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Items where Subject is "Institute of Aerodynamics and Flow Technology > Transport Aircraft"

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Number of items at this level: 304.

A

  Abu-Zurayk, Mohammad and Brezillon, Joel (2012) Aero-elastic Multipoint Optimization using the Coupled Adjoint Approach. 18. DGLR-Fach-Symposium der STAB, 06-07 Nov 2012, Stuttgart, Germany. Volltext nicht online.

  Abu-Zurayk, Mohammad and Brezillon, Joel (2013) Development of the Adjoint Approach for Aeroelastic Wing Optimization. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics VIII, 121. Springer Verlag. pp. 59-66. ISBN 978-3-642-35679-7. ISSN 1612-2909 filefile

  Abu-Zurayk, Mohammad and Brezillon, Joel (2014) Aero-Elastic Multipoint Optimization Using the Coupled Adjoint Approach. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics IX, 124. Springer Verlag. pp. 45-52. ISBN 978-3-319-03157-6. ISSN 1612-2909 Volltext nicht online.

  Akkermans, R.A.D and Delfs, J.W. and Marquez, C.O. and Stuermer, A. and Richter, C. and Clemen, C. and Caruelle, B. and Omais, M. (2012) Aeroacoustic and Aerodynamic Importance of a CROR Propulsion System with Unequal Rotor Rotation Speeds. 18. DGLR-Fach-Symposium der STAB, 06. - 07. November 2012, Stuttgart, Deutschland. Volltext nicht online.

  Akkermans, R.A.D. and Delfs, J.W. and Marquez, C.O. and Stuermer, A. and Richter, C. and Clemen, C. and Caruelle, B. and Omais, M. (2014) Aeroacoustic and Aerodynamic Importance of a Unequal Rotor Rotation Speeds of a CROR. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics IX, 124. Springer‐Verlag. pp. 593-600. ISBN 978-3-319-03157-6. ISSN 1612-2909 Volltext nicht online.

B

  Belligoli, Zeno and Lüdeke, Heinrich (2014) DNS of Simple Verification Test Cases Using OpenFOAM. DLR-Interner Bericht. DLR-IB 124-2014/2, 40 S. Volltext nicht online.

  Benini, E. and Ponza, R. and Iannelli, P. and Strüber, H. and Hrncir, Z. and Moens, F. and Kühn, T. (2012) Multi-Point Shape and Setting Optimization of High-Lift Airfoils in Both Take-Off and Landing Conditions. ECCOMAS 2012 - European Congress on Computational Methods in Applied Sciences and Engineering, 10-14 September 2012, Vienna, Austria. Volltext nicht online.

  Bier, N. and Rohlmann, D. and Rudnik, R. (2012) Numerical Maximum Lift Predictions of a Realistic Commercial Aircraft in Landing Configuration. 50th AIAA Aerospace Sciences Meeting, 09 - 12 January 2012, Nashville, TN, USA. Volltext nicht online.

  Bier, Niko (2012) Title confidential. DLR-Interner Bericht. IB 124-2012/911. Volltext nicht online.

  Bier, Niko (2013) Title confidential. DLR-Interner Bericht. DLR-IB 124-2013/903. Volltext nicht online.

  Bier, Niko and Rohlmann, David (2012) Maximum lift predictions of a realistic commercial aircraft in landing configuration. FOR1066 Symposium “Simulation of Wing and Nacelle Stall”, 21.-22. June 2012, Braunschweig, Germany. Volltext nicht online.

  Bier, Niko (2014) Title confidential. DLR-Interner Bericht. IB 124-2014/909, 38 S. Volltext nicht online.

  Bier, Niko and Keye, Stefan and Rohlmann, David (2013) Design of a Wind Tunnel Model for Maximum Lift Predictions Based on Flight Test Data. 31st AIAA Applied Aerodynamics Conference, 24.-27. Juni 2013, San Diego. Volltext nicht online.

  Brezillon, Joel and Carrier, Gerald and Laban, Martin (2010) Multi-Disciplinary Optimization Including Environmental Aspects Applied To Supersonic Aircraft. 27TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES, 19.-24. September 2010, Nizza, Frankreich. file

  Brezillon, Joel and Carrier, Gerald and Laban, Martin (2011) Multidisciplinary Optimization of Supersonic Aircraft Including Low-Boom Considerations. Journal of Mechanical Design (Vol.133, Iss.10). DOI: 10.1115/1.4004972. ISSN 1050-0472. Volltext nicht online.

  Brezillon, Joel and Guntzer, Frederic (2010) Applications of modeFRONTIER on Aeronautical Problems: an overview of experiences at the German Aerospace Centre (DLR). International modeFRONTIER Users’ Meeting 2010, 27.-28. Mai 2010, Trieste, Italien. 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 Abu-Zurayk, Mohammad (2013) Aerodynamic Inverse Design Framework using Discrete Adjoint Method. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics VIII, 121. Springer Verlag. pp. 489-496. ISBN 978-3-642-35679-7. ISSN 1612-2909 file

  Brezillon, Joel and Dwight, Richard and Wild, Jochen (2008) Numerical Aerodynamic Optimisation of 3D High-Lift Configurations. 26th Congress Of The International Council Of The Aeronautical Sciences, 2008-09-14 - 2008-09-19, Anchorage, AK (USA). ISBN 0-9533991-9-2. file

  Brodersen, Olaf (1992) Untersuchung einer Matrix-Dissipation in einem Zelleneckpunkt-Finite-Volumen-Schema zur Lösung der Navier-Stokes-Gleichungen. Master's. DLR-Forschungsbericht. Volltext nicht online.

  Brodersen, Olaf and Crippa, Simone (2012) RANS-based Aerodynamic Drag and Pitching Moment Predictions for the Common Research Model. 18. DGLR-Fach-Symposium der STAB, 6.-7. Nov. 2012, Stuttgart. Volltext nicht online.

  Brodersen, Olaf and Crippa, Simone and Eisfeld, Bernhard and Keye, Stefan and Geisbauer, Sven (2010) DLR Results from the Fourth AIAA CFD Drag Prediction Workshop. AIAA Applied Aerodynamics Conference, 28. Juni - 1. Juli 2010, Chicago, USA. 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.

  Brodersen, Olaf and Monsen, Eric and Ronzheimer, Arno and Rudnik, Ralf and Rossow, Cord (1999) Computation of aerodynamic coefficients for the DLR-F6 configuration using MEGAFLOW. In: New Results in Numerical and Experimental Fluid Mechanics II, 72, pp. 85-92. Vieweg. 11th AG STAB/DGLR Symposium, 1998-11-10 - 1998-11-12, Berlin (DE). ISBN 3-528-03122-0. ISSN 0179-9614 Volltext nicht online.

  Brodersen, Olaf and Rakowitz, Mark and Amant, Stephane and Larrieu, Pascal and Destarac, Daniel and Sutcliffe, Mark (2005) Airbus, ONERA, and DLR Results from the Second AIAA Drag Prediction Workshop. Journal of Aircraft, 42 (4), pp. 932-940. ISSN 0021-8669. Volltext nicht online.

  Brodersen, Olaf and Ronzheimer, Arno and Keye, Stefan (2010) Calculation of Forces and Aerodynamics Effects of the Panasonic Radome installed on the A380. Other. DLR-Interner Bericht. DLR-IB 124-2010/914, 47 S. Volltext nicht online.

  Brodersen, Olaf and Crippa, Simone (2014) RANS-based Aerodynamic Drag and Pitching Moment Predictions for the Common Research Model. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design 124 New Results in Numerical and Experimental Fluid Mechanics IX, 124. Springer Verlag. pp. 485-493. ISBN 978 3 319 03157 6. ISSN 1612-2909 Volltext nicht online.

  Brodersen, Olaf and Crippa, Simone and Eisfeld, Bernhard and Keye, Stefan and Geisbauer, Sven (2009) DLR TAU Results for the AIAA 4th CFD Drag Prediction Workshopi. AIAA 4th CFD Drag Prediction Workshop, 20.-21. Juni 2009, San Antonio, Texas, USA. file

  Brodersen, Olaf and Crippa, Simone and Eisfeld, Bernhard and Keye, Stefan and Geisbauer, Sven (2014) DLR Results from the Fourth AIAA Computational Fluid Dynamics Drag Prediction Workshop. Journal of Aircraft, 51 (4), pp. 1135-1148. AIAA. DOI: 10.2514/1.C031533. ISSN 0021-8669. Volltext nicht online.

C

  Campbell, Richard L. and Campbell, Matthew L. and Streit, Thomas (2011) Progress Toward Efficient Laminar Flow Analysis and Design. 29th AIAA Applied Aerodynamics Conference, 27 - 30 June 2011, Honolulu, Hawaii, USA. Volltext nicht online.

  Carrier, Gérald and Gebhardt, Lutz (2005) A Joint DLR-ONERA Contribution to CFD-based Investigations of Unconventional Empennages for Future Civil Transport Aircraft. In: 2005 CEAS/KATnet Conference on Key Aerodynamic Technologies. CEAS/KATnet Conference on Key Aerodynamic Technologies, 20 - 22 June 2005, Bremen, Germany, 2005-06-20 - 2005-06-22, Bremen (Germany). file

  Casper, Marcus and Scholz, Peter and Radespiel, Rolf and Wild, Jochen and Ciobaca, Vlad (2011) Separation Control on a High-Lift Airfoil using Vortex Generator Jets at High Reynolds numbers. 41st AIAA Fluid Dynamics Conference, 27.-30. Juni 2011, Honolulu, USA. Volltext nicht online.

  Ciobaca, Vlad (2007) Assesment of blocking/mean flow effects in the Cepra19 w/t analyzed by means of CFD simulations. DLR-Interner Bericht. DLR-IB 124-2007/906, 38 S. Volltext nicht online.

  Ciobaca, Vlad (2010) Parameter study for a slatless 2D high-lift airfoil with active separation control using a URANS approach. 17. DGLR-Fach Symposium der STAB, 09. - 10.11.2010, Berlin, Deutschland. Volltext nicht online.

  Ciobaca, Vlad and Dandois, Julien and Bieler, Heribert (2012) A CFD BENCHMARK FOR FLOW SEPARATION CONTROL APPLICATION. Volltext nicht online.

  Ciobaca, Vlad and Melber-Wilkending, Stefan and Wichmann, Georg and Bergmann, Andreas and Küpper, Albert (2012) Experimental and numerical studies of the low speed wind tunnel DNW-NWB’s open test section towards an aeroacoustic facility. In: AIAA Paper 2012-2174. 18th AIAA/CEAS Aeroacoustics Conference (33rd AIAA Aeroacoustics Conference), , 4-6 June 2012, Colorado Springs, Colorado . Volltext nicht frei. file

  Ciobaca, vlad and Kühn, Timo (2011) Active Separation Control on High-Lift Configurations using a URANS approach. ODAS 2011, 9-11 Februar 2011, Toulouse, Frankreich. Volltext nicht online.

  Ciobaca, vlad and Pott-Pollenske, Stephan-Michael and Melber-Wilkending, Stefan and Wichmann, Georg (2012) Computational and Experimental Results in the Open Test Section of the Aeroacustic Windtunnel Braunschweig. 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, Vol121 (10.100). Springer-Verlag. pp. 135-142. ISBN 978-3-642-35679-7. ISSN 1612-2909 file

  Ciobaca, Vlad and Dandois, Julien and Bieler, Heribert (2014) A CFD Benchmark for Flow Separation Control Application. International Journal of Flow Control, 6 (3), pp. 67-81. Multi-Science Publishing. ISBN ISSN 1756-8250. ISSN 1756-8250. Volltext nicht frei. file

  Ciobaca, Vlad and Kühn, Timo and Rudnik, Ralf and Bauer, Matthias and Gölling, Burkhard and Breitenstein, Wiebke (2013) Active Flow-Separation Control on a High-Lift Wing-Body Configuration. Journal of Aircraft (2013, ), pp. 56-72. AIAA. DOI: 10.2514/1.C031659. ISSN 0021-8669. Volltext nicht frei. file

  Ciobaca, Vlad and Rudnik, Ralf and Huacke, Frank and Nitsche, Wolfgang (2013) Active Flow Control on a High-Lift Airfoil: URANS Simulations and Comparison with Time-Accurate Measurements. 31st AIAA Applied Aerodynamics Conference, June 24-27, 2013, San Diego, CA. Volltext nicht frei. file

  Ciobaca, Vlad and Wild, Jochen (2014) Active Flow Control for an Outer Wing Model of a Take-off Transport Aircraft Configuration - A Numerical Study. In: AIAA 32nd Applied Aerodynamics Conference. AIAA Applied Aerodynamics Conferece, Atlanta, 16.-20- Juni. 2014, USA. Volltext nicht frei. file

  Ciobaca, vlad and Kühn, Timo and Rudnik, Ralf and Bauer, Matthias and Gölling, Burkhard (2011) Active Flow Separation Control on a High-Lift Wing-Body Configuration. Part 2: The Pulsed Blowing Application. 29th AIAA Applied Aerodynamics Conference, 27 - 30 June 2011,, Honolulu, Hawaii. file

  Ciobaca, vlad and Wild, Jochen (2013) An Overview of Recent DLR Contributions on Active Flow-Separation Control Studies for High-Lift Configurations. Aerospace Lab, Issue . ISSN 2107-6596. Volltext nicht frei. file

  Cummings, R. and Schütte, A. (2010) An Integrated Computational/Experimental Approach to UCAV Stability & Control Estimations: Overview of NATO RTO AVT-161. 28th AIAA Applied Aerodynamics Conference, 28. Juni - 01. Juli 2010, Chicago, USA. Volltext nicht online.

  Cummings, Russel M. and Schütte, Andreas and Hübner, Andreas-Rene (2013) Overview of Stability and Control Estimation Methods from NATO Task Group AVT-201. AIAA. 51st AIAA Aerospace Sciences Meeting, 07. - 10. Jan. 2013, Dallas, Texas, USA. Volltext nicht online.

  Cummings, Russel M. and Schütte, Andreas (2013) Detached-Eddy Simulation of the Vortical Flowfield about the VFE-2 DeltaWing. Aerospace Science and Technology, Vol. 24, pp. 66-76. Elsevier. DOI: 10.1016/j.ast.2012.02.007. ISSN 1270-9638. Volltext nicht online.

  Cummings, Russel M. and Schütte, Andreas (2012) Integrated Computational/Experimental Approach to Unmanned Combat Air Vehicle Stability and Control Estimation. Journal of Aircraft, Volume 49 (6), pp. 1542-1557. AIAA. DOI: 10.2514/1.C031430. ISSN 0021-8669. Volltext nicht online.

  Cummings, Russel M. and Schütte, Andreas (2014) The NATO STO Task Group AVT-201 on ‘Extended Assessment of Stability and Control Prediction Methods for NATO Air Vehicles’. In: 32nd AIAA Applied Aerodynamics Conference (2000), pp. 1-13. 32nd AIAA Applied Aerodynamics Conference, 16.-20. Juni 2014, Atlanta, GA, USA. Volltext nicht online.

  Cummings, Russel, M and Schütte, Andreas (2008) Detached-Eddy Simulation of the Vortical Flowfield about the VFE-2 DeltaWing. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008-01-07 - 2008-01-10, Reno, Nevada, USA. Volltext nicht frei. file

D

  Dargel, G. and Hansen, H. and Wild, J. and Streit, T. and Rosemann, H. and Richter, K. (2002) Aerodynamische Flügelauslegung mit multifunktionalen Steuerflächen. DGLR Jahrbuch 2002, Band I, S. 1605. DGLR. Volltext nicht online.

  Dietz, Markus and Khier, Walid and Knutzen, Bjoern and Wagner, Siegfried and Krämer, Ewald (2008) Numerical Simulation of a Full Helicopter Configuration Using Weak Fluid-Structure Coupling. 46th AIAA Aerospace Sciences Meeting and Exhibit., 2008-01-07, Reno (USA). file

E

  Egami, Yasuhiro and Fey, Uwe and Klein, Christian and Sitzmann, Martin and Wild, Jochen (2006) Transition Detection on High-Lift devices in DNW-KKK by means of Temperature-Sensitive Paint. Optimage Ltd. Edinburgh, UK. 12th International Symposium on Flow Visualization, 2006-09-10 - 2006-09-14, Göttingen, Germany. Volltext nicht online.

  Egami, Yasuhiro and Fey, Uwe and Klein, Christian and Sitzmann, Martin and Wild, Jochen (2006) Transition Detection on High-Lift Devices in the DNW-KKK by means of Temperature-Sensitive Paint. Other. Volltext nicht online.

  Egami, Yasuhiro and Klein, Christian and Henne, Ulrich and de Groot, Klaus and Meyer, Jörg B. and Krückeberg, Claus-Peter and Boden, Fritz (2013) In-Flight Application of Pressure Sensitive Paint. In: Research Topics in Aerospace Advanced In-Flight Measurement Techniques (Chapter 15). Springer Verlag, Heidelberg New York Dordrecht London. pp. 237-267. ISBN 978-3-642-34737-5 . ISSN 2194-8240 Volltext nicht online.

  Enk, Stephan (2007) Ein Verfahren höherer Ordnung in FLOWer für LES. DLR-Interner Bericht. DLR-IB 124-2007/8, 51 S. Volltext nicht online.

  Enk, Stephan (2008) A Fourth Order Finite Difference Method for Large Eddy Simulation at a Flate Plate. STAB Symposium 2008, 2008-11-3 -2008-11-4, Aachen. Volltext nicht online.

  Eppler, Karsten and Schmidt, Stephan and Schulz, Volker and Ilic, Caslav (2009) Preconditioning the pressure tracking in fluid dynamics by shape Hessian information. Journal of Optimization Theory and Applications, 141 (3), pp. 513-531. Springer. DOI: 10.1007/s10957-008-9507-y. file

F

  Filippone, Antonio and Bertsch, Lothar (2014) Comparison of Aircraft Noise Models with Flyover Data. Journal of Aircraft, 51 (3), pp. 1043-1046. American Institute of Aeronautics and Astronautics. DOI: 10.2514/1.C032368. ISSN 0021-8669. Volltext nicht online.

  Franke, Dirk (2012) Multidisciplinary Optimization of a Generic 2D High-Lift Configuration Regarding Kinematics, Aerodynamics and Flight Mechanics. 30th AIAA Applied Aerodynamics Conference, 25.06.-28.06.2012, New Orleans, USA. Volltext nicht online.

  Franke, Dirk M. (2013) Aerodynamic Optimization of a 3-Element High-Lift Airfoil under Kinematic Constraints. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and experimental Fluid Mechanics VIII, Vol. 121. Springer Verlag. pp. 9-16. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht online.

  Franke, Dirk M. (2010) Aerodynamic Optimization of a High-Lift System with Kinematic Constraints. 17. DGLR-Fach Symposium der STAB, 09. - 10.11.2010, Berlin, Deutschland. Volltext nicht online.

  Franke, Dirk M. and Wild, Jochen (2014) Aerodynamic Design of a Folded Krüger Device for a HLFC Wing. 19. DGLR-Fachsymposium der STAB, 4.-5.11. 2014, München. file

  Führer, Tanja and Görtz, Stefan and Abu-Zurayk, Mohammad and Ilic, Caslav and Keye, Stefan and Banavara, Nagaraj and Kruse, Martin and Brodersen, Olaf and Liepelt, René and Becker, Richard-Gregor and Bach, Tobias and Jepsen, Jonas and Ciampa, Pier Davide and Kohlgrüber, D. and Scherer, Julian and Kier, Thiemo and Leitner, Martin and Siggel, Martin (2014) Entwicklung einer Softwareplattform für die Multidisziplinäre Optimierung eines Gesamtflugzeugs. 63. Deutscher Luft- und Raumfahrtkongress 2014, 16.-18. Sept. 2014, Augsburg, Deutschland. Volltext nicht frei. filefile

G

  Gaffuri, Michele and Brezillon, Joel (2011) Unstructured mesh capabilities for supersonic wing design at low speed conditions. ECCOMAS Thematic Conference CFD & OPTIMIZATION, 23-25 May 2011, Antalya, Turkey. ISBN 978 605 61427 4 1. file

  Gaffuri, Michele and Brezillon, Joël (2012) High lift devices design of a supersonic transport aircraft based on 3D computational fluid dynamics. 6th European Congress on Computational Methods in Applied Sciences and Engineering, 10-14 Sep 2012, Vienna, Austria. ISBN 978-3-9502481-9-7. file

  Gardner, Anthony Donald and Richter, Kai and Mai, Holger and Altmikus, A.R.M. and Klein, A and Rohart, Claas-Hinrik (2013) Experimental investigation of dynamic stall performance for the EDI-M109 and EDI-M112 airfoils. Journal of the American Helicopter Society, Vol. 58 (1), pp. 1-13. AHS International. DOI: 10.4050/JAHS.58.012005. Volltext nicht online.

  Gauger, Nicolas and Ilic, Caslav and Schmidt, Stephan and Schulz, Volker (2012) Non-parametric aerodynamic shape optimization. In: Mathematics and Statistics, 160 (2). Springer. pp. 289-300. file

  Gazaix, Anne and Gendre, Pascal and Chaput, Eric and Blondeau, Christophe and Carrier, Gérald and Schmollgruber, Peter and Brezillon, Joël and Kier, Thiemo (2011) Investigation of Multi-Disciplinary Optimisation for Aircraft Preliminary Design. SAE 2011 AeroTech Congress & Exhibition, 18-21 Oct. 2011, Toulouse, Frankreich. Volltext nicht online.

  Gebhardt, Lutz and Weber, Carsten and Enk, Stephan and Joel, Brezilion (2008) Numerical Optimization on the Vertical Tailplane of Transport Aircraft. STAB Symposium 2008, 2008-11-3 -2008-11-4, Aachen. Volltext nicht online.

  Gebhardt, Lutz and Kröhnert, Anna (2014) Heck- und Leitwerksaerodynamik. In: Handbuch der Luftfahrzeugtechnik Carl Hanser Verlag München. pp. 192-212. ISBN 978-3-446-42341-1. Volltext nicht online.

  Geisbauer, Sven (2010) Unsteady CFD Calculations of Pitching Motions for the DLR-F6 Configuration. DLR-Interner Bericht. DLR-IB 124-2010/1, 56 S. Volltext nicht frei. file

  Geisbauer, Sven (2011) Unsteady CFD Calculations of Pitching and Heave Motions for the DLR-F6 Configuration. DLR-Interner Bericht. DLR-IB 124-2011/1, 71 S. Volltext nicht frei. file

  Geisbauer, Sven (2012) Untersuchung des Einflusses generischer Vorderkantenbeschädigungen auf die aerodynamische Leistungsfähigkeit von Flugzeugprofilen. DLR-Interner Bericht. DLR-IB 124-2012/903, 50 S. Volltext nicht online.

  Geisbauer, Sven (2013) Dokumentation einer Prozesskette zur Simulation von Lastabsetzvorgängen. DLR-Interner Bericht. DLR-IB 124-2013/915, 31 S. Volltext nicht frei. file

  Geisbauer, Sven and Bier, Niko and Kirz, Jochen and Roosenboom, Eric (2013) Title confidential. DLR-Interner Bericht. DLR-IB 124-2013/910, 145 S. Volltext nicht online.

  Geisbauer, Sven (2011) Numerical Spoiler Wake Investigations at the Borders of the Flight Envelope. 29th AIAA Applied Aerodynamics Conference, 27.-30. Juni 2011, Honolulu, USA. Volltext nicht frei. file

  Geisbauer, Sven and Bier, Niko and Kirz, Jochen and Roosenboom, Eric (2013) Validation of the Flow Topology Around Several Airdrop Cargo Configurations at Static Conditions. American Institute of Aeronautics and Astronautics. 31st AIAA Applied Aerodynamics Conference, 24.-27. Juni 2013, San Diego, USA. Volltext nicht frei. file

  Geisbauer, Sven and Schade, Niko and Enk, Stephan and Schmidt, Hauke and Arnold, Jürgen (2011) Experimental and Numerical Investigation of the Flow Topology During Airdrop Operations. 21st AIAA Aerodynamic Decelerator Systems Technology Conference, 23.-26. Mai 2011, Dublin, Irland. Volltext nicht frei. file

  Geisbauer, Sven and Schmidt, Hauke (2014) Title confidential. DLR-Interner Bericht. DLR-IB 124-2014/902, 63 S. Volltext nicht online.

  Geisbauer, Sven and Schmidt, Hauke (2014) Validierung von Lastabsetzsimulationen im wirbelbehafteten Nahfeld eines Transportflugzeuges mit geöffneter Heckrampe. 19. DGLR-Fach-Symposium der STAB, 4.-5. November 2014, München. Volltext nicht online.

  Geyr, Frfr. von, Judith and Knoblauch zu Hatzbach, von, Fedime and Streit, Thomas and Wichmann, Georg (2014) Wing Design Based on a Tapered Wing Natural Laminar Flow Airfoil Catalogue. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design Springer Verlag. pp. 183-191. ISBN 978-3-319-03157-6. ISSN 1612-2909 Volltext nicht online.

  Görtz, Stefan and Eisfeld, Bernhard and Alrutz, Thomas and Ronzheimer, Arno (2007) Evaluation of TAU Flow Solver Capabilities in the Aero-Data-for-Loads Context – Part I: Megaflug. DLR-Interner Bericht. DLR-IB 124-2007/911. Volltext nicht online.

H

  Haar, Danil and Brezillon, Joel (2011) Engine Integration Based on Multi-Disciplinary Optimisation Technique. 11th ONERA-DLR Aerospace Symposium (ODAS) 2011, 9-11 February, 2011, Toulouse. file

  Haar, Danil and Brezillon, Joel (2011) Engine integration based on multidisciplinary optimisation technique. CEAS Aeronautical Journal. DOI: 10.1007/s13272-011-0013-9. Volltext nicht online.

  Haar, Danil (2009) Engine integration based on high-fidelity optimisation technique. KATnet II Conference on Key Aerodynamic Technologies, 12.-14. Mai 2009, Bremen, Germany. file

  Hatanaka, Keita and Brezillon, Joel and Ronzheimer, Arno (2012) A FULLY AUTOMATED CAD-BASED FRAMEWORK FOR SHAPE OPTIMIZATION. 28TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES, September 23rd to 28th, 2012, Brisbane, Australia. Volltext nicht online.

  Heidebrecht, Alexander (2014) Untersuchungen zur Modellierung und Simulation der transsonischen Messstrecke des ETW. Dissertation. DLR-Forschungsbericht. DLR-FB 2014-13, 117 S. Volltext nicht online.

  Hepperle, Martin (2012) Electric Flight - Potential and Limitations. Energy Efficient Technologies and Concepts of Operation, 22-24 October 2012, Lisbon, Portugal. file

  Himisch, Jan and Melber-Wilkending, Stefan and Horstmann, K.H. (2006) Anwendung von modernen CFD-Verfahren fuer den Segelflug - Numerische Untersuchungen der Stroemungseffekte im Kreisflug. 30th Segelflugsymposium, Darmstadt, 23.-24. Nov. 2006, Darmstadt, Deutschland. Volltext nicht online.

  Hoheisel, Heinz and Frhr. von Geyr, Heiko (2012) The influence of engine thrust behaviour on the aerodynamics of engine airframe integration. CEAS Aeronautical Journal, 3 (1), pp. 79-92. Springer. DOI: 10.1007/s13272-012-0044-x. Volltext nicht online.

  Horst, Peter and Keller, Dennis and Diekmann, Jobst Henning and Krukow, Ian and Sommerwerk, Kay (2013) SFB880: FLIGHT DYNAMICS. Deutscher Luft- und Raumfahrtkongress 2013, 10.-12. September 2013, Stuttgart, Deutschland. Volltext nicht online.

  Horstmann, Karl Heinz (2014) Flügelentwurf. In: Handbuch der Luftfahrzeugtechnik Carl Hanser Verlag München. pp. 173-184. ISBN 978-3-446-42341-1. Volltext nicht online.

  Huber, Kerstin Claudie (2010) Numerical Investigation of the Aerodynamic Properties of a Flying Wing Configuration. DLR-Interner Bericht. DLR-IB 124-2010/4, 105 S. Volltext nicht online.

  Huber, Kerstin Claudie and Schütte, Andreas and Löser, Thomas and Vicroy, Dan D. and Rohlf, Detlef and de Groot, Klaus and Mühlmann, Philipp and Weddig, Thomas (2014) Static and dynamic forces, moments and pressure distribution measurements an the DLR-F19 configuration. DLR-Interner Bericht. DLR-IB 124-2014/908, 132 S. Volltext nicht online.

  Huber, Kerstin Claudie and Schütte, Andreas and Rein, Martin (2012) Numerical Investigation of the Aerodynamic Properties of a Flying Wing Configuration. American Institute of Aeronautics and Astronautics, 30th Applied Aerodynamics Conference, 25.-28. Jun. 2012, New Orleans, Louisiana, USA. file

  Huber, Kerstin Claudie and Vicroy, Dan D. and Schütte, Andreas and Hübner, Andreas-René (2014) UCAV model design and static experimental investigations to estimate control device effectiveness and Stability and Control capabilities. In: 32nd AIAA Applied Aerodynamics Conference (2002), pp. 1-21. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, Atlanta, GA, USA. file

  Hübner, Andreas-Rene and Vicroy, Dan D. and Schütte, Andreas and Huber, Kerstin (2011) Experimental and Numerical Investigation of Dynamic Derivatives of an UCAV Configuration. In: NATO RTO Meeting Proceedings (RTO-AVT-MP-189), 23-1-23-20. NATO RTO. NATO RTO AVT Specialists' Meeting on "Assessment of Stability and Control Prediction Methods for NATO Air and Sea Vehicles", 12.-14. Oct. 2011, Portsdown, UK. Volltext nicht online.

  Hühne, Claus-Philipp and Scholz, Peter and Radespiel, Rolf and Wild, Jochen and Ciobaca, Vlad (2012) Active Control of Leading Edge Flow Separation for a Swept High-Lift Airfoil. Deutscher Luft- und Raumfahrtkongress 2012, 10.-12. Sept. 2012, Berlin. Volltext nicht online.

  Hübner, Andreas-René and Kilian , Thomas and Spiering, Frank (2013) Influence ofWing Elasticity on the Experimental and Numerical Determination of Dynamic Derivatives. In: Notes in Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental FGluid Mechanics VIII, Vol. 121. Spinger. pp. 515-523. ISBN 978-3-642-35679-7. ISSN 1612-2909 file

  Hübner, Andreas-René and Vicroy, Dan and Schütte, Andreas and Huber, Kerstin Claudie (2011) Experimental and Numerical Investigation of Dynamic Derivatives of an UCAV Configuration. RTO / AVT-189/RSM-028 Specialists’ Meeting, 12.-14. Okt. 2011 , Schottland. Volltext nicht online.

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  Iannelli, Pierluigi and Wild, Jochen and Minervino, Mauro and Moens, Frederic and Raets, Michael (2012) Analysis and Application of Suitable CFD-Based Optimization Strategies for High-Lift System Design. ECCOMAS 2012, 10.-14. Sept. 2012, Wien, Austria. ISBN 978-3-9502481-9-7. file

  Iannelli, Pierluigi and Wild, Jochen and Minervino, Mauro and Strüber, Henning and Moens, Frederic and Vervliet, Antoon (2013) Design of a High-Lift System for a Laminar Wing. In: Proceedings CD-Rom. 5th European Conference for Aeronautics and Space Sciences (EUCASS) 2013, 1.-4. Juli 2013, München, Deutschland. file

  Ilic, Caslav (2013) Adjoint gradient-based approach for aerodynamic optimization of transport aircraft. European Conference on Computational Optimization (EUCCO), July 17-19, 2013, Chemnitz, Germany. file

  Ilic, Caslav and Brezillon, Joël (2011) Optimization of an airfoil polar in transonic RANS flow using an adjoint gradient-based approach. 15. STAB-Workshop, 9-10 Nov 2011, Göttingen, Germany. file

  Ilic, Caslav and Führer, Tanja and Banavara, Nagaraj and Abu-Zurayk, Mohammad and Einarsson, Gunnar and Kruse, Martin and Himisch, Jan and Seider, Doreen and Richard-Gregor, Becker (2014) Towards cooperative high-fidelity aircraft MDO: comparison of Breguet and ODE evaluation of the cruise mission segment. STAB Symposium 2014, 4-5 Nov 2014, München. file

  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

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  Jann, Thomas and Geisbauer, Sven (2013) Approximated Steady Aerodynamic Coefficients for Two Cuboids and a Hemispherical Shell Used in Airdrop Simulation. In: 22nd AIAA Aerodynamic Decelerator Systems Conference and Seminar. 22nd AIAA Aerodynamic Decelerator Systems Conference and Seminar, 25.-28. März 2013, Daytona Beach, Florida, USA. ISBN 978-1-62410-202-8. Volltext nicht online.

  Jirasek, Adam and Cummings, Russel M. and Schütte, Andreas and Huber, Kerstin Claudie (2014) The NATO STO AVT-201 Task Group on Extended Assessment of Stability and Control Prediction Methods for NATO Air Vehicles: Summary. In: 32nd AIAA Applied Aerodynamics Conference (2394), pp. 1-32. American Institute of Aeronautics and Astronautics. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, Atlanta, GA, USA. Volltext nicht online.

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  Keller, Dennis (2012) Numerische Untersuchung der statischen Längstabilität eines Transportflugzeugs mit Zirkulationskontrolle. 18. DGLR-Fach-Symposium der STAB, 6.-7. Nov. 2012, Stuttgart. Volltext nicht online.

  Keller, Dennis (2013) Numerical Investigation of Engine Effects on the Stability and Controllability of a Transport Aircraft with Circulation Control. 31st AIAA Applied Aerodynamics Conference, 24.-27. Juni 2013, San Diego, USA. Volltext nicht online.

  Keller, Dennis (2014) Numerical Approach Aspects for the Investigation of the Longitudinal Static Stability of a Transport Aircraft with Circulation Control. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design 124 New Results in Numerical and Experimental Fluid Mechanics IX, 124. Springer. pp. 13-22. ISBN 978-3-319-03157-6. ISSN 1612-2909 Volltext nicht online.

  Keller, Dennis and Rudnik, Ralf (2013) Aerodynamic Aspects of the Longitudinal Motion of a High-Lift Aircraft Configuration with Circulation Control. Project Report. Shaker Verlag. file

  Keye, Stefan (1993) Experimental Wall Interference Assessment for a DLR R4C Airfoil in the Transonic Variable Slotted Wall Test Section of the VKI-S1 Wind Tunnel. Other. Other. VKI-PR 1993-04. Volltext nicht online.

  Keye, Stefan (2011) Fluid-Structure Coupled Analysis of a Transport Aircraft and Flight Test Validation. Journal of Aircraft, Vol. 48 (2), pp. 381-390. DOI: 10.2514/1.C000235. Volltext nicht online.

  Keye, Stefan (2012) Simulation eines vollständig elastischen Transportflugzeugs mit Hilfe der Strömungs-Struktur-Kopplung. 18. DGLR-Fach-Symposium der STAB, 6.-7. November 2012, Stuttgart, D. Volltext nicht online.

  Keye, Stefan (2011) Analyse der vollständigen Hochauftriebskonfiguration des Transportflugzeugs Airbus A350-900 XWB mit Hilfe der Fluid-Struktur-Kopplung. DLR-Interner Bericht. DLR-IB 124-2011/910, 24 S. (Unpublished) Volltext nicht online.

  Keye, Stefan and Rudnik, Ralf (2009) Aero-Elastic Simulation of DLR’s F6 Transport Aircraft Configuration and Comparison to Experimental Data. In: 48th AIAA Aerospace Sciences Meeting. 48th AIAA Aerospace Sciences Meeting, 2009-01-05 - 2009-01-08, Orlando, FL (USA). Volltext nicht online.

  Keye, Stefan and Sitzmann, Martin and Brodersen, Olaf and Heinrich, Ralf (2008) Fluid-Structure Coupled Loads Analysis of DLR’s F6 Wing-Body Configuration. In: 46th AIAA Aerospace Sciences Meeting, 2008. 46th AIAA Aerospace Sciences Meeting, 2008, 7.1.2008-10.1.2008, Reno, NV (USA). Volltext nicht online.

  Keye, Stefan (2014) An Assessment of the Influence of Fuselage Deformations on the Numerical Prediction of High-Lift Performance. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics IX, 124. pp. 385-393. ISBN 978-3-319-03157-6. ISSN 1612-2909 Volltext nicht online.

  Keye, Stefan and Brodersen, Olaf and Rivers, Melissa, B. (2014) Investigation of Aeroelastic Effects on the NASA Common Research Model. Journal of Aircraft, 51 (4), pp. 1323-1330. AIAA. DOI: 10.2514/1.C032598. ISSN 0021-8669. Volltext nicht online.

  Keye, Stefan and Togiti, Vamshi and Eisfeld, Bernhard and Brodersen, Olaf and Rivers, Melissa (2013) Investigation of Fluid-Structure-Coupling and Turbulence Model Effects on the DLR Results of the Fifth AIAA CFD Drag Prediction Workshop. In: 31st AIAA Applied Aerodynamics Conference. 31st AIAA Applied Aerodynamics Conference, 24.-27.6.2013, San Diego, CA, USA. Volltext nicht online.

  Kompenhans, Jürgen and Pallek, Dieter and von Geyr, Heiko and Schröder, Andreas (2009) Experimental and Numerical Study on the Flow behind a TPS. Seminar China Aerodynamics Research and Development Center (CARDC), 27.03.2009, Mianyang, China. Volltext nicht online.

  Kroll, Norbert and Brezillon, Joel and Abu-Zurayk, Mohammad and Li, Chunna and Ilic, Caslav and Ronzheimer, Arno (2013) Progress in Numerical Shape Optimization. CAE Aerdoynamics Seminar 2013, 14.-19. Sept. 2013, Peking, China. Volltext nicht online.

  Kroll, Norbert and Abu-Zurayk, Mohammad and Dimitrov, Diliana and Franz, Thomas and Führer, Tanja and Gerhold, Thomas and Görtz, Stefan and Heinrich, Ralf and Ilic, Caslav and Jepsen, Jonas and Jägersküpper, Jens and Kruse, Martin and Krumbein, Andreas and Langer, Stefan and Liu, Dishi / D. S. and Liepelt, René and Reimer, Lars and Ritter, Markus and Schwöppe, Axel and Scherer, Julian and Spiering, Frank and Thormann, Reik and Togiti, Vamshi and Vollmer, Daniel and Wendisch, Jan-Hendrik (2014) "DLR-Projekt Digital-X" Auf dem Weg zur virtuellen Flugzeugentwicklung und Flugerprobung auf Basis höherwertiger Verfahren. Deutscher Luft- und Raumfahrtkongress 2014, 16.-18. Sep. 2014, Augsburg, Deutschland. Volltext nicht online.

  Kruse, Martin and Wunderlich, Tobias Franziskus and Heinrich, Lars (2012) A Conceptual Study of a Transonic NLF Transport Aircraft with Forward Swept Wings. 30th AIAA Applied Aerodynamics Conference, 25. - 28. Jun 2012, New Orleans, USA. ISBN eISBN: 978-1-62410-185-4 . Volltext nicht frei. file

  Krüger, Wolf and Cumnuantip, Sunpeth and Liersch, Carsten (2011) Multidisciplinary Conceptual Design of a UCAV Configuration. In: Proceedings AVT-MP173. RTO/AVT Panel Workshop "Virtual Prototyping of Affordable Military Vehicles Using Advanced MDO", 16.-18. Mai 2011, Sofia, Bulgarien. Volltext nicht online.

  Kröhnert, Anna and Gebhardt, Lutz (2013) Investigation of the impact of simplifying the aircraft geometry on the characteristics of the vertical tailplane. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics VIII, Vol. 121. Springer Verlag. pp. 1-8. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht online.

  Kröhnert, Anna and Gebhardt, Lutz (2012) The Influence of geometric Simplifications of an Aircraft with Respect to the Optimization of the Aerodynamic Characteristics of the Vertical Tailplane. Deutscher Luft- und Raumfahrtkongress 2012, 10.-12. Sept. 2012, Berlin, Deutschland. Volltext nicht online.

  Kröhnert, Anna (2014) Title confidential. DLR-Interner Bericht. DLR-IB 124-2014/904, 62 S. Volltext nicht online.

  Kröhnert, Anna (2014) Title confidential. DLR-Interner Bericht. DLR-IB 124-2014/903, 112 S. Volltext nicht online.

  Kröhnert, Anna (2012) Titel confidential. DLR-Interner Bericht. DLR-IB 124-2012/915, 32 S. Volltext nicht online.

  Kröhnert, Anna (2014) Numerical Investigation of Tangential Blowing at the Rudder of a Vertical Tailplane Airfoil. In: 32nd AIAA Applied Aerodynamics Conference. 32nd AIAA Applied Aerodynamics Conference, AIAA Aviation and Aeronautics Forum and Exposition 2014, 16.-20. Juni 2014, Atlanta, Georgia, USA. Volltext nicht online.

  Kröhnert, Anna (2014) Numerical Investigation of Unsteady Tangential Blowing at the Rudder of a Vertical Tailplane Airfoil. 19. DGLR-Fach-Symposium der STAB, 4.-5. November 2014, München. Volltext nicht online.

  Kwak, Dongyoun and Gaffuri, Michele and Ohira, Keisuke and Brezillon, Joël (2012) Numerical Study of the Reynolds Number Effect on Low Aspect Ratio Wing at Low Speed. 28th Congress of the International Council of the Aeronautical Sciences , 23-28 Sep 2012, Brisbane, Australia. ISBN 978-0-9565333-1-9. Volltext nicht online.

  Kwak, Dongyoun and Ohira, Keisuke and Rudnik, Ralf (2014) Reynolds number effect on vortex dominant flow on the SST configurations. APISAT2014, 24.-26. Sept. 2014, Shanghai, China. Volltext nicht online.

  Kühn, Timo and Ciobaca, Vlad and Rudnik, Ralf and Gölling, Burkhard and Breitenstein, Wiebke (2010) Pilot Study of a High Lift Wing Configuration for Performance Optimization. Joint Symposium of DFG FOR 1066 and DLR-Airbus CASE, Braunschweig, Germany. (Unpublished) Volltext nicht online.

  Kühn, Timo and Ciobaca, Vlad and Rudnik, Ralf and Gölling, Burkhard and Breitenstein, Wiebke (2011) Active Flow Separation Control on a High-Lift Wing-Body Configuration - Part 1: Baseline Flow and Constant Blowing. 29th AIAA Applied Aerodynamics Conference, 27 - 30 June 2011, Honolulu, HI, USA. file

  Kühn, Timo and Lenfers, Carsten (2012) A Numerical Assessment of Side Plate Effects for a Low Aspect Ratio Wind Tunnel Model with a Smart Droop Nose Device. 30th AIAA Applied Aerodynamics Conference, 25-28 June 2012, New Orleans, LA, USA. Volltext nicht online.

  Kühn, Timo and Wild, Jochen (2010) Aerodynamic Optimization of a Two-Dimensional Two-Element High Lift Airfoil with a Smart Droop Nose Device. 1st EASN Association Workshop on Aerostructures, Paris, France. (Unpublished) Volltext nicht online.

  Kühn, Timo (2013) Aerodynamische Vermessung lärmarmer Hochauftriebssysteme im Rahmen des DLR-Projekts SLED. Other. DLR-Interner Bericht. DLR-IB 124-2013/908, 108 S. Volltext nicht online.

  keye, stefan (2009) Fluid-Structure-Coupled Analysis of a Transport Aircraft and Comparison to Flight Data. 39th AIAA Fluid Dynamics Conference, 22 - 25 June 2009, San Antonio, TX (USA). Volltext nicht online.

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  Lenfers, Carsten (2012) Propeller Design for a future QESTOL Aircraft in the BNF Project. AIAA Applied Aero 2012, 25.-28.06.2012, USA, New Orleans. Volltext nicht frei. file

  Lenfers, Carsten (2013) Computational Investigation of the DLR Reference Noise Source in the AWB - Contribution to Garteur AG 50. DLR-Interner Bericht. DLR-IB 124-2013/1, 40 S. Volltext nicht frei. file

  Lenfers, Carsten and Janssen, Ruud and Beck, Nils and Friedrichs, Jens and Rezaeian, Alireza (2014) Experimental Investigation of the Propeller Design for future QESTOL Aircraft in the BNF Project. AIAA SciTech, 52nd Aerospace and Sciences Meeting, 13.-17. Jan. 2014, USA. DOI: 10.2514/6.2014-0562. file

  Levy, David and Laflin, Kelly and Tinoco, Edward and Vassberg, John and Rider, Ben and Mani, Mori and Rumsey, Christopher and Wahls, Richard and Morrison, Joseph and Brodersen, Olaf and Crippa, Simone and Mavriplis, Dimitri and Murayama, Mitsuhiro (2013) Summary of Data from the Fifth AIAA CFD Drag Prediction Workshop. In: AIAA (2013-46), pp. 1-31. AIAA. 51st AIAA Aerospace Sciences Meeting, 7.-10. Jan. 2013, Dallas, USA. Volltext nicht online.

  Levy, David and Laflin, Kelly and Tinoco, Edward and Vassberg, John and Mani, Mori and Rider, Ben and Rumsey, Christopher and Wahls, Richard and Morrison, Joseph and Brodersen, Olaf and Crippa, Simone and Mavriplis, Dimitri and Murayama, Mitsuhiro (2014) Summary of Data from the Fifth Computational Fluid Dynamics Drag Prediction Workshop. Journal of Aircraft, 51 (4), pp. 1194-1213. AIAA. DOI: 10.2514/1.C032389. ISSN 0021-8669. Volltext nicht online.

  Li, Chunna and Brezillon, Joel and Görtz, Stefan (2012) Efficient Global Optimization of a Natural Laminar Airfoil Based on Surrogate Modeling. STAB2012, 6-7 Nov 2012, Germany, Stuttgart. Volltext nicht online.

  Li, Chunna and Görtz, Stefan and Brezillon, Joel (2014) Efficient Global Optimization of a Natural Laminar Airfoil Based on Surrogate Modeling. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics, 124. Springer. pp. 53-63. ISBN 978-3-319-03157-6. ISSN 1612-2909 Volltext nicht online.

  Liersch, Carsten Martin and Hepperle, Martin (2011) A distributed toolbox for multidisciplinary preliminary aircraft design. 60. Deutscher Luft- und Raumfahrtkongress 2011, 27.-29. Sept. 2011, Bremen, Deutschland. Volltext nicht online.

  Liersch, Carsten Martin and Hepperle, Martin (2011) A distributed toolbox for multidisciplinary preliminary aircraft design. CEAS Aeronautical Journal, Volume 2 (Number 1-4), pp. 57-68. Springer. DOI: 10.1007/s13272-011-0024-6. ISSN 1669-5582. Volltext nicht online.

  Liersch, Carsten and Huber, Kerstin Claudie (2014) Conceptual Design and Aerodynamic Analyses of a Generic UCAV Configuration. In: 32nd AIAA Applied Aerodynamics Conference (2001). 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, Atlanta, GA, USA. file

  Löser, T. and Vicroy, D. and Schütte, A. (2010) SACCON Static Wind Tunnel Tests at DNW-NWB and 14'x22' NASA LaRC. 28th AIAA Applied Aerodynamics Conference, 28. Juni - 01. Juli 2010, Chicago, USA. Volltext nicht online.

  Lüdeke, Heinrich (2013) Validierung eines impliziten finite-Differenzen Verfahrens für Direkte Numerische Simulationen. 16. Stab-Workshop, 12.-13. Nov. 2013, Göttingen, Deutschland. Volltext nicht online.

  Lüdeke, Heinrich (2014) Influences of a Rippled Surface on Growth Rates of Tollmien-Schlichting Waves. In: IUTAM Symposium on Laminar-Turbulent Transition. IUTAM-ABCM Symposium on Laminar-Turbulent Transition, 8.-12. Sept. 2014, Rio de Janeiro, Brazil. Volltext nicht online.

  Lüdeke, Heinrich (2014) Interior Flow Simulation of Suction Chambers for HLFC Profiles. In: DLRK Beitrag. 63. Deutscher Luft- und Raumfahrtkongress 2014, 16.-18. September 2014, Augsburg, Germany. Volltext nicht online.

  Lüdeke, Heinrich and Wartemann, Viola and Seitz, Arne (2013) Direct Numerical Simulation of Tollmien Schlichting Waves to Support Linear Stability Analysis. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics VIII, 121. Springer Verlag. pp. 227-234. ISBN 978-3-642-35679-7. ISSN 1612-2909 file

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  Manso Jaume, Ana and Wild, Jochen (2014) Aerodynamic Design and Optimization of a High Lift Device for a Wind Turbine Airfoil. Jahrestagung der STAB, 04.-05. Nov. 2014, München, Deutschland. Volltext nicht frei. file

  Marquez, Carlos (2009) Steady Simulation of an Isolated Helicopter Rotor in Hover Configuration with the DLR TAU-Code. [Other] (Unpublished) Volltext nicht frei. file

  Marquez Gutierrez, Carlos Omar (2013) Title confidential. DLR-Interner Bericht. DLR-IB 124-2013/909, 95 S. Volltext nicht online.

  Marquez Gutierrez, Carlos Omar and Steiner, Sören (2013) Analysis of a CROR Propulsion System at High Angle of Attack and at Low Speed Flight Conditions. 13th ONERA-DLR Aerospace Symposium, 27.-29. Mai 2013, Palaiseau, France. Volltext nicht frei. file

  Marquez Gutierrez, Carlos Omar and Steiner, Sören (2014) Aerodynamic Installation Effects of CROR Engines at Take-off Configurations. AIAA SciTech 2014 Conference, 13-17 Januar 2014, National Harbor, Maryland. Volltext nicht frei. file

  Marquez Gutierrez, Carlos Omar and Steiner, Sören and Fuss, Uwe (2013) Installation Aerodynamics of Open Rotor Engines: An Overview of The LuFo IV Project OPERO. 62. Deutscher Luft- und Raumfahrt Kongress 2013, 10-12 September 2013, Stuttgart, Deutschland. Volltext nicht frei. file

  Marquez Gutierrez, Carlos Omar and Stuermer, Arne and Clemen, Carsten (2011) Installation Effects of a CROR Propulsion System on a Modified DLR-F6 Aircraft Configuration. 20th International Society of Airbreathing Engines Conference, 12-16 September 2011, Göteborg, Schweden. Volltext nicht frei. file

  Marquez Gutierrez, Carlos Omar and Stürmer, Arne and Clemen, Carsten and Grimminger, Andreas (2012) Validation of Actuator Disk Simulations of CROR Propulsion Systems at Low-Speed Flight Conditions. 30th AIAA Applied Aerodynamics Conference, 25.-28. Juni 2012, New Orleans, LA, USA. Volltext nicht frei. file

  Meissner, Dietmar and Cusset, Francois and Wild, Jochen and Schulz, Matthias (2013) Experimental Verification of the DESIREH High-Lift Wing at Aircraft Flight Conditions. 5th European Conference for Aeronautics and Space Sciences (EUCASS) 2013, 1.-4. Juli 2013, München, Deutschland. Volltext nicht online.

  Melber-Wilkending, Stefan (2008) Application of Advanced CFD Tools for Cryogenic Testing. 5th. European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2008), 2008-06-30 - 2008-07-04, Venice. (Unpublished) Volltext nicht online.

  Melber-Wilkending, Stefan and Bergmann, Andreas (2012) Aeroacoustic optimization of the NWB airline and turning vanes based on high fidelity CFD and acoustic simulation. 18th AIAA/CEAS Aeroacoustics Conference, Colorado Springs, Colorado, USA. Volltext nicht frei. file

  Melber-Wilkending, Stefan (2008) Aerodynamics of the Wing/Fuselage Junction at an Transport Aircraft in High-lift Configuration. 16th AG STAB/DGLR Symposium, 2008-11-03 - 2008-11-04, Aachen. file

  Melber-Wilkending, Stefan (2014) Numerische Untersuchung aerodynamischer Effekte im Flügelrumpfübergang einer Hochauftriebskonfiguration. Dissertation, TU-Braunschweig / DLR Braunschweig. Volltext nicht online.

  Melber-Wilkending, Stefan (2003) Near field CFD calculations of baseline configuration. Project Report. Volltext nicht online.

  Melber-Wilkending, Stefan (2004) Near field CFD calculations for variations on baseline configuration. Project Report. Volltext nicht online.

  Melber-Wilkending, Stefan (2005) RANS-Solutions of complex configurations as Input for Vortex-Rollup Studies, Part III. Project Report. Volltext nicht online.

  Melber-Wilkending, Stefan (2005) Synthesis of near field CFD calculations of DLR. Project Report. Volltext nicht online.

  Melber-Wilkending, Stefan and Allen, S. and Breitsamter, C. (2007) A Comparision between CFD and Wind Tunnel Measurements for Wake Vortex Prediction. First CEAS European Air and Space Conference, 10.-13. September 2007, Berlin, Deutschland. Volltext nicht online.

  Melber-Wilkending, Stefan and Wichmann, Georg (2008) Application of Advanced CFD Tools for High Reynolds Number Testing. 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, 2009-01-05 - 2009-01-08, Orlando, Florida. file

  Mialon, Bruno and Khrabrov, Alex and Ben Khelil, Salua and Hübner, Andreas and Da Ronch, Andrea and Badcock, Ken and Cavagna, Luca and Eliasson, Peter and Zang, Mengmeng and Ricci, Sergio and Jouhaud, Jean-Christophe and Rogé, Gilbert and Hitzel, Stephan and Lahuta, Martin (2011) Validation of numerical prediction of dynamic derivatives: The DLR-F12 and the Transcruiser test cases. Progress in Aerospace Sciences, Vol. 47 (8), pp. 674-694. file

N

  Nallapula, Varun and Bier, Niko and Rohlmann, David and Radespiel, Rolf (2012) Simulation of the Horizontal Tail Plane Stall of a Transport Aircraft. 42nd AIAA Fluid Dynamics Conference and Exhibit, 25.-28. Jun. 2012, New Orleans, Louisiana, USA. Volltext nicht online.

  Neitzke, Klaus-Peter and Rudnik, Ralf and Schröder, Andreas (2005) Low Speed Validation Tests on Engine/Airframe Integration within the European Project EUROLIFT II. 41st AIAA Joint Propulsion Conference, 2005-07-23 - 2005-07-26, Tucson, Arizona (USA). ISBN 978-1-56347-764-5. Volltext nicht online.

O

  Ohira, Keisuke and Kwak, Dongyoun and Brezillon, Joël and Gaffuri, Michele (2012) Numerical Study of the Eddy Viscosity Turbulence Model for High Alpha Flow over the Low Aspect Ratio Wing. 44th Fluid Dynamics Conference/Aerospace Numerical Simulation Symposium 2012, 5-6 Jul 2012, Toyama, Japan. Volltext nicht online.

P

  Pallek, Dieter and von Geyr, Heiko and Schröder, Andreas (2008) Experimental and numerical study on the flow behind a TPS. 14th International Symposium on Application of Laser Techniques to Fluid Mechanics, 2008-07-07 - 2008-07-10, Lisbon (Portugal). Volltext nicht online.

  Politz, Christina and Grüttemann, Andreas and Kreienfeld, Malte and Schröder, Andreas and Konrath, Robert and Boden, Fritz and Lawson, Nicholas and Casella, Domenico (2009) High lift flow structures: In-flight PIV feasibility study. AIM Final Workshop, 27.10.-28.10.2009, Göttingen, Germany. Volltext nicht online.

  Pott-Pollenske, Michael and Wild, Jochen and Bertsch, Lothar (2014) Aerodynamic and Acoustic Design of Silent Leading Edge Devices. 20th AIAA/CEAS Aeroacoustics Conference, 16. - 20. Juni 2014, Atlanta, USA. Volltext nicht frei. file

  Pott-Pollenske, Michael and Wild, Jochen and Herr, Michaela and Delfs, Jan Werner and Rudenko, Anton and Büscher, Alexander (2014) SLAT NOISE REDUCTION BY MEANS OF ADAPTIVE LEADING EDGE DEVICES. Aircraft Noise Reductio by Flow Control and Active/Adaptive Techniques, 25. - 26. September 2014, Vilnius, Litauen. file

Q

  Quix, Harald and Schulz, Matthias and Quest, Jürgen and Rudnik, Ralf and Schröder, Andreas (2007) Low Speed High Lift Validation Tests within the European Project EUROLIFT II. American Institute of Aeronautics and Astronautics. 25th AIAA Applied Aerodynamics Conference, 2007-06-25 - 2007-06-28, Miami, FL (USA). Volltext nicht online.

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  Raffel, Markus and de Gegorio, Fabrizio and Sheng, W. and Gibertini, G. and Seraudie, A. and de Groot, Klaus and van der Wall, Berend G. (2009) GENERATION OF AN ADVANCED HELICOPTER EXPERIMENTAL AERODYNAMIC DATABASE. 35th European Rotorcraft Forum, 2009-09-22 - 2009-09-25, Hamburg (Germany). ISBN 978-3-932182-65-0. ISSN 0178-6326 file

  Raffel, Markus and de Gregorio, Frabizio and de Groot, Klaus and Schneider, Oliver and Gibertini, G. and Seraudie, Alain (2011) On the Generation of a Helicopter Aerodynamic Database. The Aeronautical Journal, Vol. 115 (1164), pp. 103-112. Royal Aeronautical Society (RAeS). Volltext nicht online.

  Reimer, Lars and Gall, Christian and Geisbauer, Sven (2014) Eine TAU-Simulink-Kopplung zur aerodynamisch-flugdynamischen Simulation - Implementierung und Anwendung auf eine generische militärische Transportflugzeugkonfiguration mit Beschädigung. DLR-Interner Bericht. DLR-IB 124-2014/910, 89 S. file

  Rein, Martin and Höhler, Gebhard and Schütte, Andreas and Bergmann, Andreas and Löser, Thomas (2008) Ground-Based Simulation of Complex Maneuvers of a Delta-Wing Aircraft. Journal of Aircraft, 45 (1), pp. 286-291. DOI: 10.2514/1.30033. Volltext nicht online.

  Renard, Nicolas and Wild, Jochen (2012) Unsteady Simulation of The Flow During the Deployment of High-Lift Systems. ECCOMAS 2012, 10.-14. Sept. 2012, Wien, Austria. ISBN 978-3-9502481-9-7. file

  Richter, Kai and Koch, Stefan and Gardner, Anthony Donald and Mai, Holger and Klein, Alexander and Rohardt, Claas-Hinrik (2012) Experimental Investigation of Unsteady Transition on a Pitching Rotor Blade Airfoil. 38th European Rotorcraft Forum, 04. - 07. Sept. 2012, Amsterdam, Niederlande. Volltext nicht online.

  Richter, Kai and Koch, Stefan and Gardner, Anthony Donald and Mai, Holger and Klein, Alexander and Rohardt, Claas-Hinrik (2014) Experimental Investigation of Unsteady Transition on a Pitching Rotor Blade Airfoil. Journal of the American Helicopter Society, 59 (01), pp. 1-12. AHS International. DOI: 10.4050/JAHS.59.012001. ISSN 0002-8711. Volltext nicht online.

  Ritter, Sebastian (2013) Untersuchung des Einflusses der Position eines eng gekoppelten Ultra-High-Bypass-Triebwerks auf eine Hochauftriebskonfiguration. In: Jahresbericht 2013, 2013, pp. 24-25. 16. STAB-Workshop, 12.-13. Nov. 2013, Göttingen, Deutschland. file

  Rohardt, Claas-Hinrik (2012) Ermittlung des Grenz-NTS-Faktors im NWB-DNW. DLR-Interner Bericht. DLR-IB 124-2012/913, 66 S. Volltext nicht frei. file

  Ronzheimer, Arno and Hepperle, Martin and Brezillon, Joël and Brodersen, Olaf and Lieser, Jan (2013) Aerodynamic Optimal Engine Integration at the Fuselage Tail of a Generic Business Jet Configuration. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics VIII, Vol. 121. Springer Verlag. pp. 25-32. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht online.

  Ronzheimer, Arno (2006) Prospects of Geometry Parameterization based on Freeform Deformation in MDO. In: ERCOFTAC 2006: Design Optimisation: Methods & Applications, pp. 1-10. ERCOFTAC 2006 International Conference, [2006-04-05 - 2006-04-07], Las Palmas de Gran Canaria, Spain. ISBN 84-85650-12-3. Volltext nicht frei. file

  Ronzheimer, Arno (2010) Investigation and Minimization of Upsweep Drag of Aft-Loading Military Transporters with Tail Strakes. 28th AIAA Applied Aerodynamics Conference, 28 June - 1 July 2010, Chicago, Illinois. Volltext nicht frei. file

  Ronzheimer, Arno (2012) Aircraft Geometry Parameterization with High-End CAD-Software for Design Optimization. ECCOMAS 2012, 10.-14. September 2012, Wien, Östereich. ISBN 978-3-9502481-9-7. Volltext nicht frei. file

  Ronzheimer, Arno and Hepperle, Martin and Brezillon, Joël and Lieser, Jan (2012) Aerodynamic Optimal Engine Integration for a Business Jet Configuration. 8th AIAA Multidisciplinary Design Optimization Specialist Conference (MDO), 23.-26. April 2012, Honolulu, Hawaii. ISBN 978-1-60086-937-2. Volltext nicht frei. file

  Ronzheimer, Arno and Natterer, Franz Josef and Brezillon, Joël (2010) Aircraft Wing Optimization Using High Fidelity Closely Coupled CFD and CSM Methods. 13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference, Fort Worth, Texas, Fort Worth, Texas. Volltext nicht frei. file

  Roosenboom, Eric and Schade, N. and Acisu, I. and Schröder, Andreas (2009) Experimental and Numerical Investigation of the Near-Field Wake behind a Transport Aircraft with an Open Ramp. 4th Symposium on Integrating CFD and Experiments in Aerodynamics, 14-16 September 2009, Sint-Genesius-Rode, Belgium. Volltext nicht online.

  Roosenboom, Eric and Schröder, Andreas and Geisler, Reinhard and Pallek, Dieter and Agocs, Janos and Stürmer, Arne and Marquez Gutierrez, Carlos Omar and Neitzke, Klaus-Peter (2011) Experimental and numerical investigation of a counter rotating open rotor flow field. 29th AIAA Applied Aerodynamics Conference, 27.-30. Jun. 2011 , Honolulu, Hawaii, USA. Volltext nicht online.

  Roosenboom, Eric and Stürmer, Arne and Schröder, Andreas (2009) Comparison of PIV measurements with unsteady RANS calculations in a propeller slipstream. 27th AIAA Applied Aerodynamics Conference, 22 - 25 June 2009, San Antonio, Texas, USA. ISBN 978-1-56347-975-5. Volltext nicht online.

  Roosenboom, Eric and Stürmer, Arne and Schröder, Andreas (2010) Advanced Experimental and Numerical Validation and Analysis of Propeller Slipstream Flows. Journal of Aircraft, Vol. 47 (1, January-February 2010), pp. 284-291. American Institute of Aeronautics and Astronautics. DOI: 10.2514/1.45961. ISSN 0021-8669. Volltext nicht online.

  Roosenboom, Eric and Stürmer, Arne and Schröder, Andreas (2011) PIV data for numerical validation - Application to propeller flow fields -. CFD and Experiment – Integration of Simulation, Workshop of the DGLR-Querschnittsbereich Thermo- and Fluiddynamics, 05. - 06. Apr. 2011, Göttingen, Deutschland. Volltext nicht online.

  Roosenboom, Eric and Stürmer, Arne and Schröder, Andreas (2008) Comparison of uRANS CFD calculation with phase-locked PIV measurement data for propeller flow. EWA - PIV/CFD Joint Workshop, 2008-09-23 - 2008-09-24, Modane (France). Volltext nicht online.

  Rudnik, Ralf (2014) Konfigurationsaerodynamik. In: Handbuch der Luftfahrzeugtechnik Carl Hanser Verlag GmbH & Co. KG. pp. 83-113. ISBN 978-3446423411. Volltext nicht online.

  Rudnik, Ralf and Huber, Kerstin Claudie and Melber-Wilkending, Stefan (2012) EUROLIFT Test Case Description for the 2nd High Lift Prediction Workshop. 30th AIAA Applied Aerodynamics Conference, 25.-28. Juni 2012, New Orleans. Volltext nicht online.

  Rudnik, Ralf and Melber-Wilkending, Stefan (2014) DLR Contribution to the 2nd High Lift Prediction Workshop. SciTech 2014, 13.-17. Jan. 2014, National Harbor, USA. Volltext nicht online.

  Rudnik, Ralf and Melber-Wilkending, Stefan (2013) DLR Contribution to the Second High Lift Prediction Workshop. 31st AIAA Applied Aeordynamics Conference, 24.-27. Juni 2013, San Diego, USA. Volltext nicht online.

  Rudnik, Ralf and Reckzeh, Daniel and Quest, Juergen (2012) HINVA - High Lift INflight VAlidation - Project Overview and Status. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 09.-12. Jan. 2012, Nashville, USA. Volltext nicht online.

  Rudnik, Ralf and Schwetzler, Detlev (2014) High lift INflight VAlidation (HINVA) - Overview about the 1st Flight Test Campaign. 32nd AIAA Applied Aerodynamics Conference, 16.-20. Juni 2014, Atlanta, USA. Volltext nicht online.

  Runge, Hartmut and Rack, W. and Alba, Ruiz-Leon and Hepperle, Martin (2007) A Solar-Powered HALE-UAV for Arctic Research. In: CEAS Conference 2007, pp. 1-6. CEAS Conference, 2007-09-10, Berlin. Volltext nicht online.

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  Schade, Niko (2010) Simulation of Store Separation - Scaling Requirements for Wind Tunnel Experiments and Validation of Numerical Simulations. 17. DGLR-Fach Symposium der STAB, Berlin, Germany. Volltext nicht online.

  Schade, Niko (2013) Simulation of Store Separation - Scaling Requirements for Wind Tunnel Experiments and Validation of Numerical Simulations. In: New Results in Numerical and Experimental Fluid Mechanics VIII New Results in Numerical and Experimental Fluid Mechanics VIII, Vol. 121. Springer Verlag. pp. 17-24. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht online.

  Schmid, Sven and Lutz, Thorsten and Krämer, Ewald and Kühn, Timo (2009) Passive Control of the Flow Around the Stratospheric Observatory for Infrared Astronomy. Journal of Aircraft, 46 (4), pp. 1319-1325. AIAA. DOI: 10.2514/1.40777. Volltext nicht online.

  Schmidt, Stephan and Gauger, Nicolas and Ilic, Caslav and Schulz, Volker (2011) Three dimensional large scale aerodynamic shape optimization based on shape calculus. 41st AIAA Fluid Dynamics Conference and Exhibit, June 27-30, 2011, Honolulu, USA. file

  Schmidt, Stephan and Ilic, Caslav and Schulz, Volker and Gauger, Nicolas (2011) Airfoil design for compressible inviscid ï¬Â�ow based on shape calculus. Optimization and Engineering, 12 (3), pp. 349-369. Springer. DOI: 10.1007/s11081-011-9145-3. file

  Schmidt, Stephan and Ilic, Caslav and Schulz, Volker and Gauger, Nicolas (2013) Three-dimensional large-scale aerodynamic shape optimization based on shape calculus. AIAA Journal, 51 (11). DOI: 10.2514/1.J052245. ISSN 0001-1452. file

  Scholz, Peter and Kähler, Christian and Radespiel, Rolf and Wild, Jochen and Wichmann, Georg (2009) Active Control of Leading-Edge Separation within the German Flow Control Network. In: 47th AIAA Aerospace Sciences Meeting (AIAA 2009-0529). AIAA. ASM 2009, 2009-01-05 - 2009-01-08, Orlando, FL (USA). Volltext nicht online.

  Schröder, Andreas and Pallek, Dieter and Geisler, Reinhard and Lauke, Thomas and Herr, Michela and Geyr, Heiko v. and Dierksheide, Uwe (2009) Particle Image Velocimetry as Validation Tool in Aeronautics. 47th AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition, 2009-01-05 - 2009-01-08, Orlando, FL (USA). Volltext nicht online.

  Schröder, Andreas and Agocs, Janos and Geisler, Reinhard and Heider, André and Konrath, Robert and Pallek, Dieter and Roosenboom, Eric and von Geyr, Heiko and Stürmer, Arne (2008) Particle Image Velocimetry as Validation Tool in Aeronautics. Artes Gráficas Torres S.L., Morales 17, 08029 Barcelona, Spain. 5th. European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2008), 2008-06-30 - 2008-07-04, Venice (Italy). ISBN 978-84-96736-55-9. Volltext nicht online.

  Schröder, Andreas and Göing, Markus and Pallek, Dieter and Geyr, Heiko v. (2007) Experimental and numerical characterisation of the flow behind a TPS. Joint EWA and UFAST Workshop on Validation of Numerical Methods by Experiments in Aerodynamics, 2007-06-04 -2007-06-06, Prag (Tschechischen Republik). Volltext nicht online.

  Schütte, A. and Boelens, O.J. and Löser, T. and Oehlke, M. (2010) Prediction of the Flow Around the X-31 Aircraft Using Two Different CFD Methods. 28th AIAA Applied Aerodynamics Conference, 28. Juni - 01. Juli 2010, Chicago, USA. Volltext nicht online.

  Schütte, Andreas and Boelens, Okko J. and Oehlke, Martin and Jirásek, Adam and Loeser, Thomas (2012) Prediction of the flow around the X-31 aircraft using three different CFD methods. Aerospace Science and Technology, Volume 20 (Issue 1), pp. 21-37. Elsevier. DOI: doi:10.1016/j.ast.2011.07.014. ISSN 1270-9638. Volltext nicht online.

  Schütte, Andreas and Cummings, Russ M. and Loeser, Thomas (2012) An integrated computational/experimental approach to X-31 stability & control estimation. Aerospace Science and Technology, Volumne 20 (Issue 1), pp. 2-11. Elsevier. DOI: 10.1016/j.ast.2011.10.010. ISSN 1270-9638. Volltext nicht online.

  Schütte, Andreas and Hummel, D. and Hitzel, S. (2010) Numerical and Experimental Analyses of the Vortical Flow Around the SACCON Configuration. 28th AIAA Applied Aerodynamics Conference, 28. Juni - 1. Juli 2010, Chicago, USA. Volltext nicht online.

  Schütte, Andreas and Hummel, Dietrich and Hitzel, Stephan M. (2012) Flow Physics Analyses of a Generic Unmanned Combat Aerial Vehicle Configuration. Journal of Aircraft, Volume 49 (6), pp. 1638-1651. AIAA. DOI: 10.2514/1.C031386. ISSN 0021-8669. Volltext nicht online.

  Schütte, Andreas and Lüdeke, Heinrich (2013) Numerical investigations on the VFE-2 65-degree rounded leading edge delta wing using the unstructured DLR TAU-Code. Aerospace Science and Technology, 24 (1), pp. 56-65. Elsevier Masson SAS. DOI: [10.1016/j.ast.2012.03.002]. ISSN 1270-9638. Volltext nicht online.

  Schütte, Andreas and Huber, Kerstin Claudie and Boelens, Okko J. (2014) Static and dynamic numerical simulations of a generic UCAV configuration with and without control devices. In: 32nd AIAA Applied Aerodynamics Conference (2132), pp. 1-26. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, USA. file

  Schütte, Andreas and Huber, Kerstin Claudie and Liersch, Carsten and Rütten, Markus and Rein, Martin and Koch, Stefan and Jaffrezic, Benoit and Zimper, Dirk and Konrath, Robert and Wiggen, Stefan and Voß, Guido and Lindermeir, Erwin and Nauroz, Mobin and Kemptner, Erich and Steinhauser, Reinhold and Looye, Gertjan and Ehlers, Jana and Rohlf, Detlef and Siggel, Martin (2014) Abschlussbericht DLR Projekt FaUSST „Fortschrittliche aerodynamische UCAV Stabilitäts- und Steuerungs- Technologien“. DLR-Interner Bericht. DLR-IB 124-2014/907, 190 S. Volltext nicht online.

  Schütte, Andreas and Lüdeke, Heinrich (2008) Numerical investigations on the VFE-2 65-Degree rounded leading edge delta wing using the unstructured DLR-TAU-Code. 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008-01-07 - 2008-01-10, Reno, Nevada, USA. Volltext nicht frei. file

  Seitz, Arne (2008) Recent Drag Reduction Activities at DLR. Drag Reduction Workshop 4, 14.-16. Oktober 2008, Ascot, United Kingdom. Volltext nicht online.

  Seitz, Arne (2012) Rekonstruktion eines Störströmungsfeldes aus der Wandmessung von Tollmien-Schlichting Wellen. 18. DGLR-Facg-Symposium der STAB, 06. - 07. Nov. 2012, Stuttgart, Deutschland. Volltext nicht online.

  Seitz, Arne and Horn , Matthias (2012) Kleine Löcher - Große Wirkung. DLR-Interner Bericht. DLR-IB 435-2012/93. Volltext nicht online.

  Seitz, Arne and Horstmann, Karl-Heinz (2010) Design Studies on NLF and HLFC Applications at DLR. International Council of the Aeronautical Sciences. ICAS 2010, 19.-24. September 2010, Nizza, Frankreich. ISBN 978-0-9565333-0-2. Volltext nicht frei. file

  Seitz, Arne (2014) Reconstruction of a Disturbance Flow Field from Wall Measurements of Tollmien-Schlichting Waves. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics IX, 124. Springer Verlag. pp. 203-211. ISBN 978 3 319 03157 6. ISSN 1612-2909 Volltext nicht frei. file

  Spiering, Frank and Heinrich, Ralf and Keye, Stefan (2013) Development of a Parallel Fluid-Structure Coupling Environment and Application to a Wind Tunnel Model under High Aerodynamic Loads. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics VIII, 121. Springer Verlag. pp. 507-514. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht online.

  Streit, Thomas and Wedler, Sven and Kruse, Martin (2014) DLR NATURAL AND HYBRID TRANSONIC LAMINAR WING DESIGN INCORPORATING NEW METHODOLOGIES. RAeS Advanced Aero Concepts, Design and Operations Conference, 22 – 24 Jul. 2014, Bristol, United Kingdom. Volltext nicht online.

  Streit, Thomas and Horstmann, Karl Heinz and Schrauf, Géza and Hein, Stefan and Fey, Uwe and Egami, Yasuhiro and Perraud, Jean and Salah El Din, Itham and Cella, Ubaldo and Quest, Jürgen (2011) Complementary Numerical and Experimental Data Analysis of the ETW Telfona Pathfinder Wing Transition Tests. 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 4 - 7 January 2011, Orlando, Florida USA. Volltext nicht frei. file

  Streit, Thomas and Wichmann, Georg and von Knoblauch zu Hatzbach, Fedime and Campbell, Richard L. (2011) Implications of Conical Flow for Laminar Wing Design and Analysis. 29th AIAA Applied Aerodynamics Conference, 27 - 30 June 2011, Honolulu, Hawaii, USA. Volltext nicht frei. file

  Stuermer, Arne (2010) Multi-Disciplinary Numerical Analysis for the Contra-Rotating Open Rotor. MUSAF Colloquium, 27-29 Sep 2010, Toulouse, France. (Unpublished) Volltext nicht online.

  Stuermer, Arne (2010) Numerical Analysis of CROR Propulsion System Aerodynamics and Aeroacoustics at DLR. 2nd UTIAS-MITACS International Workshop on Aviation and Climate Change, 27-28 May 2010, Toronto, Canada. (Unpublished) Volltext nicht online.

  Stuermer, Arne (2010) DLR CROR & Propeller Noise Prediction: Numerical Approach Requirements & Limitations. 14th CEAS-ASC Workshop, 7-8 Oct 2010, Warsaw, Poland. (Unpublished) Volltext nicht online.

  Stuermer, Arne and Akkermans, R.A.D. (2013) Multidisciplinary Analysis of CROR Propulsion Systems: DLR Activities in the JTI SFWA Project. 62. Deutscher Luft- und Raumfahrtkongress, 10-12 Sep 2013, Stuttgart, Germany. Volltext nicht online.

  Stuermer, Arne and Yin, Jianping (2009) Low- Speed Aerodynamics and Aeroacoustics of CROR Propulsion Systems. In: 15th AIAA/CEAS Aeroacoustics Conference. AIAA. 15th AIAA/CEAS Aeroacoustics Conference, 11-13 May 2009, Miami, FL., USA. Volltext nicht online.

  Stuermer, Arne and Yin, Jianping (2010) Aerodynamic and Aeroacoustic Installation Effects for Pusher-Configuration CROR Propulsion Systems. 28th AIAA Applied Aerodynamics Conference, 8 June - 01 July, 2010, Chicago, IL, USA. Volltext nicht online.

  Stuermer, Arne and Yin, Jianping (2010) Active Control of Unsteady Blade Loads for Installed CROR Propulsion Systems. 17. DGLR-Fach Symposium der STAB, 9-10 Nov 2010, Berlin, Germany. (Unpublished) Volltext nicht online.

  Stuermer, Arne and Yin, Jianping (2012) The Case for Counter-Rotation of Installed Contra-Rotating Open Rotor Propulsion Systems. 30th AIAA Applied Aerodynamics Conference, 25-28 June 2012, New Orleans, LA, USA. Volltext nicht online.

  Stuermer, Arne and Yin, Jianping (2013) Pylon Trailing Edge Blowing for the Control of CROR Unsteady Blade Loads. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics VIII, Vol. 121. Springer Verlag. pp. 715-722. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht online.

  Stuermer, A. and Akkermans, R.A.D. and Delfs, J.W. (2014) Assessment of Front Rotor Trailing Edge Blowing for the Reduction of Open Rotor Interaction Noise. In: Notes in Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics IX, 124. Springer Verlag. pp. 609-618. ISBN 978-3-319-03157-6. ISSN 1612-2909 Volltext nicht online.

  Stürmer, Arne (2007) Unsteady Simulations of a Generic Isolated Tractor Contra-Rotating Propeller with the DLR TAU-Code. DLR-Interner Bericht. DLR-IB 124-2007/913, 41 S. Volltext nicht online.

  Stürmer, Arne (2007) CFD Validation of Unsteady Installed Propeller Flows Using the DLR TAU-Code. DGLR. 1st CEAS European Air and Space Conference, 2007-09-10 - 2007-09-13, Berlin, Deutschland. ISSN 0070-4083 Volltext nicht online.

  Stürmer, Arne and Yin, Jianping (2012) Installation Impact on Pusher CROR Engine Low Speed Performance and Noise Emission Characteristics. International Journal of Engineering Systems Modelling and Simulation, 4 (1–2/2012), pp. 59-68. Inderscience Enterprises Ltd. DOI: 10.1504/IJESMS.2012.044844. ISSN 1755-9758. Volltext nicht online.

  Stürmer, Arne (2006) Unsteady CFD Simulations of Propeller Installation Effects. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2006-07-09 - 2006-07-12, Sacramento, CA (USA). Volltext nicht online.

  Stürmer, Arne (2008) Unsteady CFD Simulations of Contra-Rotating Propeller Propulsion Systems. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2008-07-21 - 2008-07-23, Hartford, CT, USA. Volltext nicht online.

  Stürmer, Arne and Marquez Gutierrez, Carlos Omar and Roosenboom, Eric and Schröder, Andreas and Geisler, Reinhard and Pallek, Dieter and Agocs, Janos and Neitzke, Klaus-Peter (2012) Experimental and Numerical Investigation of a Contra Rotating Open-Rotor Flowfield. Journal of Aircraft, Vol. 49 (6), pp. 1868-1877. American Institute of Aeronautics and Astronautics. DOI: 10.2514/1.C031698. ISSN 0021-8669. Volltext nicht online.

  Stürmer, Arne and Yin, Jianping (2008) Aerodynamic and Aeroacoustic Analysis of Contra-Rotating Open Rotor Propulsion Systems at Low-Speed Flight Conditions. 16. DGLR/STAB-Symposium, 2008-11-03 - 2008-11-04, Aachen. (Unpublished) Volltext nicht online.

  Stürmer, Arne and Yin, Jianping and Akkermans, R.A.D. (2014) Progress in Aerodynamic and Aeroacoustic Integration of CROR Propulsion Systems. The Aeronautical Journal, 118 (1208), pp. 1137-1158. Royal Aeronautical Society. ISSN 0001-9240. Volltext nicht online.

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  Togiti, Vamshi and Eisfeld, Bernhard and Brodersen, Olaf (2014) Turbulence Model Study for the Flow Around the NASA Common Research Model. Journal of Aircraft, 51 (4), pp. 1331-1343. American Institute of Aeronautics and Astronautics. DOI: 10.2514/1.C032609. ISSN 0021-8669. Volltext nicht online.

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  Vassberg, John C. and Tinoco, Edward N. and Mani, Mori and Brodersen, Olaf P. and Eisfeld, Bernhard and Wahls, Richard A. and Morrison, Joseph H. and Zickuhr, Tom and Laflin, Kelly R. and Mavriplis, Dimitri J. (2008) Abridged Summary of the Third AIAA Computational Fluid Dynamics Drag Prediction Workshop. Journal of Aircraft, 45 (3), pp. 781-798. DOI: 20.2514/1.30572. ISSN 0021-8669. Volltext nicht online.

  Vassberg, John C. and Tinoco, Edward N. and Mani, Mori and Rider, Ben and Zickuhr, Tom and Levy, David and Brodersen, Olaf and Eisfeld, Bernhard and Crippa, Simone and Wahls, Richard and Morrison, Joseph and Mavriplis, Dimitri and Murayama, Mitsuhiro (2014) Summary of the Fourth AIAA Computational Fluid Dynamics Drag Prediction Workshop. Journal of Aircraft, 51 (4), pp. 1070-1089. AIAA. DOI: 10.2514/1.C032418. ISSN 0021-8669. Volltext nicht online.

  Vicroy, Dan D. and Loeser, Thomas D. and Schütte, Andreas (2012) Static and Forced-Oscillation Tests of a Generic Unmanned Combat Air Vehicle. Journal of Aircraft, Volume 49 (6), pp. 1558-1583. AIAA. DOI: 10.2514/1.C031501. ISSN 0021-8669. Volltext nicht online.

  Vicroy, Dan D. and Huber, Kerstin Claudie and Rohlf, Detlef and Löser, Thomas (2014) Low-speed Dynamic Wind Tunnel Test Analysis of a Generic 53° Swept UCAV Configuration with Controls. In: 32nd AIAA Applied Aerodynamics Conference (2003), pp. 1-24. 32nd AIAA Applied Aerodynamics Conference, Atlanta, GA, USA, 16.-20. Juni 2014, Atlanta, GA, USA. Volltext nicht online.

  Vollmers, Heinrich and Puffert-Meissner, Wolfgang and Schröder, Andreas (2005) Analysis of PIV Flow Field Measurements behind the ALVAST-Model in High-Lift Configuration. In: Springer-Verlag Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), Vol. 92. Springer. pp. 17-24. ISBN 3-540-33286-3. Volltext nicht online.

  Voss, Guido and Gerz, Thomas and Baumann, Robert and Stumpf, Eike and Press, Michael (2009) Wake Vortex Alleviation by Differential and Oscillating Flap Setting: A flight test. 27th Applied Aerodynamics Conference, 22-25 Jun 2009, San Antonio, Texas. file

  Voß, Guido and Melber-Wilkdending, Stefan and Rudnik, Ralf (2006) premature decay of wake vortices with differential- and oscillating flap setting. In: 2006 European Conference on Computational Fluid Dynamics. ECCOMAS 2006, 2006-09-05-2006-09-08, Egmond aan Zee (The Netherlands). Volltext nicht online.

  Voß, Guido and Carmer, Carl F. v. and Konrath, Robert and Stumpf, Eike and Krückeberg, Claus-Peter and Meyer, Hans-Henning and Mattner, Hartmut (2007) Wake vortex alleviation by differential and oscillating flap setting: a comparative numerical and experimental study. 1st CEAS European Air and Space Conference, 2007-09-10 - 2007-09-13, Berlin. ISSN 0700-4083 Volltext nicht online.

  Voß, Guido and Konrath, Robert and von Carmer, Carl and Krueckeberg, Claus-Peter and Meyer, Henning (2008) Wake vortex alleviation by differential and oscillating flap settings: A numerical and experimental study. DLR-Forschungsbericht. DLR-FB-2008-15, 26 S. Volltext nicht online.

  v. Geyr, Heiko and Schade, Niko (2010) Prediction of Maximum Lift Effects on Realistic High-Lift-Commercial-Aircraft-Configurations within the European project EUROLIFT II. Second Symposium "Simulation of Wing and Nacelle Stall", June 22nd - 23rd, 2010, Braunschweig. Volltext nicht online.

  v. Geyr, Judith and v. Knoblauch z. Hatzbach, Fedime and Arne, Seitz and Thomas, Streit and Georg, Wichmann (2012) Wing Design based on a Tapered Wing NLF Airfoil Catalogue. 18. DGLR-Fach-Symposium der STAB, 06. - 07. Nov. 2012, Stuttgart, Deutschland. Volltext nicht online.

  von Geyr, Judith and von Knoblauch zu Hatzbach, Fedime and Seitz, Arne and Streit, Thomas and Wichmann, Georg (2012) Swept Wing Design based on a Tapered Wing NLF Airfoil Catalogue. 18. DGLR-Fach-Symposium der STAB, 06. - 07. Nov. 2012, Stuttgart, Deutschland. Volltext nicht online.

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  Wedler, Sven and Seitz, Arne (2014) Specifications of HLFC Devices for Flight Test Applications. DLR-Interner Bericht. DLR-IB 124-2014/905, 34 S. Volltext nicht online.

  Wedler, Sven and Streit, Thomas (2014) New Methodologies Tailored for the design of Aerodynamically Robust Laminar Wings. Greener Aviation: Clean Sky breakthroughs and worldwide status, 12. - 14. Mrz., Brüssel, Belgien. Volltext nicht frei. file

  Wild, Jochen (2008) Multi-objective constrained optimisation in aerodynamic design of high-lift systems. International Journal of Computational Fluid Dynamics, 22 (3), pp. 153-168. Taylor & Francis. DOI: 10.1080/10618560701868420. ISSN 1061-8562. Volltext nicht online.

  Wild, Jochen (2008) Active Separation Control on the Leading Edge of a Slatless Swept Wing in High Lift Configuration Using Steady Blowing in the European Project EUROLIFT II. KATNet II Separation Control Workshop, 2008-04-01 - 2008-04-03, Toulouse. Volltext nicht online.

  Wild, Jochen (2012) 3D Anisotropic Delaunay Meshing for Ideal Interfacing to Block-Unstructured Mixed Meshes Using a Sparse Octree for Metric Size Propagation. In: Proceedings on CD-Rom, p. 2541. ECCOMAS 2012, 10.-14. Sept. 2012, Wien, Austria. ISBN 978-3-9502481-9-7. file

  Wild, Jochen (2012) Quality assessment of Smooth Block-Unstructured Mixed Meshes for Aerodynamic Applications. MASCOT/ISGG 2012, 22.-26. Okt. 2012, Las Palmas de Gran Canaria, Spain. file

  Wild, Jochen and Brezillon, Joel (2008) Optimization of 3-D Multi-Element High-Lift Device Configuration. In: 5th. European Congress on Computational Methods in Applied Sciences and Engineering. ECCOMAS 2008, 2008-06-30 - 2008-07-05, Venedig, IT. Volltext nicht online.

  Wild, Jochen and Brezillon, Joel and Amoignon, Olivier and Quest, Jürgen and Moens, Frederic and Quagliarella, Domenico (2009) Advanced Design by Numerical Methods and Wind Tunnel Verification within the European High-Lift Program. Journal of Aircraft, 46 (1), pp. 157-167. AIAA. ISSN 0021-8669. Volltext nicht online.

  Wild, Jochen and Brezillon, Joel and Mertins, Ralf and Quagliarella, Domenico and Germain, Eric and Amoignon, Olivier and Moens, Frederic (2006) REALISTIC HIGH-LIFT DESIGN OF TRANSPORT AIRCRAFT BY APPLYING NUMERICAL OPTIMIZATION. In: ECCOMAS CFD 2006. ECCOMAS CFD 2006, 2006-09-05 - 2006-09-08, Egmond aan Zee, NL. Volltext nicht online.

  Wild, Jochen and Dettmar, Holger (2006) Beeinflussung der Anlegelinie-Transition am Vorflügel durch Geometriemodifikationen. 15. DGLR Fachsymposium der STAB, 2006-11-29 - 2006-12-01, Darmstadt. Volltext nicht online.

  Wild, Jochen and Dettmar, Holger (2007) Manipulation of Attachment Line Transition by Geometry Modification at the Slat of a Multi-Element Airfoil. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 96, pp. 219-226. Springer. 15th STAB/DGLR Symposium, 2006-11-29 - 2006-12-01, Darmstadt. ISBN 3-540-74458-4. Volltext nicht online.

  Wild, Jochen and Haucke, Frank and Scholz, Peter (2008) Large scale separation flow control experiments within the German Flow Control Network. KATNet II Separation Control Workshop, 2008-04-01 - 2008-04-03, Toulouse. Volltext nicht online.

  Wild, Jochen and Mertins, Ralf and Quagliarella, Domenico and Brezillon, Joel and Quest, Jürgen and Amoignon, Olivier and Moens, Frederic (2005) Applying numerical optimization to realistic high-lift design of transport aircraft – an overview of the aerodynamic design optimisation investigations within the EUROLIFT II project. In: Proceedings of the Sixth Conference on Evolutionary and Deterministic Mehtods for Design, Optimization and Control with Applications to Indutsrial and Societal Problems. TU München. EUROGEN 2005, 2005-09-12 2005-09-14, München, BY (D). ISBN 3-00-017534-2. Volltext nicht online.

  Wild, Jochen (2011) Smooth Mixed Meshes for Acceleration of RANS CFD in Aircraft Analysis and Design. 49th AIAA Aerospace Sciences Meeting, 4.-7. Jan. 2011, Orlando, FL, USA. file

  Wild, Jochen (2012) Experimental investigation of Mach- and Reynolds-number dependencies of the stall behavior of 2-element and 3-element high-lift wing sections. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 9.-12. Jan. 2012, Nashville, TN, USA. file

  Wild, Jochen (2013) Mach and Reynolds Number Dependencies of the Stall Behavior of High-Lift Wing-Sections. Journal of Aircraft, 50 (4), pp. 1202-1216. DOI: 10.2514/1.C032138. ISSN 0021-8669. Volltext nicht online.

  Wild, Jochen (2013) Overview on the DeSiReH Project. 5th European Conference for Aeronautics and Space Sciences (EUCASS) 2013, 1.-4. Juli 2013, München, Deutschland. file

  Wild, Jochen (2013) About the Generation of Unstructured Mesh Families for Grid Convergence Assessment by Mixed Meshes. In: Adaptive Modeling and Simulation 2013, pp. 692-702. International Center for Numerical Methods in Engineering (CIMNE), Barcelona, Spain. VI International Conference on Adaptive Modeling and Simulation ADMOS 2013, 3.-5. Juni 2013, Lisbon, Portugal. ISBN 978-84-941004-8-2. file

  Wild, Jochen (2014) Mach-, Reynolds and Sweep Effects on Active Flow Seperation Control Effectivity on a 2-Element Airfoil Wing. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design Acitve Flow and Combustion Control 2014, 127. Springer Verlag. pp. 87-100. ISBN 978-3-319-11966-3. ISSN 1612-2909 Volltext nicht online.

  Wild, Jochen and Brezillon, Joel (2005) Application of multi-objective constraint optimization in aerodynamic high-lift design. In: Proceedings of the Sixth Conference on Evolutionary and Deterministic Mehtods for Design, Optimization and Control with Applications to Indutsrial and Societal Problems. TU München. EUROGEN 2005, 2005-09-12 2005-09-14, München, BY (D). ISBN 3-00-017534-2. file

  Wild, Jochen and Brezillon, Joel and Amoignon, Olivier and Quest, Jürgen and Moens, Frederic and Quagliarella, Domenico (2007) Advanced High-Lift Design by Numerical Methods and Wind Tunnel Verification within the European Project EUROLIFT II. 25th AIAA Applied Aerodynamics Conference, 2007-06-25 - 2007-06-28, Miami, FL (USA). file

  Wild, Jochen and Pott-Pollenske, Michael and Nagel, Björn (2006) An integrated design approach for low noise exposing high-lift devices. 3rd AIAA Flow Control Conference, 2006-06-05 - 2006-06-08, San Francisco, CA (USA). file

  Wild, Jochen and Wichmann, Georg and Haucke, Frank and Peltzer, Inken and Scholtz, Peter (2009) Large scale separation flow control experiments within the German Flow Control Network. In: 47th AIAA Aerospace Sciences Meeting (AIAA 2). AIAA. ASM 2009, 2009-01-05 - 9009-01-08, Orlando, FL (USA). file

  Wong, P.W.C. and Maina, M. and Nayyar, P. and Streit, Th. and Liersch, C.M. and Salah El Din, I. and Arnal, D. (2010) Numerical Analysis of Natural Laminar Flow on Forward Swept Wings. Other. ARA Technical Memo 600, 8 S. Volltext nicht frei. file

  Wunderlich, Tobias Franziskus (2013) Multidisziplinäre Optimierung von Flügeln für Verkehrsflugzeuge mit Berücksichtigung der statischen Aeroelastizität. Dissertation. DLR-Forschungsbericht. Forschungsbericht 2013-34, 214 S. file

Y

  Yin, Jianping and Stuermer, Arne and Aversano, Marco (2009) Coupled uRANS and FW- H Analysis of Installed Pusher Propeller Aircraft Configurations. AIAA. 15th AIAA/CEAS Aeroacoustics Conference, 11-13 May 2009, Miami, FL., USA. Volltext nicht online.

  Yin, Jianping and Stürmer, Arne (2013) Fast simulation of noise radiation and reduction from installed pusher propeller aircraft. CEAS Aeronautical Journal, Volume 4 (Issue 4), pp. 443-458. Springer Vienna. DOI: 10.1007/s13272-013-0089-5. ISSN 1869-5590. Volltext nicht online.

Z

  Zimper, Dirk and Hitzel, Stephan M. (2014) Model Scale and "Real" Flight of Generic UCAV and Advanced Combat Aircraft - An Industrial Perspective. In: 32nd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics. AIAA AVIATION 2014, 16.-20. Jun. 2014, Atlanta, Georgia, USA. ISBN 978-1-62410-288-2. ISSN 2014-2267 Volltext nicht frei. file

  Zimper, Dirk and Hummel, Dietrich (2014) Analysis of the transonic flow around a generic UCAV configuration. In: 32nd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics. AIAA AVIATION 2014, 16.-20. Jun. 2014, Atlanta, Georgia, USA. ISBN 978-1-62410-288-2. ISSN 2014-2266 Volltext nicht frei. file

  Zimper, Dirk and Rein, Martin (2014) Experimental and numerical analysis of the transonic vortical flow over a generic lambda wing configuration. In: 32nd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics. AIAA AVIATION 2014, 16.-20. Jun. 2014, Atlanta, Georgia, USA. ISBN 978-1-62410-288-2. ISSN 2014-2005 Volltext nicht frei. file

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