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

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A

  Adeli, R. and Longo, J.M.A. and Emunds, H. (2004) Flow field study of a supersonic jet exiting into a supersonic stream. Notes on Numerical Fluid Mechanics and Multidisciplinary Design. (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.

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

  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

  Bao, F. (2001) Experimental Investigation of Transitional Unsteady Separated Vortex Flows. Dissertation. DLR-Forschungsbericht. 2001-20, 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. file

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

  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. file

  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. file

  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. file

  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. file

  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. 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. file

  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 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. file

  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.

  Böhning, P. and Koop, Lars and Schulz, M. (2004) Bestimmung der Übertragungseigenschaften des Mikrofons KE4 von Sennheiser. DLR-Interner Bericht. IB 92517-04/B8. 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. file

  Ciobaca, Vlad (2013) Parameter study for a slatless 2D high-lift airfoil with active separation control using a URANS approach. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics VIII, Vol. 1 (10.100). Springer-Verlag. pp. 135-142. ISBN 978-3-642-35679-7. ISSN 1612-2909 file

  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. file

  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. file

  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. file

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. file

  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.

  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. file

  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.

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

  Döring, F. (2004) Synthese von Pyrenfarbstoffen und Untersuchung ihrer O2-druckabhängigen Lumineszenz für die Anwendung als Pressure Sensitive Paint. Dissertation. DLR-Forschungsbericht. 18, 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. Notes on Numerical Fluid Mechanics and Multidisciplinary Design. 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. file

  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. 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. file

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  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.

  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. file

  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. file

  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. file

  Herr, M. (2004) Experimental Study On Noise Reduction Through Trailing Edge Brushes. Notes on Numerical Fluid Mechanics and Multidisciplinary Design. 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. 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.

  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.

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  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. file

  Iniguez de Heredia, A. and Liersch, C. (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. file

  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. file

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  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 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 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.

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  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. file

  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.

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  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, 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. file

  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. Volltext nicht frei. file

  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.

  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. file

  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.

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  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.

  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. file

  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 Ltd.. 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, 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 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 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 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 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 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. Dissertation. DLR-Forschungsbericht. DLR-FB 89-38. Volltext nicht online.

  Rossow, Cord-Christian (1995) Ein Finite-Volumen-Verfahren mit Flußbilanzspaltung zur numerischen Strömungssimulation. Habilitation. DLR-Forschungsbericht. DLR-FB 95-34. 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 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. 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: Notes on Numerical Fluid Mechanics and Multidisciplinary Design Springer-Verlag Berlin Heidelberg. pp. 189-208. 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 (2009) Numerical Simulation - Complementary Theory and Experiment as the Third Pilar in Aerodynamics: Hermann Schlichting - 100 Years. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design Springer-Verlag Berlin Heidelberg. pp. 39-58. ISBN 978 3 450 95997 7. ISSN 1612-2909 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.

  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.

  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. file

  Schmidt, O.T. (2005) Vorhersage von Anlegelinien-Transition bei Hochauftriebssystemen durch 2D-Schnittberechnungen. Diploma. DLR-Interner Bericht. 124-2005/3, 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.

  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.

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  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.

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  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.

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  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.

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  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). file

  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. file

  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 &quot;Innovative Hochauftriebskonfigurationen&quot;, 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.

  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.. file

  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. Dissertation. DLR-Forschungsbericht. 2001-11, 122 S. Volltext nicht online.

  Wild, J. (2002) Geometriemodellierung und Parameteridentifikation für den Hochauftriebsflügel. Workshop &quot;Geometriemodellierung&quot; 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, 44 S. Volltext nicht online.

  Wild, J. and Herrmann, U. (2003) Designing High-Lift Systems for Low Drag. Other. VKI LS 2003-02, 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. Notes on Numerical Fluid Mechanics and Multidisciplinary Design. 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. filefile

  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 &quot;Enhancement of NATO Military Flight Vehicle Performance by Management of Interacting Boundary Layer Transition and Separation&quot;, 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.

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 &quot;8th International Congress on Sound and Vibration&quot;, 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 &quot;Strömungsakustik/Fluglärm&quot;, 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 Stuermer, Arne (2009) CROR low-speed aerodynamic and aeroacoustic analysis (Section 7.1). Journal of Sound and Vibration, 328, pp. 237-239. Elsevier. DOI: 10.1016/j.jsv.2009.07.022. ISSN 0022-460X. Volltext nicht online.

  Yin, Jianping and Stuermer, 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 Stuermer, 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 Stuermer, Arne (2011) Pylon blowing for the reduction of installation-associated noise of CROR engines (Section 8.2). Journal of Sound and Vibration, 330 (2011), pp. 4974-4975. DOI: 10.1016/j.jsv.2010.06.001. ISSN 0022-460X. Volltext nicht online.

  Yin, Jianping and Stuermer, Arne (2011) Simulation of noise radiation from installed pusher propeller aircraft configurations (Section 8.3). Journal of Sound and Vibration, 330 (2011), pp. 4975-4976. DOI: 10.1016/j.jsv.2010.06.001. ISSN 0022-460X. 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.

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.

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.

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