel (2012) Efficient polar optimization of transport aircraft in transonic RANS flow using adjoint gradient based approach. ECCOMAS 2012 (6th European congress on computational methods in applied sciences and engineering), September 10-14, 2012, Vienna.

Iniguez de Heredia, A. and Liersch, Carsten M. (2004) Preliminary design of a FCS for a Blended Wing Body: New challenges and concepts. In: Proceedings ODAS 2004, pp. 44-53. 6th ONERA-DLR Aerospace Symposium ODAS 2004, Berlin, 22.-23.06.2004. Volltext nicht online.

Isermann, Ullrich (2006) Ansätze zur Modellierung von Schallquellen bei der Berechnung von Fluglärm. Akustisches Kolloquium der ETH Zürich, 2006-01-25, Zürich (CH). Volltext nicht online.

Isermann, Ullrich (2008) The DLR Project "Quiet Air Traffic". In: Proceedings of 9th ONERA-DLR-Aerospace Symposium. 9th ONERA-DLR Aerospace Symposium, 2008-10-22 - 2008-10-24, Chatillon (F). Volltext nicht frei.

Isermann, Ullrich (2007) Die AzB im Vergleich mit ECAC Doc.29 3rd Edition als internationales Regelwerk. In: Tagungsband zum Seminar "Die Novelle des Fluglärmgesetzes", Müller-BBM, Planegg. "Die Novelle des Fluglärmgesetzes - Fakten - Hintergründe - Umsetzung", 2007-10-09, Planegg bei München. Volltext nicht frei.

J

Jacquin, L. and Fabre, D. and Sipp, D. and Theofilis, V. and Vollmers, H. (2003) Instability and unsteadiness of aircraft wake vortices. Aerospace Science and Technology, 7 (8), pp. 577-593. Volltext nicht online.

Janke, E. (2002) Receptivity of three-dimensional Boundary Layers to Roughness and Suction - linear and nonlinear Effects. In: New Results in Numerical and Experimental Fluid Mechanics III, Vol.77, pp. 367-374. Springer. 12. AG STAB / DGLR -Symposium, Stuttgart, 15.-17. Nov. 2000. Volltext nicht online.

Janke, E. (2001) Receptivity and transition control of swept-wing boundary layers; Effects of surface curvature and nonlinearity. 31st AIAA Fluid Dynamics Conference, Anaheim, CA, USA, June 11-14, 2001; Conf.-Paper AIAA 2001-2980. Volltext nicht online.

Johnston, I.A. and Weiland, M. and Martinez Schramm, J. and Hannemann, K. and Longo, J.M.A. (2002) Aerothermodynamics of the ARD: Postflight Numerics and Shock-Tunnel Experiments. 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno (usa), 14.-17.01.2002. Volltext nicht online.

Johnston, I.A. and Hannemann, K. and Weiland, M. and Schramm, J.M. and Longo, J.M.A. (2001) Investigation of the ARD Aerothermodynamics at DLR: An Overview. 4th Symposium on Aerothermodynamics for Space Vehicles, Capua (it), 14.-18.10.2001. Volltext nicht frei.

K

Kahl, M. (2002) Berechnung der Umströmung des ATR-A-Hubschrauberrotors im Vorwärtsflug durch die Lösung der Euler-Gleichungen. DLR-Interner Bericht. 124-2002/2. 139 S. Volltext nicht online.

Kersken, Hans-Peter and Schreiber, Andreas and Strietzel, Martin and Faden, Michael and Ahrem, Regine and Post, Peter and Wolf, Klaus and Beckert, Armin and Gerholt, Thomas and Heinrich, Ralf and Kügeler, Edmund (2000) AMANDA - A Distributed System for Aircraft Design. In: Euro-Par 2000 - Parallel Processing: 6th International Euro-Par Conference, 1900, pp. 1315-1322. Springer-Verlag. Euro-Par 2000, 2000-08-29 - 2000-09-01, München, Deutschland. Volltext nicht online.

Kessler, R. (2001) Brennkammermodellierung. Zentrumskolloquium, Braunschweig, 19.11.2001. Volltext nicht online.

Kessler, Roland (2002) Brennkammermodellierung mit dem THETA-Code. DLR-Kolloquium, 2002-02-21, Göttingen. Volltext nicht online.

Keye, Stefan (2003) Model Updating of Modal Parameters from Experimental Data and Applications in Aerospace. Dissertation, University of Greenwich. Volltext nicht online.

Khalid, M. and Dujardin, A. and Hennig, P. and Leavitt, L. and Leopold, F. and Mendenhall, M. and Prince, S. and Birch, T. (2004) Application of Various Turbulence Models to Investigate the Aerothermodynamic Performance of a NASA Dual Control Missile. AGARD AVT/RTO 2004, AIAA Conference, Rhode Island (usa), 16.-19.08.2004. Volltext nicht online.

Khier, W. and Le Chuiton, F. and Schwarz, T. (2002) Navier-Stokes Analysis of the Helicopter Rotor-Fuselage Interference in Forward Flight. CEAS Aerospace Aerodynamics Research Conference, 2002-06-10 - 2002-06-12, Cambridge, UK. Volltext nicht online.

Khier, W. and Schwarz, T. (2003) Application of Cartesian Background Grid in combination with Chimera Method to predict Aerodynamics of Helicopter Fuselage. 29th European Rotorcraft Forum, Friedrichshafen (de), 16.-18.09.2003. Volltext nicht online.

Khier, W. and Schwarz, T. and Raddatz, J. (2005) Time Accurate Simulation of the Flow Around the Complete BO105 Wind Tunnel Model. 31st European Rotorcraft Forum, Florenz (it), 13.-15.09.2005. Volltext nicht online.

Khier, Walid and Dietz, Markus and Schwarz, Thorsten and Wagner, Siegfried (2007) Trimmed CFD Simulation of a Complete Helicopter Configuration. 33rd European Rotorcraft Forum, 2007-09-13, Kazan, Russia.

Kim, Minkwan and Gülhan, Ali (2011) Plasma Manipulation Using a MHD-based Device for a Communication Blackout in Hypersonic Flights. 5th International Conference on Recent Advances in Space Technologies (RAST 2011), Istanbul, Turkey. Volltext nicht online.

Kindler, Kolja and Kreplin, Hans-Peter (2004) Kohärente Strukturen in kritischen Tragflügelströmungen. In: DGLR Jahrbuch 2004, 1 (DGLR-2004-074), pp. 265-271. Deutscher Luft- und Raumfahrtkongress, 2004-09-20 - 2004-09-23, Dresden. Volltext nicht online.

Klein, C. and Engler, R. and Raju, C. and Viswanath, P. R. and Jagadeeswarachar, S. P. (2001) PSP Measurements on a Delta Wing-Body Model in the NAL 1.2m Trisonic Wind Tunnel. In: PSP Measurements on a Delta Wing-Body Model in the NAL 1.2m Trisonic Wind Tunnel, pp. 1-33. National Aerospace Laboratories, Bangalore 560017, India, August 2001. Volltext nicht online.

Klein, Chr. (2004) Comparison of DLR02 and Optrod-B1 paint in a wind tunnel test. DLR/ONERA - Annex II Meeting, DLR, Köln, 6. - 7. April 2004. Volltext nicht online.

Klein, Christian and Sachs, Werner and Henne, Ulrich and Wiedemann, Andreas and Engler, Rolf (2003) PSP-Messungen mit Vergleich der DLR eigenen Farbe / russische B1-Farbe, durchgeführt am DLR-F10 Modell im TWG. 11. STAB Workshop, 2003-11-04 - 2003-11-06, Göttingen. Volltext nicht online.

Klein, Christian and Sachs, Werner and Henne, Ulrich and Wiedemann, Andreas and Engler, Rolf (2005) title confidential. DLR-Interner Bericht. 224-2005 C 01. Volltext nicht online.

Klein, M. and Sobieczky, H. (2002) Sensitivity of aerodynamic optimization to parameterized target functions. In: Inverse Problems in Engineering Mechanics 1, 3. Elsevier Science, Oxford. ISBN 0-08-043951-9. Volltext nicht online.

Klinge, F. (2003) Verfahren zur Positionsbestimmung von fadenförmigen Objekten mit Hilfe von VRIEDER Dargestellt am Beispiel der Positionsbestimmung eines Tragflächenspitzenwirbels. DGLR-Kongress München, 17-20.11. 2003. Volltext nicht online.

Klinge, F. (2003) Vermessung von Wirbeln mit der Hintergrundschlieren-Methode. Dissertation, Universität Hannover, Fachbereich Maschinenbau. Volltext nicht online.

Klinge, F. (2004) Messverfahren für Anwendungen in der Strömungs- und Strukturmechanik. Norddeutsches Mechanik Colloquium, Clausthal-Zellerfeld, 26.6.04. Volltext nicht online.

Klinge, F. (2004) Cross correlation based optical measurement techniques for fluid dynamics and structure analysis (Particle Image Velocimetry (PIV)). Messtechnik Vorlesung ,Tampere, Finnland, University of Technology, 7.10.2004. Volltext nicht online.

Klinge, F. (2004) Cross correlation based optical measurement techniques for fluid dynamics and structure analysis (Background Oriented Schlieren method (BOS), Image Pattern Correlation Technique (IPCT)). Messtechnik Vorlesung, Tampere, Finnland, University of Technology, 08.10.2004. Volltext nicht online.

Klinge, F. (2004) AIM Advanced Inflight Measurement techniques. Vortrag in der Clustersitzung Lenkungskreis Hochauftrieb Deutschland (LHD) in Braunschweig, 15.12.2004. Volltext nicht online.

Klinge, F. and Goldhahn, E., TU Hannover, (2004) Die Hintergrundschlieren Methode. Vorlesung,Technische Universität Clausthal, Clausthal-Zellerfeld, 14.12.2004. Volltext nicht online.

Klinge, F. and Kirmse, T. (2004) Investigation of the density and velocity distribution of a wing tip vortex by means of Background Oriented Schlieren method (BOS) and Particle Image Velocimetry (PIV). DLR/ONERA - Annex II Meeting, DLR, Köln, 6.-7.04.2004. Volltext nicht online.

Klinge, F. and Konrath, R. (2004) Cross correlation based optical measurement techniques for fluid dynamics and structure analysis (Projected Pattern Correlation Technique (PROPAC)). Messtechnik Vorlesung, Tampere, Finnland, University of Technology, 11.10.04. Volltext nicht online.

Klinge, F. and Riethmuller, M.L. (2002) Mesures locales de concentration par la méthode de Strioscopie orientée vers l'arrière-plan ou BOS (Background Oriented Schlieren). In: 8ème Congrès Francophone de Vélocimétrie Laser, Tagungsband, pp. 305-313. 17.-20.09.2002. Volltext nicht online.

Klinge, Falk (2005) Titel confidential. DLR-Interner Bericht. 224-2005 C 08. 32 S. Volltext nicht online.

Klinge, Falk and Kirmse, Tania and Kompenhans, Jürgen (2004) Investigation of the density and velocity distribution of a wing tip vortex by means of stereoscopic Background Oriented Schlieren Method (BOS) and stereoscopic Particle Image Velocimetry (PIV). In: Proceedings, Online-Publication, pp. 1-9. 12th International Symposium on Application of Laser Techniques to Fluid Mechanics, 2004-07-12 - 2004-07-15, Lisbon (Portugal). Volltext nicht online.

Klinkov, K. and Erdi-Betchi, A. and Rein, M. (2002) Diagnostics of supersonic two-phase flows applied to the cold spray process. 13. DGLR/STAB Symposium, München, 13.-15. Nov. 2002. Volltext nicht online.

Klinkov, K. and Erdi-Betchi, A. and Rein, M. (2003) Interaction of a particle-laden supersonic jet with an obstacle. STAB-Workshop, DLR, Göttingen, 04.-06.11.2003. Volltext nicht online.

Klinkov, K. and Erdi-Betchi, A. and Rein, M. (2004) Behavior of supersonic overexpanded jets impinging on plates. 14. DGLR-Fach-Symposium der STAB, ZARM/Universität Bremen, 16.-18. November 2004. Volltext nicht online.

Klinkov, K. V. and Rein, M. (2004) Particle dynamics in a shock layer produced by a supersonic jet impinging on a plate. 75th Annual Scientific Conference of the Gesellschaft für Angewandte Mathematik und Mechanik, Dresden, March 21-27, 2004. Volltext nicht online.

Klinkov, K.V. and Rein, M. (2004) Multi-exposure visualization of supersonic two-phase flows impinging on a plate. In: International Conference on the Methods of Aerophysical Research, Proceedings, Part II, pp. 101-106. Publishing House Nonparel. 12th International Conference on the Methods of Aerophysical Research Novosibirsk – Russia, 28.06.2004-03.07.2004. ISBN 5-93089-005-6. Volltext nicht online.

Klinkov, S.V. and Kosarev, V.F. and Erdi-Betchi, A. and Klinkov, K.V. and Rein, M. (2004) Determination of profile of velocity and concentration of particles in jet at exhaustion from conical nozzle under condition of cold spray. In: International Conference on the Methods of Aerophysical Research, Proceedings, Part I, pp. 131-136. Publishing House Nonparel. 12th International Conference on the Methods of Aerophysical Research, Novosibirsk, Russia, 28.06.2004 - 03.07.2004. ISBN 5-93089-004-8. Volltext nicht online.

Knopp, Tobias (2008) Validierung eines semi-empirschen Verfahrens für die instationäre Aerodynamik von Profil- und Ruderschwingungen. DLR-Interner Bericht. DLR-IB 224-2008 A 25. 25 S. Volltext nicht online.

Knopp, Tobias and Alrutz, Thomas and Schwamborn, Dieter (2006) A grid and flow adaptive wall-function method for RANS turbulence modelling. Journal of Computational Physics (220), pp. 19-40. Volltext nicht online.

Koch, Stefan and Krause, Udo (2004) Vergleich Numerik - Experiment für 2-D Profile am KRG. DLR-Interner Bericht. DLR-IB 224 - 2004 C 01. Other. 23 S. Volltext nicht online.

Koch, Uwe and Esser, Burkard and Gülhan, Ali (2006) Characterization of Martian Atmosphere Flow Fields in LBK by Laser Induced Fluorescence and Emission Spectroscopy. In: Proceedings of the 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, SP-629. 2nd International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, 2006-09-06 - 2006-09-08, Rom (Italien). Volltext nicht online.

Koch, Uwe and Riehmer, Johannes and Esser, Burkard and Gülhan, Ali (2008) Hypersonic Free Stream Characterization in LBK by Laser Induced Fluorescence and Diode Laser Absorption Spectroscopy. In: ESA Publication. 3rd Internation Workshop on Radiation of High Temperature Gases in Atmospheric Entry, 2008-09-30 - 2008-10-03, Heraklion, Kreta (Griechenland). (Unpublished) Volltext nicht online.

Koch, Uwe and Riehmer, Johannes and Esser, Burkard and Gülhan, Ali (2008) Laser Induced Fluorescence and Diode Laser Absorption Spectroscopy Measurements in CO/CO2 Hypersonic Flow of LBK. In: Proceedings of the 6th European Symposium on Aerothermodynamics for Space Vehicles, SP-659. 6th European Symposium on Aerothermodynamics for Space Vehicles, 2008-11-03 - 2008-11-06, Versailles, Frankreich. Volltext nicht online.

Koch, W. (2002) On the spatio-temporal stability of primary and secondary crossflow vortices in a three-dimensional boundary layer. Journal of Fluid Mechanics, 456, pp. 85-111. Volltext nicht online.

Koch, W. (2001) Ende der DLR-Transitionsforschung ? - Zum Stand der Entwicklung eines laminar-turbulenten Transitionskriteriums. DLR-Kolloqium, Göttingen, 22. Nov. 2001. Volltext nicht online.

Koch, W. (2001) On the spatio-temporal stability of primary and secondary crossflow vortices in a three-dimensional boundary layer. First Symposium on Global Flow Instability and Control, Crete, Greece, 23-25 Sept. 2001 (Vortrag). Volltext nicht online.

Koch, W. (2002) Zum Stand der Entwicklung eines laminar-turbulenten Transitionskriterium. Kolloquium "Thermo- und Fluiddynamik", ETH Zürich, 5. April 2002 (Vortrag). Volltext nicht online.

Koch, W. (2004) Acoustic Resonances in Rectangular Open Cavities. In: 10th AIAA/CEAS Aeroacoustics Conference, 43 (11), pp. 2342-2349. 10th AIAA/CEAS Aeroacoustics Conference, 2004-05-10 - 2004-05-12, Manchester, UK. Volltext nicht online.

Koch, W. (2004) Resonances in Open Systems. Tottori University, Tottori/Japan, 16.12.2004. Volltext nicht online.

Koch, W. (2004) Resonances in Open Systems. Kyoto University, Kyoto/Japan, 15.12.2004. Volltext nicht online.

Kompenhans, J. (2001) Gegenwärtiger Stand der Entwicklung der. In: E-H030-12-058-1, 7Seiten-. Tagungsunterlagen, Operative und strategische Ziele der Fahrzeug-AERODYNAMIK, 11.- 12. Dezember 2001, München. Volltext nicht online.

Kompenhans, J. (2001) Particle Image Velocimetry. In: Book of Abstracts. 4th InternationalSymposium in Particle Image Velocimetry, Göttingen, Germany; 17.09.-19.09.01. Volltext nicht online.

Kompenhans, J. (2001) PIV'01 CD ROM Proceedings. DLR-Mitteilung. 2001-03. Volltext nicht online.

Kompenhans, J. (2002) Experimental Methods. High Speed Aerodynamics, Institute (HSAI), CARDC, Mianyang, China, 18.10.02. Volltext nicht online.

Kompenhans, J. (2002) Application of Particle Image Velocimetry for the investigation of high speed flow fields. High Speed Aerodynamics, Institute (HSAI), CARDC, Mianyang, China, 18.10.02. Volltext nicht online.

Kompenhans, J. (2002) State-of-the art and future prospects of non-intrusive measurement techniques for aerodynamic design. Nanjing University of Aeronautics and Astronautics, China, 21.10.02. Volltext nicht online.

Kompenhans, J. (2002) Experimental Methods. Nanjing University of Aeronautics and Astronautics, China, 21.10.02. Volltext nicht online.

Kompenhans, J. (2002) State-of-the art and future prospects of non-intrusive measurement techniques for aerodynamic design. Beijing University of Aeronautics and Astronautics, China, 23.10.02. Volltext nicht online.

Kompenhans, J. (2002) Application of Particle Image Velocimetry for the investigation of high speed flow fields. Beijing University of Aeronautics and Astronautics, China, 24.10.02. Volltext nicht online.

Kompenhans, J. (2001) 'State-of-the art and future prospects of the PIV measurement technique for applications in aerodynamics'. Korea Maritime University, Pusan, Korea, 28.03.01. Volltext nicht online.

Kompenhans, J. (2001) 'State-of-the art and future prospects of the PIV measurement technique for applications in aerodynamics'. Pusan National University, Pusan, Korea, 29.03.01. Volltext nicht online.

Kompenhans, J. (2001) 'State-of-the art and future prospects of the PIV measurement technique for applications in aerodynamics'. POSTECH, Pohang, Korea, 30.3.01. Volltext nicht online.

Kompenhans, J. (2001) 'State-of-the art and future prospects of the PIV measurement technique for applications in aerodynamics'. Seoul National University, Seoul, Korea, 02.04.01. Volltext nicht online.

Kompenhans, J. (2001) 'State-of-the art and future prospects of the PIV measurement technique for applications in aerodynamics'. KARI, Taejon, Korea, 03.04.01. Volltext nicht online.

Kompenhans, J. and Bütefisch, K.-A. (2002) The Use of Modern Experimental Methods for Validation of Numerical Codes - Advances and Problems. In: Proceedings FLOWnet Workshop, 2002. FLOWnet Case Studies Open Day, January 24-25, 2002. Volltext nicht online.

Kompenhans, J. and Bütefisch, K.-A. (2001) State-of-the-art and future prospects of non-intrusive measurement techniques for aerodynamic design. In: Vortrag. Aeronautics Days 2001, Hamburg, 29 - 31 January 2001. Volltext nicht online.

Kompenhans, J. and Bütefisch, K.-A. and Schröder, A. and Engler, R. and Klein, C. and Pallek, D. and Otter, D. (2002) State-of-the-art and future prospects of non-intrusive measurement techniques for aerodynamic design. In: Seiken Symposium on "Paticle Image Velocimetry " - its application and development -, Seiken Symposium No.33, pp. 127-166. SEIKEN Symposium “Particle Imaging Velocimetry – its application and development”, August 23, 2002, Tokyo. ISBN UTNL-R-0420. Volltext nicht online.

Kompenhans, J. and Dieterle, L. and Raffel, M. and Monnier, J.-C. and Gilliot, A. and De Gregorio, F. and Pengel, K., DNW, (2001) Particle Image Velocimetry: Status of Development and Examples of Application in Industrial Test Facilities. In: 3rd ONERA-DLR Aerospace ODAS 2001, 12Seiten-. 3rd ONERA-DLR Aerospace Symposium, Paris, France, 20.06.-22.06.2001. ISBN 2-7257-006-X. Volltext nicht online.

Kompenhans, J. and Dieterle, L. and Vollmers, H. and Stuff, R. and Schneider, G. and Raffel, M. and Dewhirst, T. and Kähler, C. and Pengel, K., DNW, Emmeloord, NL, and Monnier, J.-C., ONERA, Lille, F, and Gilliot, A., ONERA, Lille, F, and Coton, P., ONERA, Lille, F, (2000) Qualitative and Quantitative Visualization of Wake Vortices in Industrial Test Facilities. In: 9th (Millennium) International Symposium on Flow Visualization, 437-1-437-10. 9th International Symposium on Flow Visualization, Heriot-Watt University, Edinburgh, August 2000. ISBN 0-9533991-1-7. Volltext nicht online.

Kompenhans, J. and Kähler, Chr. (2002) Particle Image Velocimetry an advanced experimental tool for the investigation of turbulent flow fields. Seminar, INSEAN, Rom, Italien, Dec. 6, 2002. Volltext nicht online.

Kompenhans, J. and Raffel, M. and Kähler, C. and Richard, H. and Arnott, A. and Schröder, A. and Vollmers, H. and Sammler, B. and Schneider, G. and Stasickí, B. and Agocs, J. and Mattner, H. and Micknaus, I. and Dreykluft, U. and Stanislas, M.; CNRS, LML, F, and Hinsch, K.; Uni Oldenburg and Westerweel, J.; TU Delft, NL, and Willert, C.; EN-AT and Zimmer, L.; VKI,B, (2001) Application of Particle Image Velocimetry, Theory and Partice. PIV-Course, Göttingen, Germany, 12.03.-16.03.01. Volltext nicht online.

Kompenhans, J. and Schröder, A. and Engler, R. and Klinge, F. and Stasicki, B. (2004) Development and application of image based measurement techniques for aerodynamic investigations in wind tunnels. In: High-Speed Flow Fundamental Problems, Conference Proceedings. International Scientific Conference High-Speed Flow Fundamental Problems, Zhukovsky, Russia, 21-24 September 2004. Volltext nicht online.

Kompenhans, J. and Schröder, A. and Raffel, M. and Kähler, C. and Arnott, A. and Bao, F. and Sammler, B. and Schneider, G. and Stasicki, B. and Frahnert, H. and Klinge, F. and Vollmers, H. and Agocs, J. and Mattner, H. and Stanislas, M. and Hinsch, K. and Westerweel, J. and Willert, C. and Ehrenfried, K. and Micknaus, I. and Rosenstock, C. and Henze, D. (2003) Application of Particle Image Velocimetry, Theory and Practice. In: Application of Particle Image Velocimetry, Theory and Practice, Ordner-. PIV-Course, Göttingen, Germany, 03.03.-07.03.2003. Volltext nicht online.

Kompenhans, J. and Schröder, A. and Raffel, M. and Kähler, C. and Arnott, A. and Bao, F. and Sammler, B. and Schneider, G. and Stasicki, B. and Frahnert, H. and Kuduz, M. and Klinge, F. and Vollmers, H. and Agocs, J. and Mattner, H. and Stanislas, M. and Hinsch, K. and Westerweel, J. and Willert, C. and Micknaus, I. and Rosenstock, C. (2002) Application of Particle Image Velocimetry, Theory and Partice. In: Application of Particle Image Velocimetry, Theory and Partice, Ordner-. PIV-Course, Göttingen, Germany, 04.03.-08.03.2002. Volltext nicht online.

Kompenhans, J. and Stanislas, M. (2000) Application of the PIV MeasurementTechnique for Aerodynamic Research in EC Projects. Workshop on European-Research on Aerodynamic Engine/Airframe Integration for Transport Aircraft, Braunschweig, Germany, 26.09.-27.09.00. Volltext nicht online.

Kompenhans, J. and Stasicki, B. (2004) The high-speed videostroboscope - a versatile instrument for the investigation of periodic events. European Windtunnel Association Initial Joint Workshop, Toulouse, France, 18 - 20 October 2004. Volltext nicht online.

Konrath, R. and Klinge, F. and Schröder, A. (2003) Vorstellung eines neuen optischen Messverfahrens (PROPAC) zur zeitaufgelösten flächenhaften Bestimmung von Oberflächengeschwindigkeiten zur Schwingungsanalyse von Strukturen. 11. STAB Workshop, DLR Göttingen, 04.11.-06.11.2003. Volltext nicht online.

Konrath, R. and Schröder, A. and Agocs, J. and Kompenhans, J. (2004) Machbarkeitsstudie, Auslegung und Entwurf einer PIV-Apparatur unter den erschwerten Zugänglichkeitsbedingungen am Hochdruckwindkanal des DNW-GÖ. DLR-Interner Bericht. 224-2004 C 14. 16 S. Volltext nicht online.

Konrath, Robert and Schröder, Andreas and Kompenhans, Jürgen (2005) Recent Applications or Particle Image Velocimetry for Investigation of Unsteady Flow Fields in Industrial Transonic Wind Tunnels. PivNet 2 International Workshop on the Application of PIV in Compressible Flows, 2005-06-06 - 2005-06-08, Delft (The Netherlands). Volltext nicht online.

Konrath, Robert and Schröder, Andreas and Kompenhans, Jürgen and Raffel, Markus and Bosbach, Johannes (2003) title confidential. DLR-Interner Bericht. 224-2003 C 27. 11 S. Volltext nicht online.

Konstantinov, Mikhail and Rütten, Markus and Lambert, Markus and Wagner, Claus (2009) Strahlung als wesentlicher Faktor der numerischen Simulation von Flugzeugkabineninnenströmungen für Komfortvorhersagen. (Submitted) Volltext nicht online.

Konstantinov, Mikhail and Wagner, Claus (2007) Numerical Simulation of Unsteady Nozzle Cavitation and Spray Formation under Diesel Engine Conditions.

Koop, Lars (2012) Charakterisierung von aeroakustischen Lärmquellen mit PIV und Mikrofonarraymessungen. Strömungsinduzierter Schall - Praxisrelevante Themen und Numerische Werkzeuge, 05. - 07. Mar. 2012, Erlangen, Deutschland. Volltext nicht online.

Koop, Lars and Dillmann, Andreas and Michel, U. (2004) Beeinflussung der Schallentstehung an Hinterkantenklappen durch Ausblasen Abschlussbericht: Beeinflussung komplexer turbulenter Scherschichten. Project Report. SFB 557, Teilprojekt A7. 30 S. Volltext nicht online.

Koop, Lars and Ehrenfried, Klaus and Dillmann, Andreas (2004) Reduction of Flap Side-Edge Noise: Passive and Active Flow Control. American Institute of Aeroacoustics and Astronautics (AIAA). 10th AIAA/CEAS Aeroacoustics Conference, 2004-05-10 - 2004-05-12, Manchester (United Kingdom). Volltext nicht online.

Kovar, A. (2004) Untersuchung zur Beeinflussung der Ablösung am Seitenstrahl in einer Überschallströmung. 14. DGLR-Symposium der STAB, Bremen, 16.-18. November 2004, Bremen. Volltext nicht online.

Kovar, A. and Schülein, E. (2003) Untersuchungen zur aerodynamischen Wechselwirkung von Querschubstrahlen an hochagilen Flugkörpern. 11. Stab-Workshop, DLR , Göttingen, 05.-06.11.2003. Volltext nicht online.

Kovar, A. and Schülein, E. (2004) COMPARISON OF EXPERIMENTAL AND NUMERICAL INVESTIGATIONS ON SIDE JETS IN A SUPERSONIC CROSS FLOW. Royal Aeronautical Society, London, 14./15.9.04. Volltext nicht online.

Kreplin, Hans-Peter and Raffel, Markus (2012) Vorlesung Strömungsmess- und Versuchstechnik - Wandschubspannungsmessung / Heißfilmtechnik. Vorlesung Strömungsmess- und Versuchstechnik, 04.-08. Juni 2012, Göttingen, Deutschland. Volltext nicht online.

Krogmann, P. and Schülein, E. and Stanewsky, E. (1996) Survey of some recent investigations in the DLR Ludwieg tube wind tunnel facility (RWG). In: International Conference on Methods of Aerophysical Research. VIII International Conference on Methods of Aerophysical Research; 2 – 6 September, 1996, Novosibirsk, Russia. Volltext nicht online.

Kroll, N. (2002) MEGAFLOW - An Industrial Flow Simulation Tool für Aircraft Applications. In: Lecture Notes in Computational Science and Engineering, pp. 21-28. Springer. Fortwihr-Konferenz 2001, Erlangen (de), 13.-14.03.2001. Volltext nicht online.

Kroll, N. (2004) Flow Simulation and Shape Optimization in Aircraft Design. PDE, Scientific Computing and Optimization in Applications, Trier (de), 08.-10.09.2004. Volltext nicht online.

Kroll, N. and Faßbender, J.K. (2005) MEGAFLOW - Numerical Flow Simulation for Aircraft Design Results of the second phase of the German CFD initiative MEGAFLOW, presented during its closing syposium at DLR, Braunschweig, Germany, December 10 and 11, 2002. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6. Volltext nicht online.

Kroll, N. and Gauger, N. (2001) Industrial Aerodynamic Aircraft Design - Potential of Adjoint Approaches for Shape Optimization. Workshop 'Adjoints - Analysis and Applications', Decin (cz), 27.-29.09.2001. Volltext nicht online.

Kroll, N. and Gauger, N. and Wild, J. and Brezillon, J. and Ronzheimer, A. (2002) Numerical Shape Optimization for Aircraft Design. Workshop on Optimization in Partial Differential Equations and Applications, Heidelberg (de), 07.-09.10.2002. Volltext nicht online.

Kroll, N. and Gerhold, T. and Melber, S. and Heinrich, R. and Schwarz, T. and Schöning, B. (2002) Parallel Large Scale Computations for Aerodynamic Aircraft Design with the German CFD System MEGAFLOW. In: Parallel Computational Fluid Dynamics - Practice and Theory Elsevier Science B.V.. pp. 227-236. ISBN 0444 506721. Volltext nicht online.

Kroll, N. and Gerhold, T. and Melber, S. and Heinrich, R. and Schwarz, T. and Schöning, B. (2002) Parallel Large Scale Computations for Aerodynamic Aircraft Design with the German CFD System MEGAFLOW. In: Parallel Computation Fluid Dynamics - Practice and Theory Elsevier Science B.V.. pp. 227-236. ISBN 0-444-50672-1. Volltext nicht online.

Kroll, N. and Heinrich, R. (2004) MEGAFLOW - A numerical Simulation Tool for Aircraft Design. JAXA ANSS2004 (Aerospace Numerical Simulation Symposium), Tokyo (ja), 24.-25.06.2004. Volltext nicht online.

Kroll, N. and Rossow, C.-C. and Schwamborn, D. and Becker, K. and Heller, G. (2002) MEGAFLOW - A Numerical Flow Simulation Tool For Transport Aircraft Design. In: CD-Rom, 1.105.1-1.105.20. ICAS Congress 2002, 2002-09-09 - 2002-09-13, Toronto (CAN). Volltext nicht online.

Kroll, Norbert (2007) Challenges for Development of Numerical Simulation. In: 2007 Berlin, First CEAS Conference. 1st CEAS Conference, 2007-09-10, Berlin, Germany. Volltext nicht online.

Kroll, Norbert (2007) Challenges for Development of Numerical Simulation. In: 2007 Berlin, First CEAS Conference. 1st CEAS Conference 2007, 2007-09-10, Berlin, Germany. Volltext nicht online.

Kroll, Norbert (2009) ADIGMA - A European Project on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications. In: 2009 47th AIAA Aerospace Sciences Conference, Orlando. 47th AIAA Aerospace Sciences Meeting, 2009-01-05, Orlando, Miami (USA). (Unpublished) Volltext nicht online.

Kroll, Norbert and Becker, Klaus (2007) Numerical Simulation of Aircraft Aerodynamics - Success and Expectation. In: International Supercomputing Conference, Dresden, June 2007. International Supercomputing Conference, Dresden, 2007-06-26, Dresden (Germany). Volltext nicht online.

Kroll, Norbert and Becker, Klaus (2007) Numerical Simulation of Aircraft Aerodynamics - Success and Expectation. In: 22nd ISC'07 Dresden. 22nd International Supercomputing Conference ISC'07, 2007-06-26, Dresden (Germany). Volltext nicht online.

Kroll, Norbert and Becker, Klaus and Klenner, J. and Cross, M. (2007) Future Simulation Concept. In: 1st CEAS Confrence, Berlin (2007). 1st CEAS Conference, 2007-09-10, Berlin, Germany. Volltext nicht online.

Kroll, Norbert and Becker, Klaus and Rieger, Herbert and Thiele, Frank (2006) ONGOING ACTIVITIES IN FLOW SIMULATION AND SHAPE OPTIMIZATION WITHIN THE GERMAN MEGADESIGN PROJECT. ICAS 2006, 25th International Congress of the Aeronautical Sciences, 2006-09-03 - 2006-09-08, Hamburg.

Kroll, Norbert and Brezillon, Joel and Ronzheimer, Arno (2007) Numerical Shape Optimization. In: DLR Visit at NPU, China (June 2007). DLR Visit at NPU, China (June 2007), 2007-06-03, Xi'an (China). (Unpublished) Volltext nicht online.

Kroll, Norbert and Brezillon, Joel and Ronzheimer, Arno (2007) Numerical Shape Optimization. In: 2007 DLR Visit at NPU, China. 2007 Visit at NPU, China, 2007-06-03, Xi'an (China). Volltext nicht online.

Kroll, Norbert and Gauger, Nicolas and Brezillon, Joel and Becker, Klaus and Schulz, Volker (2004) Ongoing Activities in Shape Optimization Within The German Project MEGADESIGN. In: CD. ECCOMAS 2004, 2004-07-24 - 2004-07-28, Jyväskylä (FI). Volltext nicht online.

Kroll, Norbert and Klenner, J. and Becker, Klaus and Cross, M. (2007) Future Simulation Concept. In: 2007 Berlin, First CEAS Conference. 1st CEAS Conference 2007, 2007-09-10, Berlin, Germany. Volltext nicht online.

Kroll, Norbert and Rossow, Cord-Christian and Schwamborn, Dieter (2005) The MEGAFLOW-Project - Numerical Flow Simulation for Aircraft. In: Progress in Industrial Mathematics at ECMI 2004 Springer-Verlag Berlin Heidelberg New York. pp. 3-33. Volltext nicht online.

Kroll, Norbert and Schwamborn, Dieter (2007) Development of CFD Tools at DLR. In: 2007 DLR Visit at NPU, China. NPU, China 2007, 2007-06-03, Xi'an (China). Volltext nicht online.

Kroll, Norbert and Schwamborn, Dieter (2007) Development of CFD Tools at DLR - Activities Trends. In: 2007 DLR Visit at NPU, China. 2007 Visit at NPU, China, 2007-06-03, Xi'an (China). Volltext nicht online.

Krumbein, A. (2002) Transition Prescription and Prediction. DLR-Interner Bericht. IB 124-2002/7. 79 S. Volltext nicht online.

Krumbein, A. (2003) On Modeling of Transitional Flow and its Application on a High Lift Multi-element Airfoil Configuration. 41st AIAA Aerospace Sciences Meeting and Exhibit, Reno (usa), 06.-09.01.2003. Volltext nicht online.

Krumbein, A. (2005) Transition Modeling in FLOWer - Transition Prescription and Prediction. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 45-62. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6. Volltext nicht online.

Krumbein, A. and Stock, H.W. (2002) Description of Transitional Flow Modeling. DLR-Interner Bericht. IB 124-2002/8. 56 S. Volltext nicht online.

Krumbein, A. (2003) Transitional Flow Modeling and Application to High-Lift Multi-Element Airfoil Configurations. Journal of Aircraft, 40 (4), pp. 786-794.

Krumbein, A. (2003) On Modeling of Transitional Flow and its Application on a High Lift Multi-element Airfoil Configuration. 41st AIAA Aerospace Sciences Meeting and Exhibit, Reno (usa), 06.-09.01.2003, 2003-01-06 - 2003-01-09, Reno, NV (USA).

Krumbein, A. (2004) Automatic Transition Prediction and Application to High-Lift Multi-Element Configurations. 34th AIAA Fluid Dynamics Conference and Exhibit, Portland (usa), 28.06.-01.07.2004, Portland (USA).

Krüger, Hans and Brucks, Antje and Božić, Ognjan and Longo, José and Theil, Stephan and Richter, Lutz and Feuerbacher, Berndt (2007) Concepts for Lunar Sample Return Missions. 9th ILEWG International Conference on Exploration and Utilisation of the Moon (ICEUM9), 22.10.2007 - 26.10.2007, Sorrento (Italien). Volltext nicht online.

Kähler, C. and Sammler, B. and Kompenhans, J. (2001) Generation and Control of Particle size distributions for Optical Velocity Measurement Techniques in Fluid Mechanics. 4th International Symposium on Particle Image Velocimetry, Göttingen, Germany, September 17-19, 2001. Volltext nicht online.

Kähler, C. and Stanislas, M. and Eckelmann, H . (2001) Investigation of near wall Turbulence using Multiplane Stereo PIV. In: CD ROM Proceedings, Proceedings, 1-. 4th International Symposium on Particle Image Velocimetry, Göttingen, Germany, September 17-19, 2001. Volltext nicht online.

Kähler, Christian and Sammler, Bernd and Kompenhans, Jürgen (2002) Generation and control of tracer particles for optical velocity measurements in air. In: Lasermethoden in der Strömungsmesstechnik, Tagungsband, 49.1-49.6. Universitätsdruckerei Rostock 866-02. Lasermethoden in der Strömungsmesstechnik,, 10. - 12. September 2002, Rostock. ISBN 3-86009-233-2. Volltext nicht online.

Körner, H. (2001) Aeroacoustic Problems of Fixed Wing Aircraft. Vortrag an den Universitäten NPU, Xian und BUAA, Peking (vrc), April 2001. Volltext nicht online.

Körner, H. (2001) Aerodynamics of Aircraft Components. Vortrag an den Universitäten NPU, Xian und BUAA, Peking (vrc), April 2001. Volltext nicht online.

Körner, H. (2001) Progress in CFD. Vortrag an den Universitäten NPU, Xian und BUAA, Peking (vrc), April 2001.. Volltext nicht online.

Körner, H. (2001) Numerical Methods for the Design of Aircraft at DLR. NAL-Symposium on Numerical Methods, Tokio (ja), Juni 2001.. Volltext nicht online.

Körner, H. (2001) Aerodynamic Investigation of Engine Integration and Tailplane Integration for Regional Aircraft. 2nd HTD Forum, Peking (vrc), Oktober 2001.. Volltext nicht online.

L

Laflin, K. and Klausmeyer, S. and Zickuhr, T. and Vassberg, J. and Wahls, R. and Morrison, J. and Brodersen, O. and Rakowitz, M. and Tinoco, and Godard, J.-L. (2004) Summary of Data from the Second AIAA CFD Drag Prediction Workshop. 42nd Aerospace Sciences Meeting, Reno (usa), 05.-08.01.2004. Volltext nicht online.

Laflin, Kelly and Klausmeyer, Steven and Zickuhr, Tom and Vassberg, John and Wahls, Richard and Morrison, Joseph and Brodersen, Olaf and Rakowitz, Mark and Tinoco, Edward and Godard, Jean-Luc (2005) Data Summary from Second AIAA Computational Fluid Dynamics Drag Prediction Workshop. Journal of Aircraft, 42 (5), pp. 1165-1178. AIAA. ISSN 0021-8669. Volltext nicht online.

Laflin, Kelly and Klausmeyer, Steven and Zickuhr, Tom and Vassberg, John and Wahls, Richard and Morrison, Joseph and Brodersen, Olaf and Rakowitz, Mark and Tinoco, Edward and Godard, Jean-Luc (2005) Results from the Second AIAA Computational Fluid Dynamics Drag Prediction Workshop. In: 2005 East West High Speed Flow Field Conference, pp. 286-297. International Aviation Group, Beijing, China. 2005 East West High Speed Flow Field Conference, 2005-10-19 - 2005-10-22, Beijing, (CHina). Volltext nicht online.

Le Chuiton, F. (2002) Actuator Disc Modelling for Helicopter Rotors. 28th European Rotorcraft Forum, 2002-09-16 - 2002-09-20, Bristol, UK. Volltext nicht online.

Le Chuiton, F. (2002) On the Non-Dimensionalisation of the Navier-Stokes Equations. On its Implementation in FLOWer. Related User-Guide. DLR-Interner Bericht. IB 124-2002/5. 47 S. Volltext nicht online.

Le Chuiton, F. (2004) Actuator disc modelling for helicopter rotors. Aerospace Science and Technology, 8 (4), pp. 285-297. Volltext nicht online.

Le Chuiton, F. (2004) On the non-dimensionalisation of the Navier-Stokes equations. Related FLOWer user-guide. (1st revision). DLR-Interner Bericht. 124-2004/10. 50 S. Volltext nicht online.

Le Chuiton, F. (2004) Chimera simulation of a complete helicopter with rotors as actuator discs. 14th DGLR STAB Symposium, Bremen (de), 16.-18.11.2004. Volltext nicht online.

Le Chuiton, F. (2005) Quasi-steady simulation of a complete EC-145 helicopter: fuselage + main/tail actuator discs + engines. 31st European Rotorcraft Forum, 2005-09-13 - 2005-09-15, Firenze, Italy. Volltext nicht online.

Leblanc, S. and Le Duc, A. (2005) The unstable spectrum of swirling gas flows. Journal of Fluid Mechanics, 537, pp. 433-442. Volltext nicht online.

Lefebvre, T. and Beaumier, P. and Canard-Caruana, S. and Pisoni, A. and Pagano, A. and Sorrentino, A. and van der Wall, Berend G. and Yin, J. and Arzoumanian, C. and Voutsinas, S. and Hermans, C. (2004) Aerodynamic and aero-acoustic optimization of modern tilt-rotor blades within the ADYN project. 4th European Congress on Computational Methods in Applied Sciences and Engineering, 2004-07-24 - 2004-07-28, Jyväskylä (fi). Volltext nicht online.

Lenfers, Carsten and Beck, Nils and Bauer, Marc (2014) Propeller and Active High Lift Wing Interaction in Experiement and Simulation. 19. DGLR-Fachsymposium der STAB, 04.-05.11.2014, München, Deutschland. Volltext nicht frei.

Leopold, F. and Richard, H. and Raffel, M. and Christnacher, F. (2002) Experimental Investigations of the Interaction of Supersonic Wing-Tip Vortices with a Normal Shock. In: Book of Abstracts, paper No. 4.2 ; (auch ISL-Publication PU 630/2002). 11th Intern. Symposium on Applications of Laser Techniques in Fluid Mechanics, Lisbon, Portugal, July 8-11, 2002. Volltext nicht online.

Lier, Max and Krenik, Alex and Kunze, Philipp and Kohlgrüber, Dieter and Schwinn, Dominik and Lützenberger, Marius (2015) A Toolbox for Rotorcraft Preliminary Design. AHS 71st Annual Forum, 5.-7. Mai 2015, Virginia Beach, USA.

Liersch, Carsten M. (2001) Entwicklung von Schnittstellen zur Integration des Strukturanalyse und -dimensionierungstools SAM in das PrADO des DLR Braunschweig. DLR-Interner Bericht. 129-2001/21. 88 S. Volltext nicht online.

Liersch, Carsten M. and Hepperle, M. (2003) Weiterentwicklung eines Traglinienverfahrens und Einbindung in das Vorentwurfsverfahren PrADO. STAB-Workshop, Göttingen (de), 04.-05.11.2003. Volltext nicht online.

Lim, J.W. and Tung, C. and Yu, Y.H. and Burley, C.L. and Brooks, T. and Boyd, D. and van der Wall, Berend G. and Schneider, O. and Richard, H. and Raffel, M. and Beaumier, P. and Bailly, J. and Delrieux, Y. and Pengel, K. and Mercker, E. (2003) HART II: Prediction of Blade-Vortex Interaction Loading. In: 29th European Rotorcraft Forum Proceedings. 29th European Rotorcraft Forum, Friedrichshafen, 16-18 September 2003, 2003-09-16 - 2003-09-18, Friedrichshafen, Germany. Volltext nicht online.

Lindblad, I. and Wallin, S. and Johansson, A. and Friedrich, R. and Lechner, R. and Krogmann, P. and Schülein, E. and Courty, J.-C. and Ravachol, M. and Giordano, D. (1998) Method for High Speed Turbulent Separated Flows with Experimental Verification. In: AIAA -98-2547, 12p.-. 29th AIAA Fluid Dynamics Conference, June 15-18, 1998/Albuquerque, NM. Volltext nicht online.

Longo, J.M.A. (2001) German Participation in the Aerothermodynamic Design of the Experimental Vehicle X-38. XII. Congress on Numerical Methods and their Applications, Cordoba (ar),30.10.-02.11.2001. Volltext nicht online.

Longo, J.M.A. (2001) Aerothermodynamics - A Critical Review -. 4th Symposium on Aerothermodynamics for Space Vehicles, Capua (it), 14.-18.10.2001. Volltext nicht online.

Longo, J.M.A. (2001) Aerothermodynamics - A critical review at DLR. 4th European Symposium on Aerothermodynamics for Space Vehicles, Capua (it), 15.-18.10.2001. ISBN 92-9092-789-5. Volltext nicht online.

Longo, J.M.A. (2001) Aerothermodynamics - A critical review at DLR. 4th European Symposium on Aerothermodynamics for Space Vehicles, Capua (it), 15.-18.10.2001. Volltext nicht online.

Longo, J.M.A. (2003) Aerothermodynamics - A critical review at DLR. Aerospace Science and Technology, 7 (6), pp. 429-438. Volltext nicht online.

Longo, J.M.A. (2004) Modelling of Hypersonic Flow Phenomena. RTO/AVT/VKI Lecture Series: "Critical Technologies for Hypersonic Vehicle Development Technology", Brüssel (b), 10.-14.05.2004. Volltext nicht online.

Longo, J.M.A. (2004) SHEFEX - A Low Cost Highly Efficient Flight Experiment. 5th European Symposium on Aerothermodynamics of Space Vehicles, Köln (de), 08.-11.11.2004. Volltext nicht online.

Longo, J.M.A. and Püttmann, N. (2004) The DLR Sharp Edge Flight Experiment SHEFEX. Deutscher Luft- und Raumfahrtkongress 2004, Dresden (de), 20.-23.09.2004. Volltext nicht online.

Longo, J.M.A. and Bozic, O. and Behrens, J. and Lehmann, P. (2005) Future Prospects for Hypersonic Flight Test For University Students. In: RTO AVT VKI Lecture Series. Lecture Series "Flight Experiments for Hypersonic Vehicle Development", 2005-24-10, Brüssel, Belgien.

Longo, J.M.A. and Eggers, Th. and Gülhan, A. and Turner, J. and Weihs, H. (2005) Designing Flight Experiments for Hypersonic Flow Physics. In: RTO AVT VKI Lecture Series. Lecture Series "Flight Experiments for Hypersonic Vehicle Development", 2005-24-10, Brüssel, Belgien.

Longo, J.M.A. and Lüdeke, H. and Kordulla, W. and Molina, R. (2005) Extrapolating Aero Data from a Demonstrator to an Operational Vehicle. In: 4th International Symposium Atmospheric Reentry Vehicles & Systems Proceedings. 4th International Symposium Atmospheric Reentry Vehicles & Systems, [2005-03-21 - 2005-03-23], Arcachon, Frankreich.

Longo, Jose Maria and Eggers, Thino and Turner, John and Jung, W. and Hörschgen, Marcus and Stamminger, A. and Gülhan, Ali and Siebe, F. and Requardt, G. and Laux, Torsten and Reimer, T. and Weihs, Hendrik (2006) The Shefex Flight Experiment - Pathfinder Experiment for a Sky Based Test Facility. DGLR Jahrbuch 2006, I & II. ISSN 0700-4083.

Loose, Sigfried and Lauterbach, Andreas and Algermissen, Stephan and Heckmann, Andreas (2011) Activities in acoustics. In: RTR Special - Next Generation Train Railway Technical Review Special. Eurailpress. pp. 51-60. ISBN 1869-7801. ISSN 978 3 7771 0435 5.

Lu, M. (2001) Widerstandsverminderung durch Ventilation stumpfer Körper bei höheren Reynoldszahlen. DLR-Forschungsbericht. 2001-28. Dissertation. 142 S. Volltext nicht online.

Lube, Gerd and Knopp, Tobias and Gritzki, R. and Rösler, M. and Seifert, J. (2008) Application of domain decomposition methods to indoor air flow simulation. International Journal of Computer Mathematics (85), pp. 1551-1562. Volltext nicht online.

Lube, Gerd and Knopp, Tobias and Rapin, G. and Gritzki, R. and Rösler, M. (2008) Stabilized finite element methods to predict ventilation efficiency and thermal comfort in buildings. International Journal for Numerical Methods in Fluids (57), pp. 1269-1290. Volltext nicht online.

Lummer, M. and Delfs, J. and Lauke, T. (2002) CAA Calculations of Vortex Trailing-Edge Interactions Using Nonlinear Disturbance Equations. 3rd Aeroacoustics Workshop (SWING), Stuttgart (de), 26.-27.09.2002. Volltext nicht online.

Lummer, M. and Delfs, J. and Lauke, T. (2002) Simulation of Sound Generation by Vortices passing the Trailing Edge of Airfoils. 8th AIAA/CEAS Aeroacoustics Conference, Breckenridge (usa), 17.-19.06.2002. ISBN 1-56347-533-2 (CD). Volltext nicht online.

Lummer, M. and Delfs, J.W. and Lauke, T. (2004) CAA-Simulation of Flap Noise Generation using Perturbation Equations. 4th Aeroacoustics Workshop in connection with the national project SWING+ (Simulation of Wing-flow Noise Generation), Aachen (de), 26.-27.02.2004. Volltext nicht online.

Lüdeke, H. (2001) Computation of Görtler Vortices in Separated Hypersonic Flows. In: Computational Fluid Dynamics 2000, pp. 171-176. Springer. 1st International Conference on Computational Fluid Dynamics, Kyoto (ja), 10.-14.07.2000. ISBN 3-540-41459-2. Volltext nicht online.

Lüdeke, H. (2003) Das Erprobungsträgersystem Phoenix als Testfall für den TAU-Code im Unterschall. DLR-Interner Bericht. 124-2003/16. 35 S. Volltext nicht online.

Lüdeke, H. (2001) CRV-Early Tasks, Interim Report CFD Analysis. Other. CRV-DLRG-TN-AD B003. ESA. 9 S. Volltext nicht online.

Lüdeke, H. and Filimon, A. (2004) Investigation of Transient Flow Phenomena at the Ariane-5 Propulsion System during Ascent. 5th European Symposium on Aerothermodynamics for Space Vehicles, Köln (de), 08.11.-11.11.2004. Volltext nicht online.

Lüdeke, H. and Filimon, A. (2004) Time Accurate Simulation of Turbulent Nozzle Flow by the DLR TAU-Code. (In Press) Volltext nicht online.

Lüdeke, H. and Longo, J.M.A. (2004) Contribution of DLR to the Aerodynamic Data Base of the SPHYNX Re-entry vehicle. DLR-Interner Bericht. 124-2004/01. 35 S. Volltext nicht online.

Lüdeke, H. and Radespiel, R. and Schülein, E. (2004) Simulation of streamwise vortices at the flaps of reentry vehicles. Aerospace Science and Technology, 8 (8), pp. 703-714. Volltext nicht online.

Lüdeke, H. and Radespiel, R. and Schülein, E. (2004) Simulation of Streamwise Vortices at the Flaps of Re-entry Vehicles. In: CD. 42nd AIAA Aerospace Science Meeting and Exhibit, Reno (usa), 05.-08.01.2004. Volltext nicht online.

Lüdeke, H. and Schülein, E. (2002) Simulation of Streamwise Vortices on Turbulent Hypersonic Ramps. 2nd International Conference on Computational Fluid Dynamics, Sydney (aus), 15.-19.07.2002. Volltext nicht online.

Lüdeke, H. and Schülein, E. (2004) Investigation of Streamwise Vortices at Deflected Flaps of Re-entry Vehicles. RTO Conference "Enhancement of NATO Military Flight Vehicle Performance by Management of Interacting Boundary Layer Transition and Separation" , Prag (cz), 04.-08.10.2004. Volltext nicht online.

Löser, Thomas and Vicroy, Dan D. and Schütte, Andreas (2009) SACCON STATIC WIND TUNNEL TESTS AT DNW-NWB AND 14ft × 22ft NASA LARC. NATO RTO - Research and Technology Organisation. [Other] Volltext nicht online.

Lübker, Jannis and Alder, Marko and Fink, Helena (2016) DESIGN AND INITIAL RUN OF A NEW TEST SETUP FOR INVESTIGATIONS ON THE AEROELASTIC STABILITY OF PANELS IN THE TRANSONIC MACH DOMAIN. ECSSMET 2016, 27.-30. Sept. 2016, Toulouse, Frankreich.

Lüdeke, H. and Sandham, N.D. (2009) An Extended Numerical Study of Mach 6 Boundary Layer Stabilization by Means of a Porous Surface. DLR-Interner Bericht. DLR-IB 124-2009/909. DLR. 28 S. Volltext nicht frei.

M

Ma, Fei and Brezillon, Joel and Abu-Zurayk, Mohammad and Ilic, Caslav (2011) Drag Reduction of a 2D Airfoil with Constraints on Lift and Pressure Distribution using Adjoint Approach. 15. STAB-Workshop, 9-10 Nov. 2011, Göttingen, Deustchland.

Mack, A. and Emran, M. and Schäfer, R. (2004) Fluid-Structure Interaction on the Leeside Flow of a Generic Body-Flap Model. 14th DGLR/STAB Fach-Symposium, Bremen (de), 16.-18.11.2004. Volltext nicht online.

Mack, A. and Hannemann, V. (2002) Validation of the Unstructured DLR-TAU-Code for Hypersonic Flows. 32nd AIAA Fluid Dynamics Conference, St. Louis (usa), 24.-27.06.2002. Volltext nicht online.

Mack, A. and Schäfer, R. (2004) Thermal Coupling Effects of a Generic Body-Flap Model. 5th European Symposium on Aerothermodynamics for Space Vehicles, Köln (de), 08.-11.11.2004. Volltext nicht online.

Mack, A. and Schäfer, R. and Esser, B. and Gülhan, A. (2004) Fluid Structure Interaction of a Hypersonic Generic Body-Flap Model. 3rd International Conference on Computational Fluid Dynamics, ICCFD, Toronto (can), 12.-16.06.2004. Volltext nicht online.

Mack, A. and Schäfer, R. and Gülhan, A. and Esser, B. (2002) IMENS Flowfield Tropology changes due to Fluid-Structure Interaction in Hypersonic Flow using ANSYS and TAU. 13. DGLR-Fach Symposium, München (de), 12.-14.11.2002. Volltext nicht online.

Mack, Andreas and Schäfer, Roger (2005) Fluid Structure Interaction on a Generic Body-Flap Model in Hypersonic Flow. Journal of Spacecraft and Rockets, 42 (5), pp. 769-779. ISSN 0022-4650. Volltext nicht online.

Madrane, A. and Raichle, A. and Stürmer, A. (2004) Parallel Implementation of a Dynamic Overset Unstructured Grid Approach. In: CD, Vortrag Nr. 14. ECCOMAS 2004, Jyväskylä (fi), 24.-28.07.2004. Volltext nicht online.

Mai, Holger and Dietz, Guido and Geissler, Wolfgang and Richter, Kai and Bosbach, Johannes and Richard, Hugues and de Groot, Klaus (2008) Dynamic stall control by leading edge vortex generators. Journal of the American Helicopter Society, 53 (1), pp. 26-36. ISSN 0002-8711. Volltext nicht online.

Mai, Holger and Dietz, Guido and Geißler, Wolfgang and Richter, Kai and Bosbach, Johannes and Richard, Hughes and de Groot, Klaus (2006) Dynamic Stall Control by Leading Edge Vortex Generators. In: Proceedings of the 62nd Annual Forum and Technology Display, 62. American Helicopter Society 62nd Annual Forum and Technology Display, 2006-05-09 - 2006-05-11, Phoenix, AZ (USA). ISSN 1552-2938. Volltext nicht online.

Martinez Schramm, Jan and Barth, Tarik and Wagner, Alexander and Hannemann, Klaus (2011) Post Flight Analysis of SHEFEX I: Shock Tunnel Testing and Related CFD Analysis. 7th European Symposium on Aerothermodynamics for Space Vehicles , 9. Mai - 12. Mai 2011, Brugge, Belgien. Volltext nicht online.

Meier, G.E.A. and Rein, M. (1998) A new type of hypersonic wind tunnels. IX International Conference on the Methods of Aerophysical Research, Novosibirsk, Russia, 29 June - 3 July 1998. Volltext nicht online.

Melber, S. (2002) 3D RANS-Simulations for High-Lift Transport Aircraft Configurations with Engines. DLR-Interner Bericht. IB 124-2002/27. Volltext nicht online.

Melber, S. (2002) Wirbelkorrektur für Ein- und Zweigleichungs-Turbulenzmodelle und Implementation für das Spalart-Allmaras Turbulenzmodell in den Strömungslöser DLR-TAU. DLR-Interner Bericht. IB 124-2002/17. Volltext nicht online.

Melber, S. and Heinrich, R. (2004) Low Mach Number Preconditioning for the DLR-TAU Code and Application to High-Lift Flows. In: New Results in Numerical and Experimental Fluid Mechanics IV, Vol. 87, pp. 390-397. Springer Verlag, Berlin Heidelberg, New York. 13th STAB/DGLR Symposium, München (de), 12.-14.11.2002. ISBN 3-540-20258-7. Volltext nicht online.

Melber, S. and Wild, J. and Rudnik, R. (2002) Overview about the HLRS Project "Numerical High Lift Research" (NHLRes). DLR-Interner Bericht. IB 124-2002/15. 15 S. Volltext nicht online.

Melber, S. and Wild, J. and Rudnik, R. (2002) Overview about the HLRS Project "Numerical High Lift Research" (NHLRes). In: High Performance Computing in Science and Engineering 2002 Springer Verlag Berlin Heidelberg New York. pp. 406-421. ISBN 3-540-43860-2. Volltext nicht online.

Melber-Wilkending, S. (2003) Modifikation der Triebwerksrandbedingung und Einführung einer Windkanalrandbedingung in TAU. DLR-Interner Bericht. IB 124-2003/7. 69 S. Volltext nicht online.

Melber-Wilkending, S. (2004) Aerodynamic Analysis of Jet-Blast using CFD considering as example a Hangar and an AIRBUS A380 configuration. 14th AG STAB/DGLR Symposium, Bremen (de), 16.-18.11.2004. Volltext nicht online.

Melber-Wilkending, S. (2004) Aerodynamische Untersuchungen von Strömungen kleiner Mach- und Reynoldszahl unter Berücksichtigung der Transition am Beispiel eines Segelflugzeuges. Symposium für Segelflugzeugentwicklung, Stuttgart (de), 18.-19.11.2004. Volltext nicht online.

Melber-Wilkending, S. (2004) Aerodynamische Untersuchungen zu den Auswirkungen der Strahlinteraktion am Beispiel eines Hangars und einer AIRBUS A380 Konfiguration mittels CFD-Verfahren. DGLR-Symposium "Nachbar Flughafen", Bremen (de), 25.-27.10.2004. Volltext nicht online.

Melber-Wilkending, S. and Brodersen, O. and Kallinderis, Y. and Wilhelm, R. and Sutcliffe, M. and Wild, J. and Ronzheimer, A. (2005) Hybrid unstructured Grid Generation in MEGAFLOW. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 3-24. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6. Volltext nicht online.

Melber-Wilkending, S. and Heinrich, R. (2002) Implementierung einer Präkonditionierungstechnik für Strömungen kleiner Mach-Zahlen im DLR TAU-Code und Anwendung im Hochauftrieb. 13. DGLR-Fachsymposium der AG STAB 2002, München (de), 12.-14.11.2002. Volltext nicht online.

Melber-Wilkending, S. and Rudnik, R. and Ronzheimer, A. and Schwarz, T. (2005) Verification of MEGAFLOW-Software for High Lift Applications. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 163-178. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6. Volltext nicht online.

Melber-Wilkending, S. and Schrauf, G. and Rakowitz, M. (2004) Aerodynamic Analysis of Flows with Low Mach- and Reynolds-Number under Consideration and Forecast of Transition on the Example of a Glider. 14th AG STAB/DGLR Symposium, Bremen (de), 16.-18.11.2004. Volltext nicht online.

Melber-Wilkending, S. and Stumpf, E. and Stürmer, A. and Wild, J. and Rudnik, R. (2005) Numerical High Lift Research II/III. In: High Performance Computing in Science and Engineering '04, pp. 237-259. Springer Verlag, Berlin Heidelberg New York. HLRS Workshop, Stuttgart (de), 04.-06.10.2004. ISBN 3-540-22943-4. Volltext nicht online.

Melber-Wilkending, S. and Stumpf, E. and Wild, J. and Rudnik, R. (2003) Overview about the HLRS Project "Numerical High Lift Research II" (NHLRes II). DLR-Interner Bericht. IB 124-2003/17. 23 S. Volltext nicht online.

Melber-Wilkending, S. and Stumpf, E. and Wild, J. and Rudnik, R. (2003) Overview about the HLRS Project "Numerical High Lift Research II" (NHLRes II). In: High Performance Computing in Science and Engineering 2003 Springer Verlag, Berlin Heidelberg New York. ISBN 3-540-40850-9. Volltext nicht online.

Melber-Wilkending, S. and Wilhelm, R. and Geyr, H. von (2004) RANS Solution for a Complex High-Lift Configuration of a Transport Aircraft with Engine Including Improved Resolution of the Nearfield. 22nd AIAA Applied Aerodynamics Conference, Rhode Island (usa), 16.-19.08.2004. Volltext nicht online.

Melber-Wilkending, Stefan and Heidebrecht, Alexander and Wichmann, Georg (2006) A new approach in CFD supported Wind Tunnel testing. In: 25th International Congress of the Aeronautical Sciences, ICAS, Hamburg, 3.-8. September, 2006. 25th International Congress of the Aeronautical Sciences, ICAS, Hamburg, 3.-8. September, 2006, 2006-03-09 - 2006-08-09, Hamburg. (Submitted) Volltext nicht online.

Melber-Wilkending, Stefan and Wichmann, Georg (2006) Project ForMEx - A new CFD approach for transposition of Wind Tunnel data towards Flight Conditions. In: 15th AG STAB/DGLR Symposium Darmstadt, 29.11 - 1.12.2006. 15th AG STAB/DGLR, 29.11 - 1.12.2006, Darmstadt. (Submitted) Volltext nicht online.

Meyer, J. and Groot, K. de and Krückeberg, C.-P. and Weddig, T. and Sitzmann, M. and Horstmann, K.H. (2003) System Layout and Instrumentation of a Laminar Flow System for the DLR Do 228 Test Vehicle. CEAS 2003 Conference, London (uk), 10.-12.06.2003. Volltext nicht online.

Monnier, J.C.,, and Gillot, A.,, and Vollmers, H. and Schröder, A. and Lozier, J.L.,, (2002) Caractérisation de Sillage d'Avion de Transport par Vélocimétrie par Images de Particules (PIV). In: 8ème Congrès Francophone de Vélocimétrie Laser, pp. 219-220. 8ème Congrès Francophone de Vélocimétrie Laser, Orsay, France, 17.-10. Septembre 2002. Volltext nicht online.

Mori, H. and Dankert, C. and Niimi, T. (2001) Resonantly Enhanced Multiphoton Ionization for Analyses of rarefied Supersonic H2 + N2 Flows. DLR-Interner Bericht. 223- 2001 A 09. 15 S. Volltext nicht online.

N

Nassif, S. and Lüdeke, H. (2001) Investigation of Görtler Vortices on Hypersonic Ramp Configurations. DLR-Interner Bericht. 129-2001/3. 49 S. Volltext nicht online.

Neeb, Dominik and Gülhan, Ali and Cosson, Emmanuel and Ameziane, Rachida and Binetti, Paolo and Walloschek, Thomas (2008) An Experimental Study on Aerothermal Heating of the IXV Configuration During Reentry. In: ESA Special Publication. Sixth European Symposium on Aerothermodynamics for Space Vehicles, 2008-11-03 - 2008-11-05, Versailles (Frankreich). Volltext nicht online.

Neumann, J. and Einarsson, G.Ó. and Schütte, A. (2005) Multidisziplinäre Simulation eines rollenden, generischen Deltaflügels - Kopplung von Aerodynamik, Flugmechanik und Strukturdynamik. In: Proceedings. Deutscher Luft- und Raumfahrtkongress 2005, Friedrichshafen, 26.-29. September 2005, 2005-09-26 - 2005-09-29, Friedrichshafen, Deutschland (Europa).

Noeding, P. and Bregman, E. and Longo, J.M.A. (2005) Assessment of Aerothermodynamic Analysis Methods with Regard to the Planned SHEFEX Flight Experiment. In: 4th International Symposium Atmospheric Reentry Vehicles & Systems Proceedings. 4th International Symposium Atmospheric Reentry Vehicles & Systems, [2005-03-21 - 2005-03-23], Arcachon, Frankreich.

Noll, B. and Kessler, R. and Lehmann, B. and Rachner, M. and Frank, P. and Schmitz, G. and Geigle, K.-P. and Meier, W. and Schütz, H. and Forkert, T. and Aigner, M. (2002) Ergebnisse des Projekts "Brennkammermodellierung" (BKM II). DLR-Forschungsbericht, Project Report. 2002-16. 83 S. Volltext nicht online.

Novelli, P. and Duveau, P. and Eggers, T. and Haupt, M. (2001) JAPHAR - Etude preliminaire d'un Vehicule Experimental pur la Demonstration en vol du Bilan Propulsif du Statimixte. 37 int. colloque d'Aérodynamique Appliquée "Aérodynamique et Propulsion des Véhicules à grande vitesse", Arcachon (fr), 28.-30.03.2001. Volltext nicht online.

O

Opitz, K. (2002) Numerische Untersuchung zweidimensionaler, laminar-turbulenter Profilumströmungen und Auswirkung der Transition auf integrale Kraftbeiwerte. DLR-Interner Bericht. IB 124-2002/9. 130 S. Volltext nicht online.

Orlt, M. (2002) Entwicklungen am TAU-Code im Rahmen von AEROSUM. Institutskolloquium, 2002-05-17, DLR Göttingen. Volltext nicht online.

Ortmann, J. and Wild, J. (2006) Effect of Noise Reducing Modifications of the Slat on Aerodynamic Properties of the High-Lift System. Springer Verlag. DGLR/STAB Symposium, Bremen (de), 16.-18.11.2004, 2004-11-16 - 2004-11-18, Bremen (de). ISBN 3-540-33286-3. Volltext nicht online.

Otter, D. (2001) Optische berührungslose Positionserfassung eines bewegten Deltamodells im Windkanal. DLR-Interner Bericht. 223-2001 A04. 81 S. Volltext nicht online.

P

P.C. Palma, and W.H. Beck, (2001) Diode-Laser Absorption Spectroscopy of Rubidium in Hypersonic Flows. DLR-Interner Bericht. DLR-IB 223-01 A13. 86 S. Volltext nicht online.

Pahlke, K. and Costes, M. and D'Alascio, A. and Castellin, C. and Altmikus, A. (2005) Overview of Results Obtained During the 6-Year French-German Project. European Rotorcraft Forum, Florenz (it), 13.-16.09.2005. Volltext nicht online.

Pahlke, K. and van der Wall, Berend G. (2001) Calculation of Multibladed Rotors in High-Speed Forward Flight with Weak Fluid-Structure-Coupling. In: 27th European Rotorcraft Forum Proceedings, 27.1-27.11. 27th European Rotorcraft Forum, Moscow (Russia), 11-14 September 2001. Volltext nicht online.

Pahlke, K. and van der Wall, Berend G. (2001) Calculation of Multibladed Rotors in High-Speed Forward Flight Accounting for Elastic Blade Deformations. In: Proceedings of the CEAS Conference on Multidisciplinary Aircraft Design and Optimization, pp. 259-270. DGLR-Deutsche Gesellschaft für Luft- und Raumfahrt, Lilienthal-Oberth e.V., Godesberger Allee 70, 53175 Bonn. CEAS Conference on Multidisciplinary Aircraft Design and Optimization, Cologne (de), 25.-26.06.2001. ISBN 3-932182-21-9. Volltext nicht online.

Pahlke, K. and van der Wall, Berend G. (2002) Progress in Weak Fluid-Structure-Coupling for Multibladed Rotors in High-Speed forward Flight. In: 28th European Rotorcraft Forum Proceedings, 67.1-67.13. 28th European Rotorcraft Forum, Bristol (uk), 17-20 September 2002. Volltext nicht online.

Pahlke, K. and van der Wall, Berend G. (2002) Berechnung der Umströmung von Mehrblattrotoren im schnellen Vorwärtsflug mit einer schwachen Fluid-Struktur-Kopplung. Other. ISBN-Nr. 3-18-091682-6. VDI. 20 S. Volltext nicht online.

Pahlke, K. and van der Wall, Berend G. (2003) Chimera Simulations of Multibladed Rotors in High-Speed Forward Flight with Weak Fluid-Structure-Coupling. In: 29th European Rotorcraft Forum (CD), 63.1-63.13. 29th European Rotorcraft Forum, Friedrichshafen (de), 16.-18.09.2003. ISBN CD. Volltext nicht online.

Pahlke, K. and van der Wall, Berend G. (2005) Chimera Simulations of Multibladed Rotors in High-Speed Forward Flight with Weak Fluid-Structure-Coupling. Aerospace Science and Technology, 9 (5), pp. 379-389. Volltext nicht online.

Pahlke, Klausdieter (2010) GARTEUR Helicopter Cooperative Research. In: Proceedings of 36th European Rotorcraft Forum, pp. 1-10. 36th European Rotorcraft Forum, 7.-9. Sept. 2010, Paris, Frankreich.

Pahlke, Klausdieter and Demaret, Blanche (2012) New Technologies for Efficient Rotorcraft. airtec GmbH & Co. KG. 3rd International Conference HELI WORLD 2011, 3.-4. Nov. 2011, Frankfurt, Deutschland. ISBN 978-3-942939-02-7. Volltext nicht online.

Pahlke, Klausdieter (2011) New Technologies for Green Rotorcraft. The Korean Association of the Global R&D Centers (GRDC). GRDC Symposium 2011, 15. Nov. 2011, Seoul, Korea.

Pallek, D. (2004) Measurement of wing deformation in ETW by means of Moiré Interferometry. DLR/ONERA - Annex II Meeting, DLR, Köln, 6. -7. April 2004. Volltext nicht online.

Pallek, D. and Bütefisch, K.A. and Quest, J. and Strudthoff, W. (2003) Model Deformation Measurement in ETW using the Moiré Technique. In: ICIASF 2003 Record, Tagungsband, pp. 110-114. IEEE. ICIASF'03, 2003-08-25 - 2003-08-29, Göttingen (Deutschland). ISBN 0-7803-8149-1. Volltext nicht online.

Peltzer, Inken and Nitsche, Wolfgang and Seitz, Arne and Weismüller, Michael and Tropea, Cameron (2007) In-Flight Investigations on Tollmien-Schlichting Waves and Receptivity on Laminar Airfoils. ERCOFTAC Bulletin, 74. Volltext nicht online.

Pidd, Mike and Dummel, Andreas and Falchero, Daniele and Prospathopoulos, John and Visingardi, Antonio and Voutsinas, Spyros G and Yin, Jianping (2006) VALIDATION OF AEROACOUSTIC PREDICTIONS USING THE HELINOVI DATABASE. In: European Rotorcraft Forum. 32st ERF 2006, AC03, 2006-12-09 - 2006-14-09, Maastricht (NL). Volltext nicht online.

Pott-Pollenske, M. (2003) KATO-Passagier-Bestandsaufnahme und Arbeitsplanung für 2004. DLR-Interner Bericht. 124-2003/45. 10 S. Volltext nicht online.

Pott-Pollenske, M. and Alvarez-Gonzales, J. and Dobrzynski, W. (2003) Effect of Slat Gap on Farfield Radiated Noise and Correlation with Local Flow Characteristics. 9th AIAA/CEAS Aeroacoustics Conference, Hilton Head (usa), 12.-14.05.2003. Volltext nicht online.

Pott-Pollenske, M. and Dobrzynski, W. (2003) Assessment of acoustic quality of differently designed control devices. DLR-Interner Bericht. 124-03/39. 65 S. Volltext nicht online.

Pott-Pollenske, M. and Dobrzynski, W. and Buchholz, H. and Gehlhar, B. and Walle, F. (2002) Validation of a Semiempirical Airframe Noise Prediction Method through Dedicated A319 Flyover Noise Measurements. 8th AIAA/CEAS Aeroacoustics Conference; Breckenridge (usa), 17.-19.06.2002. Volltext nicht online.

Pott-Pollenske, Stephan-Michael and Guder, Carolin (2008) Handbuch zur Lärmmessung - ICAO Annex 16, Chapter 6 -. DLR-Forschungsbericht. DLR-IB 124-2008/906. 81 S. Volltext nicht online.

Pott-Pollenske, Stephan-Michael and Guder, Carolin (2008) Manual for Aircraft Exterior Noise Measurements - ICAO Annex 16, Chapter 6 -. DLR-Interner Bericht. DLR-IB 124-2008/907. 79 S. Volltext nicht online.

Pott-Pollenske, Stephan-Michael and Guder, Carolin (2008) Handbuch zur Lärmmessung - ICAO Annex 16, Chapter 10. DLR-Interner Bericht. DLR-IB 124-2008/908. 83 S. Volltext nicht online.

Pott-Pollenske, Stephan-Michael and Wild, Jochen (2008) Entwicklung und Validierung eines Verfahrens zur Beurteilung der Schallabstrahlung von Hochauftriebssystemen. Deutsche Jahrestagung für Akustik 2008, 2008-03-11 - 2008-03-13, Dresden.

Psolla-Bress, H. and Haselmeyer, H. and Heddergott, A. and Höhler, G. and Holst, H. (2001) HIGH-ROLL RATE EXPERIMENTS ON A DELTA WING IN TRANSONIC FLOW. In: ICIASF 2001 RECORD, 12.1. ICIASF, Cleveland, Ohio, August 27-30, 2001. Volltext nicht online.

Psolla-Bress, H. and Haselmeyer, H. and Heddergott, A. and Höhler, G. and Jacobs, M. and Otter, D. and Sachs, W. and Schirmacher, R. (2002) Stationäre Kraft- und Druckverteilungsmessungen am AS-Modell im TWG. Project Report, DLR-Interner Bericht. 223 - 2001 - A 03. 286 S. Volltext nicht online.

Puffert-Meißner, W. and Wilhelm, R. (2002) Analysis of ALVAST Half-Model Investigations in the Low-Speed Wind Tunnels DNW-LST and DNW-NWB. DLR-Interner Bericht. IB 124-2002/28. Volltext nicht online.

Püttmann, N. and Longo, J.M.A. (2004) The Sharp Edge Flight Experiment SHEFEX - The ideas behind and status of the project, IAC-04-V.6.08. 55th Congress of International Astronautical Federation, Vancouver (can), 04.-08.10.2004. Volltext nicht online.

Q

Quast, A. (2001) Maßnahmen zur Destabilisierung von Flugzeug-Wirbeln. DLR-Interner Bericht. 129-2001/8. Volltext nicht online.

Quast, A. (2002) Thermographie. Vorlesung in der Berufsakademie Mannheim, Mannheim (de), 16.05.2002. Volltext nicht online.

Quast, A. (2002) Parameterstudie und Vorentwurf für ein hochfliegendes Aufklärungsflugzeug. 10. Fortschrittspräsentation EADS-M, München (de), 14.08.2002. Volltext nicht online.

R

Raddatz, J. and Fassbender, J.K. (2005) Block Structured Navier-Stokes Solver FLOWer. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 27-44. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6. Volltext nicht online.

Raddatz, Jochen (2016) Numerical Assessment of the airfoils EDI-M109 and EDI-M112 by 3D CFD calculations of the 5-bladed INROS rotor in Hover and Forward Flight. DLR-Interner Bericht. DLR-EB-AS-BS-2016-902. Deutsches Zentrum für Luft- und Raumfahrt e.V.. 35 S. Volltext nicht online.

Radespiel, R. and Lüdeke, H. and Brück, S. (2001) Computation of Transitional Reentry Flows over 3D Vehicles and Systems. 2nd International Symposium "Atmospheric Reentry Vehicles and Systems, Arcachon (fr), 26.-29.03.2001. Volltext nicht online.

Raffel, M. (2001) Optische Untersuchungen in technischen Strömungen unter besonderer Berücksichtigung eines Verfahrens zur Detektion von Dichtegradienten. In: - Habilitationsschrift. ISBN 3-89720-582-3. Volltext nicht online.

Raffel, Markus and Richard, Hugues and Agocs, Janos and Otter, Dirk and Mattner, Hartmut and Göhmann, Uwe (2001) Experimental aspects of PIV applied to a Bo 105 helicopter in hover-flight condition. 4th Intern. Symposium on Particle Image Velocimetry, 17. - 18. Sept. 2001, Göttingen, Germany.

Raffel, Markus and Richard, Hugues and Ehrenfried, Klaus and van der Wall, Berend G. and Burley, C. and Beaumier, P. and McAlister, K. and Pengel, Kurt (2004) Recording and evaluation methods of PIV investigations on a helicopter rotor model. Experiments in Fluids, 36 (1), pp. 146-156. Volltext nicht online.

Raffel, M.,, and Richard, H. (2002) Detection of Density Gradients at Helicopter Rotor Blades in Flight. In: New Results in Numerical and Experimental Fluid Mechanics III, Vol.77, pp. 426-431. Springer. 12th STAB/DGLR Symposium, Stuttgart, November 2000.. Volltext nicht online.

Raichle, A. (2004) Extension of the Unstructured TAU-Code for Rotating Flows. DGLR-STAB Symposium, Bremen (de), 16.-18.11.2004. Volltext nicht online.

Rakowitz, M. (2001) Grid Refinement Study with a UHCA Wing-Body Configuration using Richardson Extrapolation and Grid Convergence Index GCI. 12.DGLR/AG STAB Tagung, Stuttgart (de), 15.-17.11.2000. Volltext nicht online.

Rakowitz, M. (2003) Investigation of High-Lift System Variations on the A400M Sol. 86 (Status 5.2) Geometry using CFD. DLR-Interner Bericht. IB 124-2003/19. Volltext nicht online.

Rakowitz, M. (2003) "Euler and Navier-Stokes Computations on several A400M Sol. 76 (Status 5.1) Geometries". DLR-Interner Bericht. IB 124-2003/18. Volltext nicht online.

Rakowitz, M. (2003) "CFD Analysis of a Transport Aircraft with Propellers". RTO-Symposium AVT-100, Warschau (pl), 06.-10.10.2003. Volltext nicht online.

Rakowitz, M. (2000) Grid Refinement Study with a UHCA Wing-Body Configuration Using Richardson Extrapolation and Grid Convergence Index GCI. 12. DGLR-Fachsymposium AG STAB, Stuttgart (de), 15.-17.11.2000. Volltext nicht online.

Rakowitz, M. (2002) Grid Refinement Study with a UHCA Wing-Body Configuration Using Richardson Extrapolation and Grid Convergence Index GCI. In: Notes on Numerical Fluid Mechanics, Vol. 77, pp. 297-303. Springer. 12. DGLR-Fachsymposium AG STAB, Stuttgart (de), 15.-17.11.2000. ISBN 3-540-42696-5. Volltext nicht online.

Rakowitz, M. and Eisfeld, B. and Schwamborn, D. and Sutcliffe, M. (2003) Structured and Unstructured Computations on the DLR-F4 Wing-Body Configuration. Journal of Aircraft, 40 (2), pp. 256-264. Volltext nicht online.

Rakowitz, M. and Heinrich, S. and Krumbein, A. and Eisfeld, B. and Sutcliffe, M. (2005) Computation of Aerodynamic Coefficients for Transport Aircraft with MEGAFLOW. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 135-150. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6. Volltext nicht online.

Rakowitz, M. and Sutcliffe, M. and Eisfeld, B. and Schwamborn, D. and Bleecke, H. and Faßbender, J. (2002) Structured and Unstructured Computations on the DLR-F4 Wing-Body Configuration. 40th AIAA Aerospace Science & Exhibit, 2002-01-14 - 2002-01-17, Reno (USA). Volltext nicht online.

Redeker, G. (2001) Vortex Flow Experiment 2. Kolloquium des Instituts für Strömungsmechanik der TU Braunschweig, Braunschweig (de), 28.09.2001. Volltext nicht online.

Rein, M. (2002) Capillary effects at newly formed liquid–liquid contacts. Physics of Fluids, 14 (1), pp. 411-414. Volltext nicht online.

Rein, M. (2002) Introduction to Drop-Surface Interactions. In: Drop-Surface Interactions CISM Courses and Lectures, 456. Springer Wien New York. pp. 1-24. ISBN 3-211-83692-6. Volltext nicht online.

Rein, M. (2002) Interactions between Drops and Hot Surfaces. In: Drops-Surface Interactions CISM Courses and Lectures, 456. Springer Wien New York. pp. 185-217. ISBN 3-211-83692-6. Volltext nicht online.

Rein, M. (2003) Das Beschichtungsverfahren Kaltgasspritzen. Technische Universität Wien, 23.5.2003. Volltext nicht online.

Rein, M. (2003) Simulation aerothermischer und mechanischer Belastungen des bodennahen HFK-Flugs an Werkstoffoberflächen. Symposium "Hochtemperaturwerkstoffe - Entwicklung, Prüfverfahren und Einsatzmöglichkeiten", 8.-10.4.2003, Erding. Volltext nicht online.

Rein, M. (1998) Turbulent open-channel flows: drop generation and self-aeration. Journal of Hydraulic Engineering, 124 (1), pp. 98-102. Volltext nicht online.

Rein, M. (1998) Spray deposition: the importance of droplet impact phenomena. In: Sprühkompaktieren / Sprayforming SFB 372, Vol. 3. Universität Bremen, Bremen 1998. ISBN 3-88722-419-1. Volltext nicht online.

Rein, M. (1998) The impact of droplets on plane liquid surfaces. Zeitschrift für angewandte Mathematik und Mechanik, 78 (S2), pp. 685-688. Volltext nicht online.

Rein, M. (1999) The reflection of drops off hot surfaces. Zeitschrift für angewandte Mathematik und Mechanik, 79 (S3), pp. 743-744. Volltext nicht online.

Rein, M. (1999) Zur Stabilität von Grenzflächen zwischen Fluiden, die in Richtung der Flächennormalen beschleunigt werden. Seminar, Techn. Univ. Wien, Wien, 3. März 1999. Volltext nicht online.

Rein, M. (1999) The interaction of droplets with plane liquid surfaces. Seminar, Department of Mechanical and Aerospace Engineering Colorado School of Mines, Golden, CO, 15. November 1999. Volltext nicht online.

Rein, M. (1999) Stosswellen, Kavitation und Kapillarität beim Tropfenaufprall. Kolloquium Thermo- und Fluiddynamik, ETH Zürich, Zürich, Schweiz, 2. Dezember 1999. Volltext nicht online.

Rein, M. (2000) Wechselwirkungen zwischen Tropfen und ebenen Flüssigkeitsoberflächen. Hermann-Föttinger-Institut Seminar für Strömungsmechanik, Techn. Univ. Berlin, Berlin, 15. Dezember 2000. Volltext nicht online.

Rein, M. (2003) Kaltgasspritzen: eine innovative Technologie für Schichten in Luft- und Raumfahrt. Congress Industrielle Oberflächentechnik, Braunschweig 11.02.2003. Volltext nicht online.

Rein, M. (2000) Minisymposium 17: Compressible Multiphase Flows. GAMM Jahrestagung, Göttingen, 2.-7. April 2000. Volltext nicht online.

Rein, M. (2000) Overview of fluid mechanical and thermodynamic phenomena of drop-surface interactions. Advanced School and Workshop on Drop-Surface Interactions, Udine, Italien, 17. - 21. Juli 2000. Volltext nicht online.

Rein, M. (2000) Cavitation and capillary effects during liquid-liquid impacts. Advanced School and Workshop on Drop-Surface Interactions, Udine, Italien, 17. - 21. Juli 2000. Volltext nicht online.

Rein, M. (2000) Drop impact on hot surfaces: importance of the wall temperature and the Weber number. Advanced School and Workshop on Drop-Surface Interactions, Udine, Italien, 17. - 21. Juli 2000. Volltext nicht online.

Rein, M. (2000) Approaches to modeling of the dynamic Leidenfrost phenomenon I. Advanced School and Workshop on Drop-Surface Interactions, Udine, Italien, 17. - 21. Juli 2000. Volltext nicht online.

Rein, M. (2000) Approaches to modeling of the dynamic Leidenfrost phenomenon II. Advanced School and Workshop on Drop-Surface Interactions, Udine, Italien, 17. - 21. Juli 2000. Volltext nicht online.

Rein, M. (2003) Simulation von Bedingungen eines bodennahen Hochgeschwindigkeitsfluges II - Abschlussbericht -. DLR-Interner Bericht. 224 - 2003 C 19. 57 S. Volltext nicht online.

Rein, M. (2004) Zur Strömungsmechanik des Tropfenaufpralls. Fakultät für Physik der Universität Göttingen, Workshop über neue Forschungsarbeiten, Göttingen, 25. Juni 2004. Volltext nicht online.

Rein, M. (2004) Schnell und kalt – Beschichten von Oberflächen mittels Kaltgassspritzen. mo – Metalloberfläche, 58 (4), pp. 55-57. Volltext nicht online.

Rein, M. and Bütefisch, K.-A. (1999) Experimentelle Simulation von Bedingungen eines bodennahen Hochgeschwindigkeitsfluges an Materialoberflächen. DLR-Interner Bericht. 223 - 99 C 25. Volltext nicht online.

Rein, M. and Erdi-Betchi, A. and Klinkov, K. (2004) Zur Strömungsmechanik des Beschichtungsverfahrens "Kaltgasspritzen". 114. Norddeutsches Mechanik-Kolloquium, Clausthal, 26.6.04. Volltext nicht online.

Rein, M. and Erdi-Betchi, A. and Klinkov, K.V. (2002) Transonic Flow Phenomena of the Cold Spray Deposition Process. IUTAM Symposium Transsonicum IV, Göttingen, 2.-6. Sept. 2002. Volltext nicht online.

Rein, M. and Erdi-Betchi, A. and Klinkov, K.V. (2003) Transonic Flow Phenomena of the Cold Spray Deposition Process. In: IUTAM Symposium Transsonicum IV Fluid Mechanics and its Applications, Vol. 73. Kluwer Academic Publishers. ISBN 1-4020-1608-5. Volltext nicht online.

Rein, M. and Meier, G.E.A. and Raffel, M, and Richard, H. (1999) A BOOT for a supersonic free jet. 52nd Annual Meeting of the Division of Fluid Dynamics of the. Volltext nicht online.

Rein, M. and Poulikakos, D. (2004) Minisymposium 8: Drop-Surface-Interactions. 75th Annual Scientific Conference of the Gesellschaft für Angewandte Mathematik und Mechanik, Dresden, March 21-27, 2004. Volltext nicht online.

Rein, M. [Hrsg.] (2002) Drop-Surface Interactions. CISM Courses and Lectures, 456. Springer Wien New York. 314 S. ISBN 3-211-83692-6. Volltext nicht online.

Rein, Martin (2006) Experimental simulation of maneuvers in a wind-tunnel. UC Davis. [Other] (Unpublished) Volltext nicht online.

Rein, Martin and Rosemann, Henning and Schülein, Erich (2004) Reduzierung des Wellenwiderstands transsonisch umströmter Tragflügelprofile mittels Spikes. 14. DGLR-Fach-Symposium der STAB, ZARM Universität Bremen, 16.-18. November 2004, 2004-11-16 - 2004-11-18, Bremen. Volltext nicht online.

Reinke, R. (2004) Neuentwicklung eines Programmpaketes zur Ansteuerung eines PIV Aufnahmesystems mit Hilfe eines Sequenzers – Konzeption, Entwicklung und Funktionstest. DLR-Interner Bericht. 224-2004 A 10. 65 S. Volltext nicht online.

Reynier, P. (2001) Coupling between an Actuator Disk and a Navier-Stokes-Solver: Application to a Missile with Latice Wings. DLR-Interner Bericht. 129-2001/12. 33 S. Volltext nicht online.

Reynier, P. and Reisch, U. and Longo, J.M.A. and Radespiel, R. (2002) Numerical study of hypersonic missiles with lattice wings using an actuator disk. 20th Applied Aerodynamics Conference, St. Louis (usa), 24.-27.06.2002. Volltext nicht online.

Reynier, P. and Reisch, U. and Longo, J.M.A. and Radespiel, R. (2004) Flow prediction around a missile with lattice wings using the actuator disc concept. Aerospace Science and Technology, 8 (5), pp. 377-388. Volltext nicht online.

Reynier, P. and Schülein, E. (2002) Incorporation of an Actuator Disc for Lattice Wing Modelling in an unstructured Navier-Stokes Solver. 13. DGLR-Fach Symposium, München (de), 12.-14.11.2002. Volltext nicht online.

Reynier, Ph. and Schülein, E. and Longo, J.M. (2003) Simulation of Missiles with Grid Fins using Unstructured Navier-Stokes Solver coupled to a Semi-Empirical Actuator Disc. International Symposium “Integrating CFD and Experiments”, 8-9 September 2003, Glasgow, UK,. Volltext nicht online.

Richard, H. and Raffel, M. (2002) Rotor wake measurements: Full-scale and model tests. 58th Annual Forum of American Helicopter Society, Montreal, Canada, June 11-13, 2002. Volltext nicht online.

Richard, H. and Raffel, M. and Rein, M. and Kompenhans, J. and Meier, G.E.A. (2000) Demonstration of the applicability of a Background Oriented Schlieren (BOS) method. In: Vortrag. 10th Intern. Symposium on Applications of Laser Techniques in Fluid Mechanics, Lisbon, Portugal, July 2000. Volltext nicht online.

Richter, Christoph and Ehrenfried, Klaus and Schönwald, Norbert and Steger, Mathias and Thiele, Frank (2009) Acoustic intensity based data analysis and assessment in computational aeroacoustics. Journal of Sound and Vibration, 327 (3-5), pp. 490-506. Elsevier. doi: 10.1016/j.jsv.2009.06.024. ISSN 0022-460X. Volltext nicht online.

Richter, K. and Rosemann, H. (2001) Experimenteller Einsatz von Mini-Klappen am Profil VC-Opt bei transsonischen Geschwindigkeiten. 10. STAB-Workshop, DLR, Göttingen, 14.-15. Nov. 2001. Volltext nicht online.

Richter, K. and Rosemann, H. (2001) Experimental investigation of trailing-edge devices at transonic speeds. Aerodynamics Conference 2001, Royal Aeronautical Society, London, UK. 9.-10. April 2001. Volltext nicht online.

Riedel, H. and Sitzmann, M. (2002) Aspects of Flow Transition Detection When Flight Testing Engine Nacelles. Journal of Aircraft, 39 (6), pp. 1019-1027. Volltext nicht online.

Riedel, Hansgeorg and Sitzmann, Martin (2008) In-flight Investigations of Atmospheric Turbulence. DLR-Interner Bericht. DLR-IB 124-2008/3. 68 S. Volltext nicht online.

Riedel, Hansgeorg and Sitzmann, Martin (2008) Prediction of the transition location on a hybrid laminar flow engine nacelle using the e<sup>N</sup> method of linear boundary layer stability theory and validation by flight testing. DLR-Interner Bericht. DLR-IB 124-2008/4. 36 S. Volltext nicht online.

Robinson, M. (2004) Stress Analysis of HEG Piston. DLR-Interner Bericht. 224-2004 A 05. 64 S. Volltext nicht online.

Robinson, M. and Hannemann, V. (2004) Studie zur Anwendbarkeit des DLR Tau-Verfahrens für Gaszentrifugen. DLR-Interner Bericht. 224-2004 A 07. 13 S. Volltext nicht online.

Rohardt, C.-H. (2004) Entwurf einer Profilfamilie für eine 2-Megawatt Windkraftanlage (RePower PP-92). DLR-Interner Bericht. 124-2004/30. 67 S. Volltext nicht online.

Rohardt, C.-H. and Horstmann, K.H. (2002) Entwurf und Vermessung einer Profilfamilie für eine 5MW Windkraftanlage. DLR-Interner Bericht. IB 124-2002/14. 167 S. Volltext nicht online.

Rohardt, C.-H. and Reckzeh, D. (2001) Abschlußbericht Megaflug DLR - AP3.1 und 3.3. DLR-Interner Bericht. 129-2001/2. Volltext nicht online.

Ronzheimer, A. (2002) Post-Parameterisation of CAD-Geometries Using Freeform Deformation and Grid Generation Techniques. 13. DGLR-Fachsymposium der AG STAB, München (de), 12.-14.11.2002. Volltext nicht online.

Ronzheimer, A. (2002) Post-Parameterization of Complex CAD-Based Aircraft-Shapes Using Freeform Deformation. In: 8th International Conference on Numerical Grid Generation in Computational Field Simulations. 8th International Conference on Numerical Grid Generation in Computational Field Simulations, Honolulu (usa), 01.-05.06.2002. ISBN 0-9651627-4-5. Volltext nicht online.

Ronzheimer, A. (2004) Post-Parameterisation of CAD-Geometries Using Freeform Deformation and Grid Generation Techniques. In: New Results in Numerical and Experimental Fluid Mechanics IV, Vol. 87, pp. 382-389. Springer Verlag, Berlin, Heidelberg, New York. 13th STAB/DGLR Symposium, München (de), 12.-14.11.2002. ISBN 3-540-20258-7. Volltext nicht online.

Ronzheimer, A. (2004) Shape Parameterisation Based on Freeform Deformation in Aerodynamic Design Optimization. In: ERCOFTAC Design Optimization: Methods & Applications, CD-ROM. ERCOFTAC Design Optimization: Methods & Applications, Athen (gr), 31.03.-02.04.2004. Volltext nicht online.

Ronzheimer, A. (2005) Shape Parametrization Using Freeform Deformation. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 211-222. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6. Volltext nicht online.

Rosemann, H. (2003) First Results from GARTEUR AG-28 Transonic Wing/Body Code Validation Experiment. Second KATnet/GARTEUR Workshop on High Speed Aerodynamics 3-4 September 2003, University of Bath, UK. Volltext nicht online.

Rosemann, H. (2004) WAVE DRAG REDUCTION CONCEPTS FOR TRANSSONIC WINGS. European Congress on Computational Methods in Applied Sciences and Engineering ECCOMAS 2004, Jyväskylä, 24–28 July 2004. Volltext nicht online.

Rosemann, H. and Richter, K. and Birkemeyer, J. and Rodde, A.-M. and Schmitt, V. (2002) APPLICATION OF A 3-D SHOCK CONTROL BUMP ON A TRANSPORT. 5th ONERA - DLR AEROSPACE SYMPOSIUM , ODAS, 4-6 June 2002, Toulouse, France. Volltext nicht online.

Rossignol, Karl-Stephane and Hu, Nan (2012) Aeroacoustic Characterisation of Shape-Optimized Low-Noise Wind Turbine Blades. DLR-Interner Bericht. DLR-IB 124-2012/914. DLR. 75 S. Volltext nicht online.

Rossow, C.-C. and Kroll, N. and Schwamborn, D. (2005) The MEGAFLOW Project - Numerical Flow Simulation for Aircraft. DLR-Interner Bericht. 124-2005/1. 24 S. Volltext nicht online.

Rossow, Cord-Christian (1987) Comparison of Cell Centered and Cell Vertex Finite Volume Schemes. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 20. Vieweg Verlag. pp. 321-334. Volltext nicht online.

Rossow, Cord-Christian (1991) Flux Balance Splitting with Rotated Differences: A Second Order Accurate Cell Vertex Upwind Scheme. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 35. Vieweg Verlag. pp. 567-576. Volltext nicht online.

Rossow, Cord-Christian (1992) Efficient Computation of Inviscid Flow Fields Around Complex Configurations Using a Multi-Block Multigrid Method. In: Communications on Applied Numerical Methods pp. 735-747. Volltext nicht online.

Rossow, Cord-Christian (1994) Accurate Solution of the 2-D Euler Equation with an Efficient Cell-Vertex Upwind Scheme. AIAA Journal, 32 (2), pp. 278-284. Volltext nicht online.

Rossow, Cord-Christian (1999) A Simple Flux Splitting Scheme for Compressible Flows. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 72. Vieweg Verlag Braunschweig. pp. 355-362. Volltext nicht online.

Rossow, Cord-Christian (2002) Convergence Acceleration on Unstructured Meshes. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 77. Springer-Verlag Berlin Heidelberg New York. pp. 304-311. Volltext nicht online.

Rossow, Cord-Christian (2003) A Pressure/Density Based Method for the Computation of Incompressible and Compressible Flows. Journal of Computational Physics, 185 (2), pp. 375-398. Volltext nicht online.

Rossow, Cord-Christian (2003) Extension of a Compressible Code Toward the Incompressible Limit. AIAA Journal, 41 (12), pp. 2379-2386. Volltext nicht online.

Rossow, Cord-Christian (2004) Flow Computation at All Speeds. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 87. Springer-Verlag Berlin Heidelberg New York. pp. 358-365. Volltext nicht online.

Rossow, Cord-Christian (1989) Berechnung von Strömungsfeldern durch Lösung der Euler-Gleichungen mit einer erweiterten Finite-Volumen Diskretisierungsmethode. DLR-Forschungsbericht. DLR-FB 89-38. Dissertation. TU Braunschweig. Volltext nicht online.

Rossow, Cord-Christian (1995) Ein Finite-Volumen-Verfahren mit Flußbilanzspaltung zur numerischen Strömungssimulation. DLR-Forschungsbericht. DLR-FB 95-34. Habilitation. TU Braunschweig. Volltext nicht online.

Rossow, Cord-Christian (1990) Flux Balance Splitting - A New Approach for a Cell Vertex Upwind Scheme. In: Lecture Notes in Physics, 371. 12th International conference on Numercial Methods in Fluid Dynamics, 1990-07, Oxford (GB). Volltext nicht online.

Rossow, Cord-Christian (1993) Accurate Solution of the 2-D Euler Equations with an Efficient Cell-Vertex Upwind Scheme. AIAA conference, 1993, Reno, NV (USA). Volltext nicht online.

Rossow, Cord-Christian (1994) A Cell-Vertex Upwind Scheme with Flux Balance Splitting for the Euler and Navier-Stokes Equations on Structured Meshes. In: VKI Lecture Series 94-05. VKI Lecture Series, 1994-03-21 - 1994-03-25, Brüssel (B). Volltext nicht online.

Rossow, Cord-Christian (1999) A Flux Splitting System for Compressible and Incompressible Flows. 14th Computational Fluid Dynamics Conference, 1999, Norfolk, VA (USA). Volltext nicht online.

Rossow, Cord-Christian (2001) A Pressure/Density Based Method for the Computation of Incompressible and Compressible Flows. 15th Computational Fluid Dynamics Conference, 2001, Anaheim, CA (USA). Volltext nicht online.

Rossow, Cord-Christian (2003) Extension of a Compressible Code Towards the Incompressible Limit. 41st Aerospace Sciences Meeting, 2003, Reno, NV (USA). Volltext nicht online.

Rossow, Cord-Christian (2006) Convergence Acceleration for Solving the Compressible Navier-Stokes Equations. AIAA Journal, 44 (22), pp. 345-352. Volltext nicht online.

Rossow, Cord-Christian (2007) Efficient Computation of Compressible and Incompressible Flows. Journal of Computational Physics (220), pp. 879-899. Academic Press Inc. Elsevier Science, San Diego/USA. ISSN 0021-9991. Volltext nicht online.

Rossow, Cord-Christian (2006) Toward Efficient Computation of Compressible and Incompressible Flows. 36th AIAA Fluid Dynamics Conference, 2006-06-05 - 2006-06-09, San Francisco, CA (USA). Volltext nicht online.

Rossow, Cord-Christian (2007) Enhanced Runge-Kutta / Implicit Methods for Solving the Navier-Stokes Equations. 15. DGLR-Fach-Symposium (STAB), 2006-11-29 - 2006-12-01, Darmstadt (D). Volltext nicht online.

Rossow, Cord-Christian (2006) Toward efficient solution of the compressible Navier-Stokes equations. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 92. Springer-Verlag Berlin Heidelberg New York. pp. 397-404. ISBN 3-540-33286-3. Volltext nicht online.

Rossow, Cord-Christian (2007) Enhanced Runge-Kutta / Implicit Methods for Solving the Navier-Stokes Equations. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Meshes Springer Verlag Berlin Heidelberg New York. pp. 202-209. ISBN 3-540-74458-4. Volltext nicht online.

Rossow, Cord-Christian (2009) Designing the Aircraft of the Future. 56th Aeronautics Conference, 5.5. - 7.5.2009, Ottawa, Kanada. (Unpublished) Volltext nicht online.

Rossow, Cord-Christian (2009) Aerodynamics: A Discipline Swept Away? Lanchester Lecture, 27.10.2009, Manchester, Grossbritannien. (Unpublished) Volltext nicht online.

Rossow, Cord-Christian (2009) Application of TAU for Aerodynamic Analysis, Design and Optimization. 21st Century Challenges in Computational Engineering and Science, 19. - 21.11.2009, Princeton, New Jersey, USA. (Unpublished) Volltext nicht online.

Rossow, Cord-Christian (2010) Institute of Aerodynamics and Flow Technology - Core Competencies. NAL-DLR Workshop , 18. - 22.1.2010, Bangalore, Indien. Volltext nicht online.

Rossow, Cord-Christian (2010) Aerodynamics - A Discipline swept away? The Aeronautical Journal, 114 (1160), pp. 599-609. Cambridge University Press. Volltext nicht online.

Rossow, Cord-Christian and Brodersen, Olaf and Ronzheimer, Arno (1997) Grundlagen zur Erzeugung strukturierter Rechennetze (Lehrveranstaltung). Harburger Sommerschule 'Gittererzeugung und Datenstruktur', 1997-09-08 - 1997-09-12, Hamburg (D). Volltext nicht online.

Rossow, Cord-Christian and Burgsmüller, Wolfgang (1999) Installation of High-Bypass-Ratio Engines on Future Transport Aircraft - The European Research Program ENIFAIR. In: Proceedings (3.1). 7th European Propulsion Forum, 1999-03, Pau (F). Volltext nicht online.

Rossow, Cord-Christian and Burgsmüller, Wolfgang and Rollin, C. (1998) Engine Integration on Future Transport Aircraft - The European Research Programs DUPRIN / ENIFAIR. 21st ICAS Symposium, 1998, Melbourne (AUS). Volltext nicht online.

Rossow, Cord-Christian and Cambier, Laurent (2009) European Numerical Aerodynamics Simulation Systems. In: 100 Volumes of ‘Notes on Numerical Fluid Mechanics’ Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 100. Springer-Verlag, Berlin Heidelberg. pp. 189-208. doi: 10.1007/978-3-540-70805-6_15. ISBN 978-3-540-70804-9. ISSN 1612-2909. Volltext nicht online.

Rossow, Cord-Christian and Godard, Jean-Luc and Hoheisel, Heinz and Schmitt, Volker (1994) Investigation of Propulsion Airframe Interference Effects on a Transport Aircraft Configuration. Journal of Aircraft, 31 (5), pp. 1022-1030. Volltext nicht online.

Rossow, Cord-Christian and Godard, Jean-Luc and Hoheisel, Heinz and Schmitt, Volker (1992) Investigation of Propulsion Airframe Interference Effects on a Transport Aircraft Configuration. AIAA conference, 1992, Nashville, TN (USA). Volltext nicht online.

Rossow, Cord-Christian and Godard, Jean-Luc and Hoheisel, Heinz and Schmitt, Volker (1996) Investigation of Interference Effects for Different Engine Positions on a Transport Aircraft Configuration. In: DLR-Mitteilungen (96-01), 11.01-11.22. DLR Workshop on 'Aspects of Engine Airframe Integration for Transport Aircraft', 1996-03-06 - 1996-03-07, Braunschweig (D). Volltext nicht online.

Rossow, Cord-Christian and Hoheisel, Heinz (1994) Numerical Study of Interference Effects of Wing-Mounted Advanced Engine Concepts. 19th ICAS Congress, 1994-09-18 - 1994-09-23, Anaheim, CA (USA). Volltext nicht online.

Rossow, Cord-Christian and Hoheisel, Heinz and Kiock, Reinhard and Ronzheimer, Arno and Baumert, W. and Capdevila, H. (1990) Aspects of Theoretical and Experimental Investigations on Engine/Airframe Integration. In: Proceedings (2.7.3). 17th ICAS Congress, 1990-09, Stockholm (S). Volltext nicht online.

Rossow, Cord-Christian and Kroll, Norbert (2008) High Performance Computing Serves Aerospace Engineering: Opportunities for Next Generation Product Development. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008-01-07 - 2008-01-10, Reno, NV (USA). (Unpublished) Volltext nicht online.

Rossow, Cord-Christian and Kroll, Norbert (2007) Numerical Simulation - Complementing Theory and Experiment as the Third Pillar in Aerodynamics. Hermann Schlichting Gedächtnis-Kolloquium, 2007-09-28 - 2007-09-29, Braunschweig, D. (Unpublished) Volltext nicht online.

Rossow, Cord-Christian and Kroll, Norbert and Radespiel, Rolf and Scherr, Steven (1988) Investigation of the Accuracy of Finite Volume Methods for 2- and 3-Dimensional Flows. In: AGARD-CPP-437, 17.1-17.11. AGARD, 1988, Lissabon (P). Volltext nicht online.

Rossow, Cord-Christian and Kroll, Norbert and Schwamborn, Dieter (2006) Numerical Aerodynamics at DLR. In: Chinese Journal of Aeronautics, 19 (2), p. 134. East West High Speed Flow Field (EWHSFF) Conference 2005, 2005-10-19 - 2005-10-22, Beijing, China. ISSN 1000-9361. Volltext nicht online.

Rossow, Cord-Christian and Radespiel, Rolf (1988) Konvergenzbeschleunigung bei der Berechnung der reibungsbehafteten Umströmung eines Tragflügels. In: DGLR-Bericht (88-05), pp. 301-312. STAB, 1988, Braunschweig (D). Volltext nicht online.

Rossow, Cord-Christian and Radespiel, Rolf (1989) Fortschritte bei der effizienten Berechnung von Strömungen mit Reibung. DLR-Nachrichten (Heft 58). Volltext nicht online.

Rossow, Cord-Christian and Radespiel, Rolf and Swanson, Charles R. (1990) An Efficient Cell-Vertex Multigrid Scheme for the Three-Dimensional Navier-Stokes Equations. AIAA Journal, 28 (8), pp. 1464-1472. Volltext nicht online.

Rossow, Cord-Christian and Radespiel, Rolf and Swanson, Charles R. (1989) An Efficient Cell-Vertex Multigrid Scheme for the Three-Dimensional Navier-Stokes Equations. In: AIAA 89-1953. AIAA, 1989, Reno (USA). Volltext nicht online.

Rossow, Cord-Christian and Ronzheimer, Arno (1991) Multi-Block Grid Generation Around Wing-Body-Engine-Pylon Configurations. In: Proceedings. Numerical Grid Generation in Computational Fluid Dynamics and Related Fields, 1991, Barcelona (E). Volltext nicht online.

Rossow, Cord-Christian and Ronzheimer, Arno (1991) Investigation of Interference Phenomena of Modern Wing-Mounted High-Bypass-Ratio Engines by the Solution of Euler-Equations. In: Proceedings. AGARD Fluid Dynamics Panel Symposium on 'Aerodynamic Engine/Airframe Integration', 1991, Fort Worth, Texas (USA). Volltext nicht online.

Rossow, Cord-Christian and Ronzheimer, Arno and Rudnik, Ralf (1992) Numerische Studie der Interferenzeffekte von zwei- und vierstrahligen Transportflugzeugkonfigurationen. In: Konferenzband. DGLR-Jahrestagung, 1992-10, Bremen (D). Volltext nicht online.

Rossow, Cord-Christian and Swanson, Ray Charles and Turkel, Eli (2007) Convergence acceleration of Runge-Kutta schemes for solving the Navier-Stokes equations. Journal of Computational Physics (224), pp. 365-388. Academic Press Inc. Elsevier Science, San Diego/USA. ISSN 0021-9991. Volltext nicht online.

Rossow, Cord-Christian and Kroll, Norbert (2009) Numerical Simulation – Complementing Theory and Experiment as the Third Pillar in Aerodynamics. In: Hermann Schlichting – 100 Years Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), 102. Springer-Verlag, Berlin Heidelberg. pp. 39-58. doi: 10.1007/978-3-540-95998-4_4. ISBN 978-3-450-95997-7. ISSN 1612-2909. Volltext nicht online.

Rudnik, R. (2001) Towards CFD Validation for 3D High Lift Flows - EUROLIFT. In: Book of Abstracts - ECCOMAS CFD 2001, 70-. ECCOMAS Computational Fluid Dynamics Conference 2001, Swansea (gb), 04.-07.09.2001. ISBN 0905091116. Volltext nicht online.

Rudnik, R. (2005) Application of the MEGAFLOW Software at DLR. In: MEGAFLOW - Numerical Flow Simulation for Aircraft Design, 89, pp. 269-282. Springer Verlag. Closing Presentation DLR Project MEGAFLOW, Braunschweig (de), 10.-11.12.2002. ISBN 3-540-24383-6. Volltext nicht online.

Rudnik, R. and Eliasson, P. and Perraud, J. (2005) Evaluation of CFD methods for transport aircraft high lift systems. The Aeronautical Journal, 109 (1092), pp. 53-64. Volltext nicht online.

Rudnik, R. and Heinrich, R. and Eisfeld, B. and Schwarz, T. (2004) DLR Contributions to Code Validation Activities within the European High Lift Project EUROLIFT. In: New Results in Numerical and Experimental Fluid Dynamics IV, 87, pp. 42-49. Springer Verlag , Berlin, Heidelberg, New York. 13th DGLR STAB Symposium, München (de), 12.-14.11.2002. ISBN 3-540-20258-7. Volltext nicht online.

Rudnik, R. and Melber, S. and Ronzheimer, A. and Brodersen, O. (2001) 3D RANS Simulations for Transport Aircraft High Lift Configurations. Journal of Aircraft, 38 (5), pp. 895-903. Volltext nicht online.

Rudnik, R. and Ronzheimer, A. (2004) Numerical Investigation of the Flow Around Different Slat Tracks on a Swept High Lift Wing Segment. In: New Results in Numerical and Experimental Fluid Mechanics IV, 87, pp. 58-65. Springer Verlag, Berlin Heidelberg New York. 13th DGLR STAB Symposium, München (de), 12.-14.11.2002. ISBN 3-540-20258-7. Volltext nicht online.

Rudnik, R. and Rossow, C.-C. and Geyr, H. von (2002) Numerical simulation of engine/airframe integration for high-bypass engines. Aerospace Science and Technology, 6 (1), pp. 31-42. Volltext nicht online.

Rudnik, Ralf (2008) Stall Behaviour of the EUROLIFT High Lift Configurations. In: AIAA 2008-836. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008-01-07, Reno, NV, USA. Volltext nicht online.

Rudnik, Ralf and Germain, Eric (2007) Re-No. Scaling Effects on the EUROLIFT High Lift Configurations. 45th AIAA Aerospace Sciences Meeting and Exhibit, 2007-01-08 - 2007-01-11, Reno, NV (USA). Volltext nicht online.

Rudnik, Ralf and Geyr von, Heiko (2007) The European High Lift Project EUROLIFT II - Objectives, Approach, and Structure. 25th AIAA Applied Aerodynamics Conference, 2007-06-25 - 2007-06-28, Miami, FL (USA). Volltext nicht online.

Rudnik, Ralf and Geyr von, Heiko and Wild, Jochen (2006) The European High Lift Programme II. In: European Congress on Computational Methods in Applied Science and Engineering, pp. 1-4. ECCOMAS 2006, 2006-09-05 - 2006-09-08, Delft (NL). ISBN 90-9020970-0. Volltext nicht online.

Rudnik, R. (2015) Schlussbericht über das BMWI Verbundvorhaben HINVA (High-Lift IN-Flight Validation). DLR-Interner Bericht. IB 124-2015/05. DLR e.V.. 53 S. Volltext nicht online.

Rudnik, Ralf (2013) Experimental Analysis of Separation and Transition Phenomena for the DLR-F11 High Lift Configuration. 31st AIAA Applied Aerodynamics Conference, 24.-27. Juni 2013, San Diego, USA. Volltext nicht online.

Rudolph, M. (2003) Entwicklung eines Programms zur automatischen Adaption blockstrukturierter Netze. DLR-Interner Bericht. IB 124-2003/3. 60 S. Volltext nicht online.

S

Sabanca, M. and Delfs, J. (2005) Numerical Investigation of Self-Excited Oscillations of a Generic Profile. 31. Deutsche Jahrestagung für Akustik (DAGA ' 2005), München (de), 14.-17.03.2005. Volltext nicht online.

Sabanca, M. and Durst, F. (2003) Flows past a tiny circular cylinder at high temperature ratios and slight compressible effects on the vortex shedding. Physics of Fluids, 15 (7), pp. 1821-1829. Volltext nicht online.

Sachs, W. (2004) ToPaS - Three Dimensional optical Pressure analysis System. Abschlusspräsentation, Niedergeschwindigkeits PSP, DLR, Göttingen, 24.05.2004. Volltext nicht online.

Sammler, B. (2004) Dual Stereo PIV Measurements over a Delta Wing Model under Transonic Conditions. DLR/ONERA - Annex II Meeting, DLR, Köln, 6. - 7. April 2004. Volltext nicht online.

Sammler, B. and Arnott, A. and Agocs, J. and Schröder, A. and Otter, D. and Kompenhans, J. (2003) Stereo PIV Measurements over a Delta Wing Model in Transonic Flow. 5th International Symposium on Particle Image Velocimetry, Busan, Süd Korea, 22.09.-24.09.03. Volltext nicht online.

Sammler, B. and Arnott, A. and Schröder, A. and Agocs, J. and Kompenhans, J. and Neitzke, K.P. (2002) Konditionierte Multi-Fenster PIV-Messmethode und die Anwendung auf Flügel-Klappen-Konfigurationen. In: Lasermethoden in der Strömungsmesstechnik, 13.1-13.5. Universität Rostock, Fachbereich Maschinenbau und Schiffstechnik, 18051 Rostock. Lasermethoden in der Strömungsmesstechnik, Rostock, 10. bis 12. September 2002. ISBN 3-86009-233-2. Volltext nicht online.

Sammler, B. and Schröder, A. and Arnott, A. and Otter, D. and Agocs, J. and Kompenhans, J. (2003) Vortex Investigations Over a Rolling Delta Wing Model in Transonic Flow by Stereo PIV Measurements. In: ICIASF 2003 Record, IEEE Catalog Number: 03CH37501, pp. 268-277. 20th International Congress on Instrumentation in Aerospace Simulation FacilitiesGöttingen, Germany, August 25 – 29, 2003. ISBN 0-7803-8149-1. Volltext nicht online.

Sammler, B. and Schröder, A. and Arnott, A. and Otter, D. and Agocs, J. and Kompenhans, J. (2003) Stereo PIV Messungen an einem Deltaflügelmodell unter transsonischen Bedingungen. 11. STAB Workshop, DLR Göttingen, 04.11.-06.11.2003. Volltext nicht online.

Sassenberg, W. (2001) Jodgas als frequenzselektiver Filter. DLR-Interner Bericht. 223-2001 A 19. 27 S. Volltext nicht online.

Sassenberg, W. (2002) Aufbau eines Doppler Global Velocimetrie-Systems für den Einsatz in kryogenen Windkanälen. DLR-Interner Bericht. 224-2002 A 11. 58 S. Volltext nicht online.

Schade, Niko (2011) Simulation of Trajectories of Cuboid Cargos Released from a Generic Transport Aircraft. 29th AIAA Applied Aerodynamics Conference, 27 - 30 June 2011, Honolulu, USA. Volltext nicht online.

Schade, Niko and Brezillon, Joel and Brodersen, Olaf and Dwight, Richard and Ronzheimer, Arno and Wild, Jochen (2006) Different Techniques of Aerodynamic Shape Optimization for Civil Transport Aircrafts. AEROCHINA China-Europe Open Seminar, 2006-10-16 - 2006-10-18, Xi'an (VR China). (Unpublished) Volltext nicht online.

Schade, Niko and Brezillon, Joel and Brodersen, Olaf and Keye, Stefan and Dwight, Richard and Ronzheimer, Arno and Wild, Jochen (2007) Improved Techniques of Aerodynamic Shape Optimization for Coupled Fluid-Structure Calculations of Civil Transport Aircraft. AEROCHINA Europe-China Open Workshop, 2007-04-25 - 2007-04-27, Barcelona (Spain). Volltext nicht online.

Schade, Niko and Acisu, Ismail (2007) Numerische und expperimentelle Untersuchungen zur Simulation von Lastabsetzvorgaengen. 13. STAB Workshop, 2007-11-14 - 2007-11-15, Goettingen. (Unpublished) Volltext nicht frei.

Schmeling, Daniel and Winter, Stefan and Bosbach, Johannes and Wagner, Claus (2016) On the Influence of the Aspect Ratio on Structure Formation in Turbulent Mixed Convection. 24th International Congress of Theoretical and Applied Mechanics (ICTAM), 21. - 26. Aug. 2016, Montréal, Canada. Volltext nicht online.

Schmidt, O.T. (2005) Vorhersage von Anlegelinien-Transition bei Hochauftriebssystemen durch 2D-Schnittberechnungen. DLR-Interner Bericht. 124-2005/3. Diploma. 70 S. Volltext nicht online.

Schmitt, V. and Archambaud, J.P. and Horstmann, K.H. and Quast, A. (2001) Hybrid Laminar Fin Investigations. In: RTO AVT Symposium on Active Control Technology for Enhanced Performance Operational Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles, 1-1-1-10. RTO AVT Symposium on Active Control Technology for Enhanced Performance Operational Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles, Braunschweig (de), 08.-11.05.2000. Volltext nicht online.

Schmitt, V. and Redeker, G. (2001) Research Programs for Transport Aircraft in Europe. 44th Paris Air Show, Le Bourget (fr), 16.-24.06.2001. Volltext nicht online.

Schopferer, Simon and Froese, Sarah and Hanke, Michael and Liersch, Carsten M. and Cumnuantip, Sunpeth and Suchaneck, Andre and Immisch, Thomas (2016) Entwurf und Auslegung Hochfliegender Plattformen. DLR-Interner Bericht. DLR-IB-FT-BS-2016-205. Institut für Flugsystemtechnik. 67 S. Volltext nicht online.

Schrauf, G. and Horstmann, K.H. (2001) Linear Stability Applied to Natural and Hybrid Laminar Flow. Springer. DragNet Conference, Potsdam (de), 19.-21.06.2000. Volltext nicht online.

Schroeder, A. (2002) Structures of a turbulent spot - an investigation by means of multi-plane stereo PIV. Beijing University of Aeronautics and Astronautics, China 23.10.03. Volltext nicht online.

Schröder, A. (2002) Modern PIV Equipment of DLR for Aerodynamics. High Speed Aerodynamics, Institute (HSAI), CARDC, Mianyang, China, 15.10.02. Volltext nicht online.

Schröder, A. (2002) Structures of a turbulent spot - an investigation by means of multi-plane stereo PIV. High Speed Aerodynamics, Institute (HSAI), CARDC, Mianyang, China, 18.10.02. Volltext nicht online.

Schröder, A. (2002) Structures of a turbulent spot - an investigation by means of multi-plane stereo PIV. Nanjing University of Aeronautics and Astronautics, China, 21.10.02. Volltext nicht online.

Schröder, A. (2002) Investigation of artificially excited transitional boundary layer flows by means of stereo PIV. Beijing University of Aeronautics and Astronautics, Beijing, China, 23.10.2002. Volltext nicht online.

Schröder, A. (2004) Messung instationärer Geschwindigkeitsfelder mit der Particle Image Velocimetry (PIV)- Stand der Technik und Einsatzmöglichkeiten in der Fahrzeugaerodynamik. In: Tagung, pp. 1-30. FAHRZEUG-AERODYNAMIK, Essen, 27.- 28. Oktober 2004. Volltext nicht online.

Schröder, A. and Arnott, A. and Agocs, J. and Sammler, B. and Schneider, G. and Kompenhans, J. (2004) PIV for high lift applications. European Windtunnel Association Initial Joint Workshop, Toulouse, October 18-20, 2004. Volltext nicht online.

Schröder, A. and Dierksheide, U., LaVision, and Wolf, J., LaVision, and Herr, M. and Kompenhans, J. (2004) Investigation on trailing-edge noise sources by means of high-speed PIV. In: Proceedings, Online-Publication, pp. 1-9. 12th International Symposium on Applications of Laser Techniques to Fluid Mechanics, Lisbon, Portugal, July 12-15 2004. Volltext nicht online.

Schröder, A. and Heider, A. and Christou, K. (2004) Noise emission of free turbulent jets, a novel approach by multiple plane PIV. PivNet2 Workshop 9./10.July 2004, Lisbon, Portugal. Volltext nicht online.

Schröder, A. and Herr, M. and Dierksheide, U., LaVision, and Wolf, J., La. Vision, and Kompenhans, J. (2004) Investigation of trailing-edge noise sources by means of high-speed PIV. DLR/ONERA - Annex II Meting, DLR, Köln, 6.-7.04.2004. Volltext nicht online.

Schröder, A. and Herr, M., AS-BS, and Lauke, T., AS-BS, and Dierksheide, U., LaVision, Göttingen, (2004) A Study on Trailing Edge Noise Sources using High-Speed Particle Image Velocimetry. In: Proceedings (rev.) Symposium, pp. 1-8. 14th Symposium of STAB 2004, Bremen, 16-18 November, 2004. Volltext nicht online.

Schröder, A. and Kompenhans, J. (2002) Investigation of a turbulent spot using. In: Proceedings. 11th International Symposium on Applications of Laser Technique to Fluid Mechanics. Volltext nicht online.

Schröder, A. and Kompenhans, J. (2002) Structures of a turbulent spot an investigation by means of multiplane stereo PIV. In: Engineering Turbulence Modelling and Experiments 5 5, Proceedings 565-584. Elsevier Science Ltd, The Boulevard, Langford Lane, Kidlington, Oxford OX5 1GB, UK. ISBN 0-08-044114-9. Volltext nicht online.

Schröder, A. and Kompenhans, J. (2003) Investigation of transitional structures in artificially excited boundary layer flows by means of stereo and multi-plane PIV. In: Recent Results in Laminar-Turbulent Transition Notes on Nummerical Fluid Mechanics and Multidisciplinary Design, Volume 86 Seite 255 - 268. Springer Verlag Berlin Heidelberg New York. ISBN 3-540-40490-2. Volltext nicht online.

Schröder, Andreas and Agocs, Janos and Heider, André and Konrath, Robert (2005) Investigations of strake wake vortices in a high-lift-configuration using Stereo-PIV. DLR/ONERA Meeting, 2005-04-05 - 2005-04-06, Lille (France). Volltext nicht online.

Schröder, Andreas and Kompenhans, Jürgen and Engler, Rolf and Goldhahn, Erik (2005) Current Topics in Experimental Transonic Aerodynamics. In: Advanced Measuring Techniques for Supersonic Flows VKI Lecture Series 2005-01. VKI. 1-23und1-8. ISBN 2-930389-57-5. Volltext nicht online.

Schröder, W. (2002) Stability analysis of the 50 data points (priority 2) of the A320 HLF fin flight tests. Project Report, DLR-Interner Bericht. IB 124-2002/18. 62 S. Volltext nicht online.

Schröder, W. (2002) Stability analysis of the 34 data points (priority 3) of the A320 HLF fin flight tests. Project Report, DLR-Interner Bericht. IB 124-2002/19. 48 S. Volltext nicht online.

Schröder, W. (2002) Stability analysis of the 51 data points (priority 2) of the ELFIN II half wing tests in S1Ma of January 2000. Project Report, DLR-Interner Bericht. IB 124-2002/29. 68 S. Volltext nicht online.

Schröder, W. and Archambaud, J.P. (2001) Determination of the laminar/turbulent transition stations of the A320 HLF fin flight tests for the 34 data points of priority 3. DLR-Interner Bericht. 129-2001/10. Volltext nicht online.

Schröder, Wolfgang and Ewert, Roland (2007) Some concepts of LES-CAA coupling. In: Large-Eddy Simulation for Acoustics Cambridge University Press. pp. 222-237. ISBN 978-0-521-87144-0. Volltext nicht online.

Schwamborn, D. and Mack, A. and Pahlke, K. and Schütte, A. and Voß, R. (2004) Recent and future DLR projects on Multi-Disciplinary Simulation and Validation. PROMUVAL Short Course on Multidisciplinary Modelling, 2004-06-28 - 2004-06-29, Barcelona, (Spain). Volltext nicht online.

Schwamborn, Dieter and Weinman, Keith (2002) ON THE INFLUENCE OF TURBULENCE MODELING ON STEADY AND UNSTEADY FLOWS. Kluwer Academic Publishers. IUTAM, 2002-09-02, Göttingen (GER). ISBN 1-4020-1608-5. Volltext nicht online.

Schweikhard, R. (2004) Implementation and Validation of an Actuator Disc Boundary Condition for Helicopter Rotors into the Hybrid DLR RANS Solver TAU. DLR-Interner Bericht. 124-2004/27. 72 S. Volltext nicht online.

Schweikhard, R. (2005) Application of the EADS-M Mesher to a Transonic and a Supersonic Aircraft in High-Lift Configuration. DLR-Interner Bericht. 124-2005/912. 16 S. Volltext nicht online.

Schweikhard, R. and Le Chuiton, F. (2005) Actuator Disc for Helicopter Rotors in the Unstructured Flow Solver TAU. 31st European Rotorcraft Forum, 2005-09-13 - 2005-09-15, Firenze, Italy. Volltext nicht online.

Schweikhard, Roland (2005) Actuator Disk for Helicopter Rotors in an Unstructured Flow Solver. Journal of the American Helicopter Society, 52 (1), pp. 58-68. ISSN 0002-8711. Volltext nicht online.

Schäfer, R. and Mack, A. and Esser, B. and Gülhan, A. (2003) Fluid-structure interaction on a generic model of a reentry vehicle nosecap. 5th Congress on Thermal Stresses and related topics, Blacksburg, Virginia, USA 5. - 8. June 2003. Volltext nicht online.

Schäfer, R. and Mack, A. and Esser, B. and Gülhan, A. (2004) Experimental and Numerical Fluid-Structure Investigations of a Generic Bodyflap Region Model. 28 th International Cocoa Beach Conference and Exposition on Advanced Ceramics & Composites, Cocoa Beach, Florida, USA, 25-30.01.2004. Volltext nicht online.

Schüle, Chan Yong and Rossignol, Karl-Stephane (2012) A separated flow model for semi-empirical prediction of trailing edge noise. 18. DLRG-Fach-Symposium, 6.-7. Nov. 2012, Stuttgart, Deutschland. Volltext nicht online.

Schülein, E. (2002) Experimentelle Untersuchungen zur Längswirbelbildung in turbulenten Überschallströmungen mit Ablösung. DLR-Interner Bericht. 224 - 2002 A 12. 32 S. Volltext nicht online.

Schülein, E. (2003) Development and Application of the Thin Oil Film Technique for Skin Friction Measurements in the Short-Duration Hypersonic Wind Tunnel. Springer-Verlag. 13. DGLR-Fach-Symposium der STAB, TU München, 12.-14. November 2002. Volltext nicht online.

Schülein, E. (2003) Optical skin friction measurements in the short-duration Ludwieg tube facility. 20th International Congress on Instrumentation in Aerospace Simulation Facilities, Göttingen, Germany, 25-29 August 2003. ISBN 0-7803-8149-1. Volltext nicht online.

Schülein, E. (2003) Aerodynamisches Auslegungs- und Optimierungstool für isolierte Gitterflügel "FastGRIDS". 11.STAB-Woprkshop, DLR Göttingen, 04.-05.11.2003. Volltext nicht online.

Schülein, E. (2004) Optical Skin Friction Measurements in Shorts-duration Facilities (Invited). In: AIAA Aerodynamic Measurement Technology and Ground Gesting Conference, pp. 1-18. 24th AIAA, Portland, Oregon, 28 June - 1 July 2004. Volltext nicht online.

Schülein, E. and Zheltovodov, A.A (1998) Development of experimental methods for the hypersonic flows studies in Ludwieg tube. In: Proceedings, ICMAR, Part 1, pp. 191-199. IX International Conference on Methods of Aerophysical Research , 29 June – 3 July 1998, Novosibirsk, Russia. Volltext nicht online.

Schülein, E. and Zheltovodov, A.A. (2001) Documentation of Experimental Data for Hypersonic 3-D Shock Waves. DLR-Interner Bericht. 99 A 26. 95 S. Volltext nicht online.

Schülein, Erich and Koch, Stefan and Rosemann, Henning (1998) Skin friction measurement and transition detection techniques for the Ludwieg-Tubes. In: Advanced Aerodynamic Measurement Technology, CP 601, 23-1-23-9. AGARD. DLR / AGARD FDP Symp. “Advanced Aerodynamic Measurement Technology, Seattle, USA, September 22-25, 1997, 1997-09-22 - 1997-09-25, Seattle, USA. Volltext nicht online.

Schütte, A. and Einarsson, G. and Madrane, A. and Schöning, B. and Mönnich, W. and Krüger, W.-R. (2002) Numerical Simulation of Manoeuvring Aircraft by CFD Aerodynamic and Flight-Mechanic Coupling. RTO-AVT Symposium 2002, Paris (fr), 22.-24.04.2002. Volltext nicht online.

Schütte, A. and Einarsson, G. and Schöning, B. and Mönnich, W. (2001) Numerical Simulation of Manoeuvring Aircraft by Aerodynamic and Flight-Mechanic Coupling. CEAS Conference on Multidisciplinary Aircraft design And Optimization, Köln (de), 25.-27.06.2001. Volltext nicht online.

Schütte, Andreas and Cummings, Russel M. and Loeser, Thomas and Vicroy, Dan D. (2009) Integrated Computational/Experimental Approach to UCAV and Delta-Canard Configurations Regarding Stability & Control. 4th Symposium on Integrating CFD and Experiments in Aerodynamics, 14-16 Sept. 2009, Brüssel, Belgien. Volltext nicht online.

Schütte, Andreas and Einarsson, Gunnar and Schöning, Britta and Alrutz, Thomas and Mönnich, Wulf and Neumann, Jens and Heinecke, Jörg (2004) Numerical simulation of maneuvering combat aircraft. 14th DGLR-Symposium of STAB, Bremen, Germany, 92, pp. 103-111. Springer-Verlag. Volltext nicht online.

Schütte, Andreas and Hanke, Michael (2009) Untersuchungen von UAV Technologien im DLR. Unmanned Vehicles II, 3.-4. Februar 2009, Bad Godesberg, Deutschland.

Schütte, Gerrit and Gülhan, Ali (2005) Experimentelle Ermittlung der Strömungsverhältnisse an Querschubsteuerungsdüsen. DLR-Interner Bericht. DLR-IB 32418-2005A07. 77 S. Volltext nicht online.

Schütte, Andreas (2009) Analyses and Assessment of the Aerodynamic Behavior of Tests with High Swept Aircraft in DNW Wind Tunnels. EWA - Demo-Workshop “Dynamic Wind Tunnel Testing”, 28.-30. April 2009, Göttingen, Deutschland.

Schütte, Andreas (2015) Wirbelströmungen an gepfeilten Flügeln mit runden Vorderkanten. DLR-Forschungsbericht. DLR-FB--2015-40. Dissertation. DLR. 180 S.

Schütte, Andreas and Cummings, Russel M. and Stern, Fredericke and Toxopeus, Serge (2009) SUMMARY OF AVT-161, LESSONS LEARNED AND THE WAY AHEAD. NATO RTO - Research and Technology Organisation. [Other] Volltext nicht online.

Schütte, Andreas and Einarsson, Gunnar and Raichle, Axel and Schöning, Britta and Alrutz, Thomas and Mönnich, Wulf and Neumann, Jens and Arnold, Jürgen and Heinecke, Jörg and Forkert, Tomas and Schumann, Holger (2005) Prediction of the Unsteady Behavior of Maneuvering Aircraft by CFD Aerodynamic, Flight-Mechanic and Aeroelastic Coupling. RTO-AVT-MP-123 - Flow-Induced Unsteady Loads and the Impact on Miltary Applications, 2005-04-25 - 2005-04-28, Budapest, Ungarn. Volltext nicht online.

Schütte, Andreas and Hummel, Dietrich and Hitzel, Stephan M. (2009) FLOW PHYSICS ANALYSES ON THE UCAV SACCON CONFIGURATION USING AN INTEGRATED COMPUTATIONAL AND EXPERIMENTAL APPROACH. NATO RTO - Research and Technology Organisation. [Other] Volltext nicht online.

Schütte, Andreas and Lüdeke, Heinrich (2009) NUMERICAL SOLUTIONS FOR THE VFE-2 CONFIGURATION ON UNSTRUCTURED GRIDS AT DLR, GERMANY. NATO RTO - Research and Technology Organisation. [Other] Volltext nicht online.

Schütte, Andreas and Oehlke, Martin and Boelens, Okko J. and Jirásek, Adam (2009) PREDICTION OF THE FLOW AROUND THE X-31 AIRCRAFT USING THREE DIFFERENT CFD METHODS. NATO RTO - Research and Technology Organisation. [Other] Volltext nicht online.

Seifert, A. and Theofilis, V. and Joslin, R. (2002) Issues in Active Flow Control: Theory, Simulation and Experiment. In: Issues in Active Flow Control: : Theory, Simulation and Experiment, 41Seiten-. 1st AIAA Flow Control Conference, June 24-26, 2002, St Louis, MO, USA. Volltext nicht online.

Seitz, A. (2001) Proposal for inflight transition detection. DLR-Interner Bericht. 129-2001/27. Volltext nicht online.

Seitz, A. and Horstmann, K.H. (2002) Propagation of Tollmien-Schlichting Waves in a Wing Boundary Layer. DLR-Interner Bericht. IB 124-2002/43. 12 S. Volltext nicht online.

Seitz, A. and Horstmann, K.H. (2002) Propagation of Tollmien-Schlichting Waves in a Wing Boundary Layer. DFG Abschlusskolloquium des Schwerpunktprogramms SPP1017 Transition, Stuttgart (de), 22.-24.04.2002. Volltext nicht online.

Seitz, A. and Horstmann, K.H. (2003) Propagation of Tollmien Schlichting waves in a wing boundary layer. In: Recent Results in laminar-turbulent transition, 86. Springer Verlag, Berlin, Heidelberg, New York. DFG Abschluß-Kolloquium Schwerpunkt "Transition", Stuttgart (de), 22.-24.04.2002. ISBN 3-540-40490-2. Volltext nicht online.

Seum, Stefan and Heinrichs, Matthias and Henning, Arne and Hepting, Michael and Keimel, Hermann and Matthias, Volker and Müller, Stephan and Neumann, Thorsten and Özdemir, Enver Doruk and Plohr, Martin and Pregger, Thomas and Sanok, Sandra and Sausen, Robert and Seebach, Oliver and Vogel, Bernhard and Winkler, Christian (2015) The DLR VEU-Project Transport and the Environment - building competency for a sustainable mobility future. 4th Conference on Transport, Atmosphere and Climate, TAC-4, 22.-25.06.2015, Bad Kohlgrub, Deutschland. Volltext nicht online.

Shishkina, O. and Wagner, C. (2005) A fourth order accurate finite volume scheme for numerical simulations of turbulent Rayleigh-Benard convection in cylindrical containers. C. R. Mechanique, 333, pp. 17-28. Volltext nicht online.

Sidès, J.; ONERA and Pahlke, K. (2002) Progress towards the CFD Computation of the complete Helicopter: Recent results obtained by research centers in the framework of the franco-german Chance Project. CEAS Aerospace Aerodynamics Research Conference, Cambridge (uk), 10.-12.06.2002. Volltext nicht online.

Siebe, Frank and Gülhan, Ali and Barth, Tarik (2007) Measurement Techniques to Study Flow Phenomena on SHEFEX 1. ODAS-Conference, 2007-10-17 - 2007-10-19, Göttingen (Germany). Volltext nicht online.

Sippel, M. and Klevanski, J. and Burkhardt, H. and Eggers, T. and Bozic, O. and Langholf, P. and Rittweger, A. (2002) Progress in the Design of a Reusable Launch Vehicle Stage. 11th AIAA/AAAF Space Planes and Hypersonic Systems, Orleans (fr), 29.09.-04.10.2002. Volltext nicht online.

Sivadas, V., Instituto Superior Técnico, Lisboa, Portugal, and Pani, B. S., Indian Institute of Technology, Bombay, India, and Bütefisch, K.-A. (2001) Laser Diagnostics of Transverse Turbulent Jets. Journal of Flow Visualization and Image Processing, ISSN 1065-3090, 8 (4), pp. 369-382. Volltext nicht online.

Sobieczky, H. (2000) New Design Concepts for High Speed Air Transport. In: New Design Concepts for High Speed Air Transport National Defence Industry Press. 356-. ISBN 7-118-02511-9/V.184. Volltext nicht online.

Sobieczky, H. (2000) Aerodynamic Design and Optimization Accelerated by Parametric Geometry Tools. ECCOMAS 2000, Barcelona, 11.-14. Sept 2000. Volltext nicht online.

Sobieczky, H. (2002) From Gasdynamic Models to High Speed Design Optimization: A Learning Process. 3rd AIAA Theoretical Fluid Dynamics Conference, St. Louis, MO, 24 - 26 June 2002. Volltext nicht online.

Sobieczky, H. (2002) Inverse Euler Solutions to solve High Speed Aerodynamics Design Problems. WCCM V: 5th World Congress in Computational Mechanics, Vienna, Austria, 7 - 12 Jul 2002. Volltext nicht online.

Sobieczky, H. (2003) IUTAM Symposium Transsonicum IV. In: IUTAM Symposium Transsonicum IV. Fluid Mechanics and its Applications, Vol 73. Kluwer Academic Publishers, Dordrecht-Boston-London. ISBN 1-4020-1608-5. Volltext nicht online.

Sobieczky, H. (2003) Transonic Singularities. Computational Fluid Dynamics Journal, 12 (2), pp. 415-419. Volltext nicht online.

Sobieczky, H. (2004) Geometry and Gasdynamics for Aerodynamic Design. University of California Davis, Course MAE-298. Volltext nicht online.

Sobieczky, H. (2004) Analytical Models for Shocks in Compressible Flow. 21th International Congress of Theoretical and Applied Mechanics, Warsaw, Poland, Aug. 15-21, 2004. Volltext nicht online.

Sobieczky, H. and Dulikravich, G. S. and Dennis, B. H. (2002) Parameterized Geometry Formulation for Inverse Design and Optimization. 4th Int. Conf. on Inverse Problems in Engineering, Angra dos Reis, Brasil, 26-31. 5. 2002. Volltext nicht online.

Sobieczky, H. and Li, P. and Seebass, A.R. (2003) Transonic Methods for the Oblique Flying Wing SST. In: IUTAM Symposium Transsonicum IV Fluid Mechanics and its Applications, Vol 73, 1. Kluwer Academic Publishers, Dordrecht-Boston-London. ISBN 1-4020-1608-5. Volltext nicht online.

Soemarwoto, B.I. and Boelens, O.J. and Fritz, W. and Arthur, M.T. and Ceresola, N. and Bütefisch, K.-A. (2003) Towards the simulation of unsteady manoeuvre dominated by vortical flow. In: AIAA, AIAA 2003-3528, pp. 1-12. American Institute of Aeronautics and Astronautics. 21st AIAA Applied Aerodynamics Conference, June 23-26, 2003, Orlando, Fl, USA. Volltext nicht online.

Spiegel, P. and Buchholz, H. and Splettstößer, W. (2003) The "RONAP" Aeroacoustic Flight Tests with a Highly Instrumented BO 105 Helicopter. 59th Annual Forum of the American Helicopter Society, Phoenix (usa), 06.-08.05.2003. Volltext nicht online.

Stahl, Bernhard and Esch, Helmut and Gülhan, Ali (2007) Experimental investigation of side jet interaction with a supersonic cross flow. Aerospace Science and Technology. Volltext nicht online.

Stanislas, M., LML, Lille, France, and Okamoto, K., University of Tokyo, Japan, and Kähler, C., TU-Braunschweig, (2003) Main results of the first International PIV Challenge. Measurement Science and Technology, PII: S0957-0233(03)54192-3 (14), R63-R89. Volltext nicht online.

Stasicki, B. and Ehrenfried, K. and Dieterle, L. and Ludwikowski, K. and Raffel, M. (2001) Advanced syncronization techniques for complex flow field investigations by means of PIV . 4th Intern. Symposium on Particle Image Velocimetry, Göttingen, Germany, September 17-19, 2001.. Volltext nicht online.

Stasicki, B. and Frahnert, H. (2004) SICHTBARMACHUNG UND AUFZEICHNUNG DER SCHALLWELLENAUSBREITUNG BEIM SCHUSS AUS EINER FEUERWAFFE. In: Vortrag. 83. Jahrestagung der Deutschen Gesellschaft für Rechtsmedizin, Göttingen, 22.-25. September 2004. Volltext nicht online.

Stasicki, B. and Kompenhans, J. (2004) THE MULTI-CAMERA VIDEO STROBOSCOPE –A VERSATILE INSTRUMENT FOR IMAGE BASED MEASUREMENT TECHNIQUES. In: ISFV11 2004 Flow Visualization, pp. 1-10. 11TH INTERNATIONAL SYMPOSIUM ON FLOW VISUALIZATION August 9-12, 2004, University of Notre Dame, Notre Dame, Indiana, USA. ISBN 0-9533991-5. Volltext nicht online.

Stasicki, B. and Pallek, D. and Otter, D. and Bütefisch, K.-A. and Kompenhans, J. (2002) The Use of Non-Standard Video Techniques for Qualitative and Quantitative Flow Visualization. In: CD ROM Proceedings The 10th International Symposium on Flow Visualization. The 10th International Symposium on Flow Visualization, August 26-29, 2002, Kyoto, Japan. Volltext nicht online.

Stasicki, Boleslaw (2003) Investigation of fast, repetitive events by means of non-standard video techniques. In: 7th International Symposium on Fluid Control, Measurement and Visualization (FLUCOME) 2003, 7Seiten. 7th International Symposium on Fluid Control, Measurement and Visualization (FLUCOME), 2003-08-25 - 2003-08-28, Sorrento (Italy). ISBN 0-9533991-4-1. Volltext nicht online.

Stasicki, Boleslaw and Abel, B. and Charvat, A. and Faubel, M. (2004) Visualization of laser-induced liquid micro-jet disintegration by means of high-speed video stroboscope. In: 26th International Congress on High-Speed Photography and Photonics. 26th International Congress on High-Speed Photography and Photonics, 2004-09-19 - 2004-09-24, Alexandria, Virginia (USA). Volltext nicht online.

Stechow, L. and Herr, M. (2001) Effect of Landing Flap Blowing on Side-Edge-Noise Radiation. In: CD-Proceedings. International Congress and Exhibition on Noise Control Engineering (inter noise) 2001, The Hague (nl), 27.-30.08.2001. Volltext nicht online.

Stock, H.W. (2001) Transitionsbestimmung an unendlich langen, schiebenden Flügeln mit Hilfe gekoppelter Navier-Stokes (RANS)und e* Methode. STAB-Workshop, Göttingen (de), 14.-16.11.2001. Volltext nicht online.

Stock, H.W. (2002) Airfoil Validation Using Coupled Navier-Stokes and e*Transition Prediction Methods. Journal of Aircraft, 39 (1), pp. 51-58. Volltext nicht online.

Stock, H.W. (2002) Windtunnel-flight correlation for laminar wings in adiabatic and heating flow conditions. Aerospace Science & Technology, 6 (4), pp. 245-257. Volltext nicht online.

Stock, H.W. and Seitz, A. (2004) Crossflow-Induced Transition Prediction Using Coupled Navier-Stokes and e(N) Method Computations. AIAA-Journal, 42 (9), pp. 1746-1754. Volltext nicht online.

Stock, H.W. and Wild, J. (2002) Feasibility Study for Navier-Stokes Infinite Swept Wing High-Lift RANS Computations with eN Transition Prediction. DLR-Interner Bericht. 124-2002/24. 32 S. Volltext nicht online.

Stock, Hans-W. (2006) e<sup>n</sup> Transition Prediction in Three-Dimensional Boundary Layers on Inclined Prolate Spheroids. AIAA Journal, 44 (1), pp. 108-118. AIAA. ISSN 0001-1452. Volltext nicht online.

Streit, T. (2004) Analysis of Benchmark Low Speed wind Tunnel Test Data: PIV Wake Analysis. DLR-Interner Bericht. 124-2004/6. 58 S. Volltext nicht online.

Streit, T. and Ronzheimer, A. and Büscher, A. (2004) Blind Test Case Data, Technical Note M-DAW. DLR-Interner Bericht. 124-2004/904. 38 S. Volltext nicht online.

Streit, T. and Ronzheimer, A. and Büscher, A. (2004) Numerical Analysis of Transport Aircraft using different Wing Tip Devices. DGLR/STAB Symposium, Bremen (de), 16.-18.11.2004. Volltext nicht online.

Streit, T. and Rudnik, R. (2002) 2D Navier-Stokes-Nachrechnungen von Mini-Trailing Edge Devices im Niedriggeschwindigkeitsbereich. DLR-Interner Bericht. IB 129-2002/4. 57 S. Volltext nicht online.

Streit, T. and Wichmann, G. and Kreuzer, P. (2001) Aerodynamische Analyse von Flügelspitzenerweiterungen der Envoy 7 im Reiseflug. 10. STAB Workshop, Göttingen (de), 14.-15.11.2001. Volltext nicht online.

Streit, T. and Wichmann, G. and Weddig, T. (2001) Aerodynamische Untersuchung verschiedener Flügelseitenkanten-Erweiterungen der Envoy 7. DLR-Interner Bericht. 129-01/16. 42 S. Volltext nicht online.

Struijs, R. and Jonville, G. and Darracq, D. and Heinrich, R. (2003) Inviscid Computation of Effect of Wake Vortices on a Scale-Model Airplane. AIAA Journal, 40 (1), pp. 100-109. Volltext nicht online.

Strüber, H. and Hepperle, M. (2004) CFD-Analysis of the Flying Wing Configuration VELA1 with FLOWer and TAU. DLR-Interner Bericht. 124-2004/17. 32 S. Volltext nicht online.

Strüber, H. and Hepperle, M. (2004) Aerodynamic Optimization of a Flying Wing Transport A/C. DGLR/STAB Symposium, Bremen (de), 16.-18.11.2004. Volltext nicht online.

Stuff, R. and Dieterle, L. and Horstmann, K.-H. and Pailhas, G. and Coton, P. and Lozier, J.-F. (2001) Near- to Midfield-Wake: Experimental Characterisation. In: 3rd ONERA-DLR Aerospace Symposium ODAS 2001, S2-1-5Seiten. 3rd ONERA-DLR Aerospace Symposium, Paris, 20.-22. Juni 2001. ISBN 2-7257-006-X. Volltext nicht online.

Stuff, R. and Vollmers, H. (2002) Aircraft with Means for a Premature Breakdown of the Wing Vortex Pair. Other. US 6,422,518 B1. United States Patent Office. 10 S. Volltext nicht online.

Stuff, R. and Vollmers, H. (2001) Flugzeug mit mindestens einem Wirbelgenerator je Tragflügel zum Reduzieren der Wirbelstärke der Flügelhauptwirbel. Other. DE 199 09 190 C 2. Deutsches Patent- und Markenamt. 18 S. Volltext nicht online.

Stuff, R. and Vollmers, H. (2002) Flugzeug mit Mitteln zum Reduzieren der Wirbelstärke des Flügelhauptwirbelpaars. Other. DE 199 50 403 C 2. Deutsches Patent- und Markenamt. 12 S. Volltext nicht online.

Stumpf, E. (2002) Numerical Study of Four-Vortex Aircraft Wakes. EuroMech Kolloquium No. 433, Aachen (de), 21.03.2002. Volltext nicht online.

Stumpf, E. (2002) Numerical Study of Four-Vortex Aircraft Wakes. 13. DGLR-Fachsymposium der AG STAB 2002, München (de), 12.-14.11.2002. Volltext nicht online.

Stumpf, E. (2004) Numerical Study of Four-Vortex Aircraft Wakes. In: New Results in Numerical and Experimental Fluid Mechanics IV, Vol. 87, pp. 10-17. Springer Verlag, Berlin, Heidelberg, New York. 13th STAB/DGLR Symposium, München (de), 12.-14.11.2002. ISBN 3-540-20258-7. Volltext nicht online.

Stumpf, E. and Hepperle, M. and Darracq, D.; CERFACS and Meese, E.A.; CFD Norway and Elphick, G.; BAe Airbus UK and Galpin, S.; BAe Airbus UK (2002) Benchmark Test for Euler Calculations of a High Lift Configuration Vortex Wake. 40th AIAA Aerospace Science Meeting & Exhibit, Reno (usa), 14.-17.01.2002. Volltext nicht online.

Stumpf, E. and Rakowitz, M. and Lekemark, L. (2003) Numerical Investigation of Flow Separation on an Isolated A400M Landing Gear Door. DLR-Interner Bericht. IB 124-2003/32. Volltext nicht online.

Stumpf, E. and Vollmers, H. and Bao, F. (2005) C-Wake Report DLR-F11 Tests in DNW-NWB and DNW-LLF 5-Hole Probe PIV Results. DLR-Interner Bericht. 224-2003 C 20. 21 S. Volltext nicht online.

Stürmer, A. (2004) Instationäre Euler und Navier-Stokes Simulationen von Propeller-Strömungen mit dem unstrukturierten DLR TAU-Code. 14. DGLR-Fachsymposium der AG STAB, Bremen (de), 16.-18.11.2004. Volltext nicht online.

Stürmer, A. (2004) Validation of an Unstructured Chimera Grid Approach for the Simulation of Propeller Flows. 22nd Applied Aerodynamics Conference, Providence (usa), 16.-19.08.2004. Volltext nicht online.

Stürmer, A. (2004) Unsteady Euler Computations of an Isolated Propeller using the DLR TAU-code. DLR-Interner Bericht. 124-2004/21. 52 S. Volltext nicht online.

Stürmer, Arne and Yin, Jianping (2010) Aerodynamic and Aeroacoustic Analysis of Contra-Rotating Open Rotor Propulsion Systems at Low-Speed Flight Conditions. New Results in Numerical and Experimental Fluid Mechanics VII, 112. Springer Verlag. ISBN 978-3-642-14242-0. ISSN 1612-2909. Volltext nicht online.

Stürmer, Arne and Yin, Jianping (2008) Aerodynamic and Aeroacoustic Analysis of Contra-Rotating Open Rotor Propulsion Systems at Low-Speed Flight Conditions. 16. DGLR/STAB-Symposium, 2008-11-03 - 2008-11-04, Aachen. (Unpublished) Volltext nicht online.

Stürmer, Arne and Yin, Jianping (2009) Coupled CFD-CAA Simulations for the Airbus A400M Propeller 15.01 Validation Case. DLR-Interner Bericht. IB 124-2009/908. 34 S. Volltext nicht online.

Swanson, Charles R. and Turkel, Eli and Rossow, Cord-Christian and Vatsa, Veer N. (2006) Convergence Acceleration for Multistage Time-Stepping Schemes. 36th AIAA Fluid Dynamics Conference, 2006-06-05 - 2006-06-09, San Francisco, CA (USA). Volltext nicht online.

Swanson, Ray Charles and Rossow, Cord-Christian (2009) An efficient Flow Solver with a Transport Equation for Modeling Turbulence. In: AIAA Paper (2009-3665). 19th AIAA Computational Fluid Dynamics Conference, Juni 2009, San Antonio, Texas, USA. Volltext nicht online.

T

Tang, W. and Orlowski, M. and Longo, J.M.A. and Giese, P. (2001) Aerodynamic optimization of re-entry capsules. Aerospace Science and Technology, 5 (1), pp. 15-25. Volltext nicht online.

Theofilis, V. (2005) Direct Numerical Simulation of the roll-up process of trailing-vortex system, using experimentally obtained data at realistic Reynolds numbers. DLR-Interner Bericht. 224-2004 C 12. 49 S. Volltext nicht online.

Theofilis, V. and Fedorov, A. and Obrist, D. and Dallmann, U.C. (2003) The extended Görtler-Hämmerlin model for linear instability in the three-dimensional incompressible swept attachment line boundary layer. Journal of Fluid Mechanics, 487, pp. 271-313. Volltext nicht online.

Theofilis, V. and Sherwin, S.J. (2001) Global instabilities in trailing-edge laminar separated flow on a NACA 0012 Airfoil. 15th ISABE (International Symposium on Airbreathing Engines), Bangalore, India, September 2-7, 2001.; Conf.-Paper: ISABE-2001-1094.. Volltext nicht online.

Trenker, M. (2003) Design Conceptes for Adaptive Airfoils with Dynamic Transonic Flow Control. Journal of Aircraft, 40 (4), pp. 734-740. Volltext nicht online.

Trenker, M. and Sobieczky, H. (2002) Using the Gasdynamic Knowledge Base for Aerodynamic Design and Optimization in the Transonic Regime. In: Inverse Problems in Engineering Mechanics 1, 3. Elsevier Science, Oxford. ISBN 0-08-043951-9. Volltext nicht online.

Trenker, M.,, and Hannemann, M. and Sobieczky, H. (2003) Parameterized Geometries for Configuration Adaptation. In: IUTAM Symposium Transsonicum IV Fluid Mechanics and its Applications, Vol 73, 1. Kluwer Academic Publishers, Dordrecht-Boston-London. ISBN 1-4020-1608-5. Volltext nicht online.

Turkel, Eli and Vatsa, Veer N. and Swanson, Charles R. and Rossow, Cord-Christian (2006) Convergence Acceleration for the Three-Dimensional Compressible Navier-Stokes Equations. In: Proceedings of European Conference on Computational Fluid Dynamics (ECCOMAS). ECCOMAS 2006, 2006-09-05 - 2006-09-08, Egmond aan Zee (NL). Volltext nicht online.

U

Ullman, T. and Gülhan, A. and Hald, H. and Schneider, H. (2004) Atmospheric Re-Entry Flight and Ground Testing Experience with Coated and Uncoated C/C-SiC Composites. Fifth International Conference on High Temperature Ceramic Matrix Composites (HTCMC-5), Seattle, Washington, USA, 12–16.09.2004. Volltext nicht online.

V

Vaculin, O. and Valasek, M. and Kortüm, W. (2003) Multi-Objective Semi-Active Truck Suspension by Spatial Decomposition. In: The Dynamics of Vehicles on Roads and on Tracks, 37, pp. 432-440. Swets & Zeitlinger. 17th IAVSD Symposium, Denmark, 20-24 August 2001. ISBN 90-265-1945-1. Volltext nicht online.

Vassberg, John and Tinoco, Edward and Mani, Mori and Brodersen, Olaf and Eisfeld, Bernhard and Wahls, Richard and Morrison, Joseph and Zickuhr, Tom and Laflin, Kelly and Mavriplis, Dimitri (2006) Summary of the Third AIAA CFD Drag Prediction Workshop. In: 45th AIAA Aerospace Science Meeting and Exhibit. 45th AIAA Aerospace Science Meeting and Exhibit, 2007-01-08 - 2007-01-11, Reno, NV (USA). (Submitted) Volltext nicht online.

Vicroy, Dan D. and Löser, Thomas and Schütte, Andreas (2009) SACCON UCAV FORCED OSCILLATION TESTS AT DNW-NWB AND NASA LANGLEY 14ft × 22ft TUNNEL. NATO RTO - Research and Technology Organisation. [Other] Volltext nicht online.

Visingardi, A. and Decours, J. and Khier, W. and Voutsinas, S. (2005) Code-to-Code Comparison for the Blind-Test Activity of the Tiltaero Project. 31st European Rotorcraft Forum, Florenz (it), 13.-15.09.2005. Volltext nicht online.

Visingardi, A. and Khier, W. and Decours, J. (2004) The Blind Test Activity of TILTAERO Project for the Numerical Aerodynamic Investigation of a Tiltrotor. ECCOMAS, Jyväskylä (fi), 24.-28.07.2004. Volltext nicht online.

Visingardi, Antonio and Dummel, Andreas and Falchero, Daniele and Pidd, Mike and Prospathopoulos, John and Voutsinas, Spyros G and Yin, Jianping (2006) AERODYNAMIC INTERFERENCE IN FULL HELICOPTER CONFIGURATIONS: VALIDATION USING THE HELINOVI DATABASE. In: European Rotorcraft Forum. 32st ERF 2006, AE19, 2006-12-09 - 2006-14-09, Maastricht (NL). Volltext nicht online.

Vollmers, H. and Bao, F. and Castagno, G., INSEAN, and Mattner, H. (2002) Measurement on interaction and stability of four vortex wakes. In: CD of Colloquium. Kolloquium No. 433, Aachen, 21.03.2002. Volltext nicht online.

Vollmers, H. and Bao, F. and Mattner, H. (2004) DLR Projekt Wirbelschleppe II HAP1. Projekttreffen, 15.07.2004, DLR Oberpfaffenhofen. Volltext nicht online.

Vollmers, H. and Puffert-Meissner, W. and Schröder, A. (2004) Analysis of PIV Flow Field Measurements behind the ALVAST-Model in High-Lift Configuration. 14th DGLR-Fach-Symposium der STAB, Bremen, November 16-18, 2004. Volltext nicht online.

Vollmers, H. and Schröder, A. and Gilliot, A. and Monnier, J.-C. and Lozier, J.-F. (2003) Erfassung des Geschwindigkeitsfeldes im Nachlauf frei fliegender Modelle mit PIV. 11. STAB Workshop, DLR, Göttingen, 04.11.-06.11.2003. Volltext nicht online.

Voß, Guido (2008) Comparison of AGU and UBV intakes with different duct widths on A330-200 ECS. DLR-Interner Bericht. DLR-IB 124-2008/918. 12 S. (Unpublished) Volltext nicht online.

Voß, Guido (2008) Numerical investigations for an optimal mounting position of intakes for the air conditioning unit. STAB, 2008-11-03 - 2008-11-04, Aachen (Deutschland). (Submitted) Volltext nicht online.

van der Wall, Berend G. and Burley, C.L. and Yu, Y. and Richard, H. and Pengel, K. and Beaumier, P. (2004) The HART II Test - Measurement of Helicopter Rotor Wakes. Aerospace Science and Technology, 8 (4), pp. 273-284. Volltext nicht online.

van der Wall, Berend G. and Junker, B. and Burley, C.L. and Brooks, T.F. and Yu, Y. and Tung, C. and Raffel, M. and Richard, H. and Wagner, W. and Mercker, E. and Pengel, K. and Holthusen, H. and Beaumier, P. and Delrieux, Y. (2002) The HART II Test in the LLF of the DNW - a Major Step towards Rotor Wake Understanding. In: 28th European Rotorcraft Forum Proceedings, 42.1-42.16. 28th European Rotorcraft Forum, Bristol (uk), 17-20 September 2002. Volltext nicht online.

von Geyr, H. and Brodersen, O. and Melber, S. (2001) Engine Integration on Transport Aircraft - The European Research Activities on Propulsion Airframe Integration. In: Book of Abstracts - ECCOMAS CFD 2001, 34-. ECCOMAS Computational Fluid Dynamics Conference 2001, Swansea (gb), 04.-07.09.2001. ISBN 0905091116. Volltext nicht online.

W

Wagner, Claus and Friedrich, R. (2004) Direct numerical simulation of momentum and heat transport in idealized Czochralski crystal growth configurations. International Journal of Heat and Fluid Flow, 25, pp. 431-443. Volltext nicht online.

Wagner, Claus and Friedrich, Rainer (2005) DNS of Turbulent Flows in Idealized Czochralski Crystal Growth Configurations. In: Notes on Numerical Fluid Mechanics Vieweg. pp. 172-190. Volltext nicht online.

Wagner, Claus and Friedrich, Rainer (2000) DNS of turbulent flow along passively permeable walls. International Journal of Heat and Fluid Flow, 29, pp. 489-498. Volltext nicht online.

Weihs, H. and Longo, J.M.A. and Gülhan, A. (2002) The Sharp Edge Flight Experiment SHEFEX. 4th European Workshop on Hot Structures and Thermal Protection System for Space Vehicles, Palermo (it), 25.-29.11.2002. Volltext nicht online.

Weihs, Hendrik and Turner, John and Longo, Jose Maria (2008) The Sharp Edge Flight Experiment SHEFEX II, a Mission Overview and Status. AIAA International Space Planes and Hypersonic Systems nad Technologies Conference, 2008-04-28 - 2008-05-01, Dayton, OH (USA).

Weihs, Hendrik and Turner, John and Longo, Jose Maria (2008) Key Experiments within the Shefex II Mission. IAC 2008, 2008-09-28 - 2008-10-3, Glasgow, Scottland UK.

Weiland, C. and Longo, J.M.A. and Gülhan, A. and Decker, K. (2002) Aerothermodynamics for Reusable Launch Systems. Deutscher Luft- und Raumfahrtkongress 2002, Stuttgart (de), 23.-26.09.2002. Volltext nicht online.

Weiland, C. and Longo, J.M.A. and Gülhan, A. and Decker, K. (2004) Aerothermodynamics for reusable launch systems. Aerospace Science and Technology, 8 (2), pp. 101-110. Volltext nicht online.

Weiland, M.K.H. and Johnston, I.A. and Martinez Schramm, J. and Hannemann, K. (2001) ARD Post-Flight Analysis , Numerical Simulation and Experiments at HEG. DLR-Interner Bericht. 223-2001 A 10. 77 S. Volltext nicht online.

Wichmann, G. (2004) Demonstratorexperiment zu 3D-Strömungskontrolle. Jahres-Review-Meeting "Innovative Hochauftriebskonfigurationen", Bremen (de), 28.-29.09.2004. Volltext nicht online.

Wichmann, G. (2004) The objectives of DLR's ForMEx project. European Windtunnel Association Initial Joint Workshop, Toulouse (fr), 18.-20.10.2004. Volltext nicht online.

Wicke, Kai and Kruse, Martin and Linke, Florian and Gollnick, Volker (2014) Impact of insect contamination on operational and economic effectiveness of aircraft with natural flow technology. In: 29th Congress of the International Council of the Aeronautical Sciences (ICAS). 29th Congress of the International Council of the Aeronautical Sciences (ICAS), 07.-12. September 2014, St. Petersburg, Russland.

Widhalm, M. and Rossow, C.-C. (2002) Improvement of upwind schemes with the Least Square method in the DLR TAU Code. In: New Results in Numerical and Experimental Fluid Mechanics IV. Springer Verlag. 13. DGLR-Fach-Symposium AG STAB, München (de), 12.-14.11.2002. ISBN 3-540-20258-7. Volltext nicht online.

Widhalm, Markus and Ronzheimer, Arno and Meyer, Joerg (2008) Lagrangian Particle Tracking on Large Unstructured Three-Dimensional Meshes. American Institute of Aeronautics and Astronautics. 46th AIAA Aerospace Sciences Meeting and Exhibit, [2008-01-07 - 2008-01-10] AIAA Reno 472, Reno, Nevada, U.S.A..

Wiedemann, A. and Möller, T. J. (2002) Measurement of a swirling pipe and combustion chamber flow by means of multi-component Laser Doppler Velocimetry. In: Engineering Turbulence Modelling and Experiments 5 5th International Symposium on Engineering Turbulence Modelling and Measurements, Mallorca, Spain, 16.-18. September 2002, Proceedings. ELSEVIER. ISBN 0-08-044114-9. Volltext nicht online.

Wild, J. (2001) Numerische Optimierung von zweidimensionalen Hochauftriebskonfigurationen durch Lösung der Navier-Stokes-Gleichungen. DLR-Forschungsbericht. 2001-11. Dissertation. 122 S. Volltext nicht online.

Wild, J. (2002) Geometriemodellierung und Parameteridentifikation für den Hochauftriebsflügel. Workshop "Geometriemodellierung" des DGLR Fachausschuß Numerische Aerodynamik, Braunschweig (de), 08.05.2002. Volltext nicht online.

Wild, J. (2002) On the Potential of Numerical Optimization of High-Lift Multi-Element Airfoils based on the Solution of the Navier-Stokes-Equations. 2nd International Conference on Computational Fluid Dynamics, Sydney (aus), 15.-19.07.2002. Volltext nicht online.

Wild, J. (2002) Validation of Numerical Optimization of High-Lift Multi-Element Airfoils based on Navier-Stokes-Equations. 20th Applied Aerodynamics Conference, St. Louis (usa), 24.-26.06.2002. Volltext nicht online.

Wild, J. (2001) Validierung der numerischen Optimierung für Mehr-Elemente-Profile. 10. AG STAB-Workshop, Göttingen (de), 14.-16.11.2001. Volltext nicht online.

Wild, J. (2004) Acceleration of Aerodynamic Optimization Based on RANS-Equations by Using Semi-Structured Grids. ERCOFTAC Design Optimization: Methods & Applications, Athen (gr), 31.03.-02.04.2004. Volltext nicht online.

Wild, J. (2003) On the Potential of Numerical Optimization of High-Lift Multi-Element Airfoils based on the Solution of the Navier-Stokes-Equations. In: Computational Fluid Dynamics 2002, pp. 267-273. ICCFD II 2002, Sydney (aus), 15.-19.07.2002. ISBN 3-540-00739-3. Volltext nicht online.

Wild, J. (2004) Multi Objective Constrained Optimization and High Lift Device Applications. Other. ISBN 2-930389-56-7. von Karman Institut. 44 S. Volltext nicht online.

Wild, J. and Herrmann, U. (2003) Designing High-Lift Systems for Low Drag. Other. VKI LS 2003-02. VKI. 45 S. Volltext nicht online.

Wild, J. and Herrmann, U. (2003) Designing High-Lift Systems for Low Drag. Lecture in Series: CFD-based Aircraft Drag Prediction and Reduction, Brüssel (b), 03.-07.02.2003. Volltext nicht online.

Wild, J. and Niederdrenk, P. and Gerhold, T. (2005) Marching Generation of Smooth Structured and Hybrid Meshes Based on Metric Identity. Proceedings of the 14th International Meshing Roundtable, pp. 109-127. Springer Verlag Berlin Heidelberg. ISBN 3-540-25137-5. Volltext nicht online.

Wild, J. and Puffert-Meißner, W. and Sitzmann, M. and Lekemark, L. (2003) Messung des FNG Hochauftriebs-Modells bei hohen Reynoldszahlen im Kryogenischen Windkanal Köln. DLR-Interner Bericht. IB 124-2003/37. 126 S. Volltext nicht online.

Wild, J. and Schmidt, O.T. and Stürmer, A. (2004) Prediction of attachment line transition for a high-lift wing based on two-dimensional flow calculations with RANS-solver. Springer Verlag. (In Press) Volltext nicht online.

Wilhelm, R. (2002) An Inverse Design Method for the Design of Isolated and Wing-Mounted Engine Nacelles. DLR-Interner Bericht. 129-01/19. 38 S. Volltext nicht online.

Wilhelm, R. (2002) Inverse Design Method for Designing Isolated and Wing-Mounted Engine Nacelles. AIAA Journal of Aircraft, 39 (6), pp. 989-995. Volltext nicht online.

Wilhelm, R. (2002) An Inverse Design Method for Designing Isolated and Wing-Mounted Engine Nacelles. 40th Aerospace Sciences Meeting and Exhibit, Reno (usa), 14.-17.01.2002. Volltext nicht online.

Wilhelm, R. (2002) Integrated Design of Installed Engine Nacelles Using an Inverse Design Method. 13. DGLR-Fachsymposium der AG STAB 2002, München (de), 12.-14.11.2002. Volltext nicht online.

Wilhelm, R. (2004) Integrated Design of Installed Engine Nacelles Using an Inverse Design Method. In: New Results in Numerical and Experimental Fluid Mechanics IV, Vol. 87, pp. 66-73. Springer Verlag, Berlin, Heidelberg, New York. 13th STAB/DGLR Symposium, München (de), 12.-14.11.2002. ISBN 3-540-20258-7. Volltext nicht online.

Wilke, Gunther (2012) Variable Fidelity Optimization of Required Power of Rotor Blades: Investigation of Aerodynamic Models and their Application. 38th European Rotorcraft Forum 2012, 04-07 Sep 2012, Amsterdam, Netherlands.

Windte, J. and Radespiel, R. and Scholz, U. and Eisfeld, B. (2005) RANS Simulation of the Transitional Flow Around Airfoils at Low Reynolds Numbers for Steady and Unsteady Onset Conditions. In: Proceedings auf CD. RTO AVT Specialists Meeting on "Enhancement of NATO Military Flight Vehicle Performance by Management of Interacting Boundary Layer Transition and Separation", Prag (cz), 04.-07.10.2004. Volltext nicht online.

Wucherpfennig, Jens and Dillmann, Andreas and Loose, Sigfried (2010) Sicher durch den Tunnel: DLR nimmt weltweit einzigartiges Katapult für Hochgeschwindigkeitszüge in Betrieb. [Other] Volltext nicht online.

Wunderlich, Tobias and Dähne, Sascha and Heinrich, Lars and Reimer, Lars (2015) Multidisciplinary Optimization of a NLF Forward Swept Wing in combination with Aeroelastic Tailoring using CFRP. Deutscher Luft- und Raumfahrtkongress 2015, 22.-24. Sept. 2015, Rostock, Deutschland. Volltext nicht frei.

Y

Yin, J. (2001) Simulation of open- and ducted-rotor noise using CAA-Multidomain method. NATO RTO-AVT Symposium on Aging Mechanisms and Control, Part A - Developments in Computational Aero- and Hydro-Acoustics, Manchester (uk), 8.-12. Oktober 2001. Volltext nicht online.

Yin, J. (2001) Acoustic Prediction Using Ffowcs-Williams/Hawkings Formulation Based on CAMRAD Aerodynamic Airload Input. DLR-Interner Bericht. 129-2001/17. 23 S. Volltext nicht online.

Yin, J. (2004) Towards Noise Abatement Flight Procedure Design: DLR Rotorcraft Noise Ground Footprints Model and its Validation. DLR-Interner Bericht. 124-2004/14. 26 S. Volltext nicht online.

Yin, J. (2004) Rotorcraft Noise Ground Footprints Estimation and Preliminary Lower Noise Flight procedure design Using DLR Flight Test Data. DLR-Interner Bericht. 124-2004/19. 21 S. Volltext nicht online.

Yin, J. (2003) Acoustic Prediction Using Ffowcs-Williams/Hawkings Formulation based on a penetrable surface Implementation and validation with analytic solution. DLR-Interner Bericht. 129-2003/8. 30 S. Volltext nicht online.

Yin, J. (2002) Status report on further improvements of APSIM-E: Improvement of Aeroacoustic Program System (APSIM) Prediction Capability. DLR-Interner Bericht. 129-2002/26. 10 S. Volltext nicht online.

Yin, J. (2003) Aeroacoustics Research in Europe: 5.1 Tail Rotor Noise Under Main/Tail Rotor Interaction. Journal of Sound and Vibration, 268 (4), pp. 809-824. Volltext nicht online.

Yin, J. and Buchholz, H. and Splettstößer, W. (2002) Numerical Simulation of Bo105 Main/Tail Rotor Interaction Noise And Preliminary Comparisons with Flight Test Results. 28th European Rotorcraft Forum, Bristol (gb), 17.-20.09.2002. Volltext nicht online.

Yin, J. and Delfs, J. (2001) Acoustic Scattering By Complex Geometry Using CAA-Chimera Method. In: CD-Proceedings "8th International Congress on Sound and Vibration", pp. 717-724. 8th International Congress on Sound and Vibration, Hongkong (vrc), 02.-06. Juli 2001. Volltext nicht online.

Yin, J. and Delfs, J. (2001) Simulation of open- and ducted-rotor noise using CAA-Multidomain method. DGLR-Fachausschuss T2.3 "Strömungsakustik/Fluglärm", Braunschweig (de), 07.12.2001. Volltext nicht online.

Yin, J. and Delfs, J. (2001) Sound Generation from Gust-Airfoil Interaction Using CAA-Chimera Method. In: CD-Proceedings. 7th AIAA/CEAS Aeroacoustics Conference, Maastricht (nl), 28.-30.05.2001. Volltext nicht online.

Yin, J. and Delfs, J. (2002) Aeroacoustics Research in Europe (edited by MJ Fisher and RH Self): 6.3 Research on open- and Ducted Rotor noise using CAA multidomain method. Journal of Sound and Vibration, 258 (1), pp. 1-30. Volltext nicht online.

Yin, J. and Delfs, J. (2000) On Computations of third CAA workshop benchmark problems. 3rd computational aeroacoustics (CAA) workshop on benchmark problems, Ohio (USA), 08.-10.11.1999. Volltext nicht online.

Yin, J. and Delfs, J. (2003) Main/Tail Rotor Interaction under Ground Effect Using DLR 3D Free Wake Code. 29th European Rotorcraft Forum, Friedrichshafen (de), 16.-18.09.2003. Volltext nicht online.

Yin, J. and Delfs, J. (2003) Improvement of DLR Rotor Aeroacoustic Code (APSIM) and its Validation with Analytic Solution. 29th European Rotorcraft Forum, Friedrichshafen (de), 16.-18.09.2003. Volltext nicht online.

Yin, J. and Spiegel, P. and Buchholz, H. (2004) Towards Noise Abatement Flight Procedure Design: DLR Rotorcraft Noise Ground Footprints Model and its Validation. 30th European Rotorcraft Forum, Marseilles (fr), 14.-16.09.2004. Volltext nicht online.

Yin, Jianping (2001) Solving Aeroacoustic Benchmark Problems Using CAA. Institutskolloquium AS, 14. Juni 2001, Braunschweig. Volltext nicht online.

Yin, Jianping (2006) Aeroacoustic and aerodynamic results (DNW test and DLR numerical simulation) EU HELINOVI (HELIcopter NOise and VIbration Reduction). Institutskolloquium, Institut für Aerodynamik und Strömungstechnik (AS), 30. Jan. 2006, Braunschweig. Volltext nicht online.

Yin, Jianping (2006) HELINOVI Aeroacoustic Main/Tail Rotor Test in DNW: Test Documentation and Representative Results. Project Report. Contract No. G4RD-CT-2002-00667 HELINOVI. 132 S. Volltext nicht online.

Yin, Jianping (2006) Report on Noise Reduction Benefits based on HELINOVI Aeroacoustic Main/Tail Rotor Test and Post-Test Prediction Results. Project Report. Contract No. G4RD-CT-2002-00667 HELINOVI. 62 S. Volltext nicht online.

Yin, Jianping (2007) Aeroacoustics research in Europe: The CEAS-ASC report on 2005 highlights (edited by Spyros G. Voutsinas): 7.2. Acoustic and aerodynamic test results from HeliNOVI main rotor/tail rotor/fuselage test in DNW. Journal of Sound and Vibration, Volume 299,Issue 3, pp. 419-459. ISSN 0022-460x. Volltext nicht online.

Yin, Jianping (2006) AEROACOUSTIC TEST RESULTS FROM HELINOVI MAIN ROTOR/TAIL ROTOR/FUSELAGE TEST IN DNW. Other. Volltext nicht online.

Yin, Jianping (2007) CEAS-ASC highlights 2006 (edited by Stephane Caro): 5.1. Analysis of tail rotor noise reduction benefits using HeliNOVI aeroacoustic main/tail rotor test and post-test prediction results. Journal of Sound and Vibration, Volume 304,Issue 3, pp. 434-435. ISSN 0022-460x. Volltext nicht online.

Yin, Jianping (2011) Simulation of Tail Rotor Noise Reduction and Comparison with HeliNovi Wind Tunnel Test Data. 67th Annual Forum of the American Helicopter Society, 3.– 5. May. 2011, Virginia Beach, Virginia (USA). Volltext nicht online.

Yin, Jianping and Buchholz, Heino (2007) Toward noise abatement flight procedure design: DLR rotorcraft noise ground footprints model. Journal of the American Helicopter Society, Volume 52,Issue 2, pp. 90-98. ISSN 0002-8711. Volltext nicht online.

Yin, Jianping and Dummel, Andreas and Falchero, Daniele and Pidd, Mike and Prospathopoulos, John and Visingardi, Antonio and Voutsinas, Spyros G (2006) Analysis of Tail Rotor noise reduction benefits using HELINOVI aeroacoustic main/tail rotor test and posttest prediction results. In: European Rotorcraft Forum. 32st ERF 2005, AC05, 2006-12-09 - 2006-14-09, Maastricht (NL). Volltext nicht online.

Yin, Jianping and van der Wall, Berend G. and Oerlemans, Stefan (2008) Acoustic wind tunnel tests on helicopter tail rotor noise (HeliNOVI). Journal of the American Helicopter Society, 53 (3), pp. 226-239. ISSN 0002-8711. Volltext nicht online.

Yin, Jianping and Stürmer, Arne (2009) CROR low-speed aerodynamic and aeroacoustic analysis (Section 7.1). Journal of Sound and Vibration, 328 (1-2), pp. 213-242. Elsevier. doi: 10.1016/j.jsv.2009.07.022. ISSN 0022-460X. Volltext nicht online.

Yin, Jianping and Stürmer, Arne (2010) Noise radiation from installed pusher propeller using coupling of Unsteady Panel Method, Actuator disk and FW-H methodology. 16th AIAA/CEAS Aeroacoustics Conference 2010, 07.-09. Juni 2010, Stockholm, Schweden. Volltext nicht online.

Yin, Jianping and Stürmer, Arne (2010) Aerodynamic and aeroacoustic analysis of installed pusher propeller aircraft configurations (Section 7.2). Journal of Sound and Vibration, 329, pp. 4824-4825. Elsevier. doi: 10.1016/j.jsv.2010.06.001. ISSN 0022-460X. Volltext nicht online.

Yin, Jianping and Stürmer, Arne (2011) Pylon blowing for the reduction of installation-associated noise of CROR engines (Section 8.2). Journal of Sound and Vibration, 330 (21), pp. 4955-4990. Elsevier. doi: 10.1016/j.jsv.2010.06.001. ISSN 0022-460X. Volltext nicht online.

Yin, Jianping and Stürmer, Arne (2011) Simulation of noise radiation from installed pusher propeller aircraft configurations (Section 8.3). Journal of Sound and Vibration, 330 (21), pp. 4955-4980. Elsevier. doi: 10.1016/j.jsv.2010.06.001. ISSN 0022-460X. Volltext nicht online.

Z

Zeibig, A. and Achilles, S. and Wilde, A. and Sabanca, M. and Delfs, J. (2005) Aeroacoustic Measurements and Validations of Numerical Simulations for the Case of a Generic Vehicle Structure. 12th International Conference on Sound and Vibration, Lissabon (p), 11.-14.07.2005. Volltext nicht online.

Zhang, X. Q. and Knopp, Tobias and Lube, Gerd (2008) Calibration of model and discretization parameters for turbulent channel flow. In: K. Kunisch et al. (eds.), pp. 529-537. Springer Verlag. 7th European Conference on Numerical Mathematics and Advanced Applications, 2007-09-00, Graz ( Austria). Volltext nicht online.

Zheltovodov, A.A. and Maksimov, A.I. and Schülein, E. and Gaitonde, D.V. and Schmisseur, J.D. (2000) Verification of crossing-shock-wave / boundary layer interaction computations with the k –epsilon turbulence model. X International Conference on Methods of Aerophysical Research 9 – 16 July 2000, Novosibirsk, Russia. Volltext nicht online.

Zheltovodov, A.A. and Maksimov, A.I. and Schülein, E. and Knight, D.D. and Thivet, F. and Gaitonde, D.V. (AFRL Wright-Patterson AFB, USA, and Schmisseur, J.D. (AFRL Wright-Patterson AFB, USA, (2001) Experimental and computational studies of crossing-shock-wave / boundary layer interactions. International Conference RDAMM-Novosibirsk, 2001. Volltext nicht online.

Zimper, Dirk (2016) Aerodynamisches Verhalten einer generischen UCAV Konfiguration. DLR-Forschungsbericht. DLR-FB-2015-42. Dissertation. DLR. 239 S. Volltext nicht frei.

Zimper, Dirk and Hitzel, Stephan (2016) WIND TUNNEL AND SIMULATION AND “REAL” FLIGHT OF ADVANCED COMBAT AIRCRAFT – AN INDUSTRIAL PERSPECTIVE. Other. STO-TR-AVT-201. NATO Science & Technology Organization. 26 S. doi: 10.14339/STO-TR-AVT-201. Volltext nicht online.

Zimper, Dirk and Hitzel, Stephan M. (2014) Model Scale and "Real" Flight of Generic UCAV and Advanced Combat Aircraft - An Industrial Perspective. In: 32nd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics. AIAA AVIATION 2014, 16.-20. Jun. 2014, Atlanta, Georgia, USA. ISBN 978-1-62410-288-2. ISSN 2014-2267. Volltext nicht frei.

Zimper, Dirk and Hummel, Dietrich (2016) ANALYSIS OF THE TRANSONIC FLOW AROUND A GENERIC UCAV CONFIGURATION. Other. STO-TR-AVT-201. NATO Science & Technology Organization. 26 S. doi: 10.14339/STO-TR-AVT-201. Volltext nicht online.

Zimper, Dirk and Rein, Martin (2014) Experimental and numerical analysis of the transonic vortical flow over a generic lambda wing configuration. In: 32nd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics. AIAA AVIATION 2014, 16.-20. Jun. 2014, Atlanta, Georgia, USA. ISBN 978-1-62410-288-2. ISSN 2014-2005. Volltext nicht frei.

Zimper, Dirk and Rossow, Cord-Christian and Schütte, Andreas (2016) Luftstreitkräfte der Zukunft – Technologische Herausforderungen und Entwurf zukünftiger bemannter sowie unbemannter Kampfflugzeuge. Mittler Report Verlag GmbH. [Other] Volltext nicht frei.

Ö

Özkaya, Emre and Gauger, Nicolas (2009) Single-Step One-Shot Aerodynamic Shape Optimization. In: International Series of Numerical Mathematics (ISNM) Birkhäuser Basel. pp. 191-204. ISBN 9783764389222. Volltext nicht online.