Items where Subject is "Institute of Aerodynamics and Flow Technology > High Speed Configurations"
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- High Speed Configurations (337)
- Institute of Aerodynamics and Flow Technology (9303)
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Ali, Syed Raza Christopher and Radespiel, Rolf and Theiß, Alexander (2014) Transition Experiment with a Blunt Apollo Shape like Capsule in Hypersonic Ludwieg Tube. 63. Deutscher Luft- und Raumfahrtkongress 2014, 16. Sept. 2014, Augsburg, Deutschland. Volltext nicht online. |
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Barth, Hans Peter and Stapel, Waldemar and Hein, Stefan and Rütten, Markus and Rosemann, Henning (2013) Auslegung eines Prinzipexperiments zur Kontrolle von Querströmungsinstabilitäten im Verbund AKSA. 16. STAB-Workshop, 12. – 13. Nov. 2013, Göttingen, Deutschland. Volltext nicht online. |
Barth, Hans Peter and Hein, Stefan and Rosemann, Henning (2016) AKSA-Aktive Kontrolle von Störungen in der Aerodynamik „Entwicklung, Aufbau und Durchführung des Prinzipexperiments der schiebenden ebenen Platte für Untersuchungen der Transitionsbeeinflussung mit der UFD-Methode“. Project Report. 25 S. Volltext nicht online. |
Barth, Hans Peter and Hein, Stefan and Rosemann, Henning (2016) Redesigned swept flat-plate experiment for crossflow-induced transition studies. 20. DGLR-Fachsymposium der STAB, 08. - 09. Nov. 2016, Braunschweig, Deutschland. Volltext nicht online. |
Berens, Thomas M. and Delot, Anne-Laure and Tormalm, Magnus H. and Ruiz-Calavera, Luis P. and Funes-Sebastian, David E. and Rein, Martin and Säterskog, Michael and Ceresola, Nicola and Zurawski, Ludovic (2014) Numerical and Experimental Investigations on Highly Integrated Subsonic Air. 52nd Aerospace Sciences Meeting - AIAA SciTech, 13. - 17. Jan. 2014, National Harbor, Maryland, USA. doi: 10.2514/6.2014-0722. Volltext nicht online. |
Berens, Thomas M. and Delot, Anne-Laure and Tormalm, Magnus H. and Ruiz-Calavera, Luis P. and Funes-Sebastian, David E. and Rein, Martin and Säterskog, Michael and Ceresola, Nicola and Zurawski, Ludovic (2014) Highly Integrated Subsonic Air Intakes. Other. AD/AG-46. 58 S. Volltext nicht online. |
Berens, Thomas M. and Delot, Anne-Laure and Tormalm, Magnus H. and Ruiz-Calavera, Luis-Pablo and Funes-Sebastian, David-Ernesto and Rein, Martin and Säterskog, Michael and Ceresola, Nicola (2015) Numerical and Experimental Investigations on Subsonic Air Intakes with Serpentine Ducts for UAV Configurations. 5th CEAS Air & Space Conference, 07. - 11. Sept. 2015, Delft, The Netherlands. Volltext nicht online. |
Boiko, Andrey and Dovgal, Alexander and Gorev, Vasily and Hein, Stefan and Wilke, Bastian (2010) Particle Image Velocimetry used for determination of the local skin friction coefficient of turbulent boundary layers. DLR-Interner Bericht. DLR-IB 224-2010 A 43. 9 S. Volltext nicht online. |
Bornhöft, Erik and Schülein, Erich (2010) Potenzial einer lokalen Strömungserhitzung zur Bugwiderstandsreduzierung im Überschall. 17. DGLR-Fach-Symposium der STAB, 09. - 10. Nov. 2010 , Berlin, Deutschland. Volltext nicht online. |
Borodulin, V. I. and Ivanov, A. V. and Kachanov, Y. S. and Mischenko, D. A. and Örlü, R. and Tillmark, N. and Hanifi, Ardeshir and Hein, Stefan and Würz, W. (2015) Title confidential. Project Report. TECHNICAL REPORT TR D1.15. 81 S. Volltext nicht online. |
Borodulin, V. I. and Ivanov, A. V. and Kachanov, Y. S. and Örlü, R. and Hanifi, A. and Hein, Stefan (2016) Characteristics of 3D Instability of a 35-Degree Swept Wing to CF and TS Modes. Experiment and Theory. 18th INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH, 27. Jun. - 03. Jul. 2016, Perm, Russland. doi: 10.1063/1.4963996. Volltext nicht online. |
Bruse, Martin and Klein, Christian and Henne, Ulrich and Yorita, Daisuke and Ondrus, Vladimir and Beifuss, Uwe and Rütten, Markus (2014) Status of Pressure Sensitive Paint Systems used in DNW. 122th Meeting of STAI, 05. - 07. Oct. 2014, Aussois, France. Volltext nicht online. |
Busse, Felix (2013) Experimentelle Untersuchung von Maßnahmen der Strömungssteuerung und des Einflusses der Transition an Vorderkanten schwach gepfeilter Delta-Flügel. DLR-Interner Bericht. DLR-IB 224-2013 A 86. Master's. Universität Göttingen. 96 S. Volltext nicht online. |
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Costantini, Marco and Hein, Stefan and Henne, Ulrich and Klein, Christian and Koch, Stefan and Schojda, Lukas and Ondrus, Vladimir and Schröder, Wolfgang (2016) Pressure Gradient and Nonadiabatic Surface Effects on Boundary Layer Transition. AIAA Journal, 54 (11), pp. 3465-3480. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J054583. ISSN 0001-1452. Volltext nicht frei. | ![]() |
Costantini, Marco and Hein, Stefan and Henne, Ulrich and Koch, Stefan and Sachs, Werner and Schojda, Lukas and Rosemann, Henning and Koop, Lars (2013) The effect of pressure gradient and a non-adiabatic surface on boundary layer transition investigated by means of TSP. AIAA. 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 07. - 10. Jan. 2013, Grapevine (Dallas/Ft. Worth Region), Texas, USA. doi: 10.2514/6.2013-1137. Volltext nicht frei. | ![]() |
Cécora, René-Daniel and Rosemann, Henning (2012) Experimentelle und numerische Untersuchungen am Laminarprofil NLF9. 18. DGLR-Fach-Symposium der STAB, 06. -07. Nov. 2012, Stuttgart, Deutschland. Volltext nicht online. |
Cécora, René-Daniel and Rosemann, Henning (2014) Experimental and Numerical Investigation of the Laminar Airfoil NLF9. In: New Results in Numerical and Experimental Fluid Mechanics IX Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 124. Springer Verlag, Cham Heidelberg New York Dordrecht London. pp. 193-201. ISBN 978-3-319-03157-6. ISSN 1612-2909. Volltext nicht online. |
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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. |
Dechamps, Xavier and Hein, Stefan (2016) Extension of the PSE code NOLOT for transition analysis in rotating reference frames. 20. DGLR-Fachsymposium der STAB, 08. - 09. Nov. 2016, Braunschweig, Deutschland. | ![]() |
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Eisfeld, Bernhard and Rütten, Markus (2012) A Coupled Heat Exchanger Boundary Condition for Pre-Design of Air-Intake Positions. AIAA. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 09. - 12. Jan. 2012, Nashville, Tennesee, USA. doi: 10.2514/6.2012-463. Volltext nicht online. |
Erdi-Betchi, Ali (2004) Beschichtungsverfahren Kaltgasspritzen: Experimentelle und numerische Untersuchungen der Dynamik der partikelbeladenen Überschallströmung. DLR-Forschungsbericht. 2004 - 20. Dissertation. 121 S. Volltext nicht online. |
Erdmann, Ralf and Leuckert, Janin and Rosemann, Henning and Nitsche, Wolfgang (2013) Active Tollmien Schlichting Wave Control with a Membrane Actuator in Compressible Flows. In: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Fluid Mechanics and Multidisciplinary Design, Vol. 121. Springer Verlag, Heidelberg New York Dordrecht London. pp. 253-260. doi: 10.1007/978-3-642-35680-3_31. ISBN 978-3-642-35679-7. ISSN 1612-2909. Volltext nicht online. |
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Gardner, Anthony and Jacobs, Markus (2005) (Vertraulich). DLR-Interner Bericht. DLR-IB-224-2005-C-11. 334 S. Volltext nicht online. |
Gardner, Anthony D. (2009) (Vertraulich). DLR-Interner Bericht. DLR-IB 224-2008 C36. DLR. 73 S. Volltext nicht online. |
Gardner, Anthony D. (2009) Numerical investigation of air jets for dynamic stall control on the OA209 airfoil. DLR-Interner Bericht. DLR-IB 224-2009 A 32. 79 S. Volltext nicht online. |
Gardner, Anthony Donald (2006) Investigation of the sting interference effect due to the TWG 15-degree, 25-degree and 45-degree rolling stings. DLR-Interner Bericht. IB 2006 A 32. 234 S. Volltext nicht online. |
Gardner, Anthony Donald (2006) Vertraulich. DLR-Interner Bericht. IB 224-2006 C 36. 99 S. Volltext nicht online. |
Gardner, Anthony Donald (2007) Design and Optimisation of the Valve Contour (Conus) of the DNW-KRG for an extended Mach number range. DLR-Interner Bericht. DLR-IB 224-2007 A02. 75 S. Volltext nicht online. |
Gardner, Anthony Donald (2007) (Vertraulich). DLR-Interner Bericht. DLR-IB 224-2007 C20. 233 S. Volltext nicht online. |
Gardner, Anthony Donald (2007) HyShot scramjet testing in the HEG. DLR-Forschungsbericht. FB 2007-14. Dissertation. University of Queensland, Australia. 302 S. Volltext nicht online. |
Gardner, Anthony Donald (2007) HyShot scramjet testing in the HEG. Dissertation, University of Queensland, Australia. Volltext nicht online. |
Gardner, Anthony Donald (2008) (Vertraulich). DLR-Interner Bericht. DLR-IB 224-2008 C27. 47 S. Volltext nicht online. |
Gardner, Anthony Donald (2008) Pre-Computations for the iGREEN Wing-Tailplane Interference Experiment in the TWG. DLR-Interner Bericht. DLR-IB 224-2008 A19. 132 S. Volltext nicht online. |
Gardner, Anthony Donald (2008) (Vertraulich). DLR-Interner Bericht. DLR-IB-224-2008-C31. 43 S. Volltext nicht online. |
Gardner, Anthony Donald (2008) (Vertraulich). DLR-Interner Bericht. DLR-IB 224-2008 C32. 120 S. Volltext nicht online. |
Gardner, Anthony Donald (2010) Interview, „RWTH-THEMEN“ zur thema TANDEN-mentoring-Programm. [Other] Volltext nicht online. |
Gardner, Anthony Donald (2010) Numerical investigation of the effect of intake integration at transonic speeds on the DLR-F17E UCAV model for the TWG. DLR-Interner Bericht. DLR-IB 224 2010 A 40. 47 S. Volltext nicht online. |
Gardner, Anthony Donald and Jacobs, Markus (2006) (Vertraulich). DLR-Forschungsbericht. DLR-IB 224-2006-C-24. 93 S. Volltext nicht online. |
Gardner, Anthony Donald and Knopp, Tobias and Richter, Kai and Rosemann, Henning (2013) Numerical Investigation of Pulsed Air Jets for Dynamic Stall Control on the OA209 Airfoil. In: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 121. Springer Verlag, Heidelberg New York Dordrecht London. pp. 287-295. doi: 10.1007/978-3-642-35680-3_35. ISBN 978-3-642-35679-7. ISSN 1612-2909. Volltext nicht online. |
Gardner, Anthony Donald and Nitzsche, Jens and Neumann, Jens and Richter, Kai and Rosemann, Henning and Voß, Ralph (2006) Adaptive load redistribution using mini-TEDs. 25th International Congress of the Aeronautical Sciences, [2006-09-03-2006-09-08], Hamburg, Germany. ISBN 0-9533991-76. Volltext nicht online. |
Gardner, Anthony Donald and Richter, Kai and Rosemann, Henning (2006) Simulation of Oscillating Airfoils and Moving Flaps Employing the DLR-TAU Unsteady Grid Adaptation. STAB 2006, 2006-11-29 - 2006-12-02, Darmstadt. Volltext nicht online. |
Gardner, Anthony Donald and Richter, Kai and Rosemann, Henning (2008) Prediction of the Wind Tunnel Sidewall Effect for the iGREEN Wing-Tailplane Interference Experiment in the TWG. [Other] (Submitted) Volltext nicht online. |
Gardner, Anthony Donald and Richter, Kai and Rosemann, Henning (2008) Prediction of the Wind Tunnel Sidewall Effect for the iGREEN Wing-Tailplane Interference Experiment. 16. DGLR-Fach-Symposium der STAB, 2008-11-03 - 2008-11-04, Aachen. Volltext nicht online. |
Gardner, Anthony Donald and Richter, Kai and Rosemann, Henning (2010) Numerical Investigation of Air Jets for Dynamic Stall Control on the OA209 Airfoil. 36th European Rotorcraft Forum, 7. - 9. September 2010, Paris, France. Volltext nicht online. |
Gardner, Anthony Donald and Richter, Kai and Rosemann, Henning (2010) Prediction of the Wind Tunnel Sidewall Effect for the iGREEN Wing-Tailplane Interference Experiment. In: New Results in Numerical and Experimental Fluid Mechanics VII Notes on Numerical Fluid Mechanics and Multidisciplanary Design, 112. Springer Verlag Berlin, Heidelberg. pp. 75-82. doi: 10.1007/978-3-642-14243-7_10. ISBN 978-3-642-14242-0. ISSN 1612-2909. Volltext nicht online. |
Gardner, Anthony Donald and Richter, Kai and Rosemann, Henning (2011) Numerical investigation of air jets for dynamic stall control on the OA209 airfoil. CEAS Aeronautical Journal. Springer. doi: 10.1007/s13272-011-0002-z. Volltext nicht online. |
Gardner, Anthony and Kaufmann, Kurt and Richter, Kai (2016) Investigation of three-dimensional Dynamic Stall. In: High Performance Computing in Science and Engineering Leibniz-Rechenzentrum (LRZ). pp. 124-125. ISBN 978-3-9816675-1-6. Volltext nicht online. |
Gardner, Anthony Donald and Klein, Christian and Richter, Kai and Wolf, C. Christian and Bauknecht, Andre and Merz, Christoph B. (2016) Vorlesung: Strömungsmesstechnik. Uni. Clausthal Vorlesung, 08. - 11. März 2016, Clausthal, Deutschland. Volltext nicht online. |
Gardner, Anthony Donald and Richter, Kai (2016) Transition Determination on a Periodic Pitching Airfoil Using Phase Averaging of Pressure Data. In: New Results in Numerical and Experimental Fluid Mechanics X Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 132. Springer International Publishing Switzerland 2016. pp. 291-301. doi: 10.1007/978-3-319-27279-5_26. ISBN 978-3-319-27278-8. ISSN 1612 - 2909. Volltext nicht online. |
Geissler, W. and Dietz, G. and Mai, H. (2005) Dynamic stall on a supercritical airfoil. Aerospace Science and Technology, Vol. 9 (No. 5), pp. 390-399. Volltext nicht online. |
Geissler, Wolfgang and Haselmeyer, Hartmut (2006) Investigation of Dynamic Stall On-Set. Aerospace Science and Technology, pp. 590-600. Elsevier Masson SAS. doi: 10.1016/j.ast2006.05.001. Volltext nicht online. |
Geissler, Wolfgang and Raffel, Markus and Dietz, Guido and Mai, Holger (2005) Helicopter Aerodynamics with Emphasis Placed on Dynamic Stall. EUROMECH Colloquium 464b Wind Energy, 2005-10-04 - 2005-10-07, Oldenburg, Deutschland (Europa). Volltext nicht online. |
Geissler, Wolfgang and Sobieczky, Helmut and Trenker, Markus (2000) New Rotor Airfoil Design Procedure for Unsteady Flow Control. 26th European Rotorcraft Forum, The Hague, The Netherlands, Sept. 26-29, 2000, [2000-09-26 - 2000 - 2000 09 - 29], The Hague (Metherland). Volltext nicht online. |
Geißler, W. and Raffel, M. and Favier, D. and Maresca, C. and Berton, E. and Nsi Mba, M. (2005) Numerical and Experimental Investigations of Dynamic Stall on both NACA0012 and OA209 Airfoil Sections. DLR-Interner Bericht. DLR-IB 224 - 2005 A 03. 38 S. Volltext nicht online. |
Geißler, Wolfgang and Koch, Stefan (2003) Adaptive Airfoil. In: IUTAM Symposium Transsonicum IV, 73, pp. 303-310. Kluwer Academic Publishers. IUTAM Symposium Transonicum IV, 2002-09-02 - 2002-09-06, Göttingen, Bundesrepublik Deutschland. ISBN 1-4020-1608-5. Volltext nicht online. |
Goerttler, Andreas and Gardner, Anthony and Richter, Kai (2016) Unsteady boundary layer transition detection by automated analysis of hot film data. 20. DGLR-Fachsymposium der STAB, 08.-09. Nov. 2016, Braunschweig, Deutschland. Volltext nicht online. |
Guyot, Daniel and Schülein, Erich (2005) Untersuchungen zum widerstandsarmen Gitterflügel. 12.STAB-Workshop, 2005-11-08 - 2005-11-09, DLR Göttingen. Volltext nicht online. |
Guyot, Daniel and Schülein, Erich (2007) Novel Locally Swept Lattice Wings for Missile Control at High Speeds. 45th AIAA Aerospace Sciences Meeting and Exhibit, 2007-01-08 - 2007-01-11, Reno, Nevada (USA). Volltext nicht online. |
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Hanifi, Ardeshir and Hein, Stefan and Romano, D. G. and Minervino, M. and Würz, W. and Borodulin, V. I. and Ivanov, A. V. and Kachanov, Y. S. (2014) Numerical and Experimental Realization of an Infinite-Swept-Wing Boundary-Layer Flow in a Wind Tunnel. 17th International Conference on the Methods of Aerophysical Research, 30. June - 06. July 2014, Novosibirsk, Russia. ISBN 978-5-9905592-8-8. Volltext nicht online. |
Hebler, Anne and Schojda, Lukas and Mai, Holger (2013) Experimental Investigation of the Aeroelastic Behavior of a Laminar Airfoil in Transonic Flow. In: Proceedings "IFASD 2013". International Forum on Aeroelasticity and Structural Dynamics (IFASD), 24. - 26. Juni 2013, Bristol, England. Volltext nicht online. |
Hein, Stefan and Koch, Werner and Nannen, Lothar (2012) Trapped modes and Fano resonances in two-dimensional acoustical duct-cavity systems. Journal of Fluid Mechanics, Vol. 692, pp. 257-287. Cambridge University Press. doi: 10.1017/jfm.2011.509. ISSN 0022-1120. Volltext nicht online. |
Hein, Stefan and Schülein, Erich and Hanifi, Ardeshir and Sousa, Joao and Arnal, Daniel (2009) Laminar flow control by suction at Mach 2. CEAS/KATnet II Conference on Key Aerodynamic Technologies, 2009-05-12 - 2009-05-14, Hilton Hotel Bremen, Germany. Volltext nicht online. |
Hein, Stefan and Schülein, Erich and Hanifi, Ardeshir and Sousa, Joao and Arnal, Daniel (2010) Laminar flow control by suction at Mach 2. In: Seventh IUTAM Symposium on Laminar-Turbulent Transition IUTAM Bookseries, Vol. 18. Springer, Dordrecht Heidelberg London New York. pp. 189-194. doi: 10.1007/978-90-481-3723-7_29. ISBN 978-90-481-3722-0 (Print), 978-90-481-3723-7 (Online). ISSN 1875-3507. Volltext nicht online. |
Hein, Stefan and Schülein, Erich and Hanifi, Ardeshir and Sousa, Joao and Arnal, Daniel (2009) Laminar flow control by suction at Mach 2. IUTAM Symposium on Laminar-Turbulent Transition, 2009-06-23 - 2009-06-26, Stockholm, Sweden. Volltext nicht online. |
Hein, Stefan and Schülein, Erich (2007) Preparation and analysis of an RWG experiment on laminar flow control by suction at Mach 2 within SUPERTRAC. 13. STAB-Workshop, 2007-11-14 - 2007-11-15, Göttingen, Germany. Volltext nicht online. |
Hein, Stefan and Schülein, Erich (2008) Transition control by suction at Mach 2. 7th ERCOFTAC SIG33 - FLUBIO Workshop on Open Issues in Transition and Flow Control, 2008-10-16 - 2008-10-18, Santa Margherita Ligure, Italy. Volltext nicht online. |
Hein, Stefan (2014) Linear and nonlinear growth of secondary instabilities of crossflow vortices studied by PSE. IUTAM – ABCM Symposium on Laminar-Turbulent Transition, 08. - 12. Sept. 2014, Rio de Janeiro, Brazil. Volltext nicht online. |
Hein, Stefan (2014) Some Applications of Linear and Nonlinear Instability Analysis at DLR Göttingen. VKI Lecture Series: Progress in Flow Instability Analysis and Laminar-Turbulent Transition Modeling, 02. - 06. Juni 2014, Rhode-Saint-Genèse, Belgium. Volltext nicht online. |
Hein, Stefan (2014) Linear and nonlinear growth of secondary instabilities of crossflow vortices studied by PSE. Seminar on Math. Dept., Imperial College London, 12. Dec. 2014, London, United Kingdom. Volltext nicht online. |
Hein, Stefan (2015) Transition Modelling for High-Speed Flows. ERCOFTAC SIG 10 Course: Transition Modelling III, 22. May 2015, Munich, Germany. Volltext nicht online. |
Hein, Stefan (2015) Title confidential. Project Report. BUTERFLI_D3.6_DLR_25052015. 22 S. Volltext nicht online. |
Hein, Stefan (2015) Title confidential. Project Report. BUTERFLI_D3.7_DLR_13052015. 26 S. Volltext nicht online. |
Hein, Stefan (2016) Linear and Nonlinear Growth of Secondary Instabilities of Stationary Crossflow Vortices Studied by Parabolized Stability Equations. 20. DGLR-Fachsymposium der STAB, Braunschweig, Deutschland. Volltext nicht online. |
Hein, Stefan and Hanifi, Ardeshir and Dadfar, Reza and Vermeersch, Olivier (2015) Title confidential. Project Report. BUTERFLI_Deliverable_D3.4. 17 S. Volltext nicht online. |
Heine, Benjamin and Mulleners, Karen and Gardner, Anthony and Mai, Holger (2009) On the effects of leading edge vortex generators on an OA209 airfoil. ODAS 2009 - 10th ONERA-DLR Aerospace Symposium, 6. Okt. - 8.Okt 2009, Berlin, Germany. | ![]() |
Henne, Ulrich and Höhler, Gebhard and Klein, Christian and Rein, Martin and Sachs, Werner and Schütte, Andreas (2005) Stationäre Druckmessungen mittels PSP und Druckanbohrungen, sowie Kraft- und Momentenmessungen am X-31 RC-Modell im DNW-NWB. DLR-Interner Bericht. DLR-IB 224-2005 A 16. 71 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. doi: 10.2514/6.2012-3325. | ![]() |
Huber, Kerstin Claudie and Schütte, Andreas and Rein, Martin and Löser, Thomas (2016) Experimental aerodynamic assessment and evaluation of an agile highly swept aircraft configuration. CEAS Aeronautical Journal, 8, pp. 17-29. Springer. doi: 10.1007/s13272-016-0219-y. ISSN 1869-5582. Volltext nicht frei. | ![]() |
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Jaffrezic, Benoit (2011) Store Separation – Literature Review. DLR-Interner Bericht. DLR-IB 224-2011 A 63. 63 S. Volltext nicht online. |
Jaffrézic, Benoit and Rütten, Markus and Rosemann, Henning (2015) Aerodynamics Flight Mechanics Approach on Compact Domains for Air Vehicle Separation. AIAA-Aviation - Modeling and Simulation Technologies Conference, 22. - 26. June 2015, Dallas, TX, USA. doi: 10.2514/6.2015-2949. ISBN 978-1-62410-355-1. Volltext nicht online. |
Jaffrézic, Benoît (2014) Novel Aerodynamics–Flight Mechanics Approach on Compact Domains. DLR-Interner Bericht. DLR-IB 224-2014 A 96. 44 S. Volltext nicht online. |
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Klein, Alexander and Richter, Kai and Altmikus, Andree and Lutz, Thorsten and Krämer, Ewald (2009) Unsteady Criteria for Rotor Blade Airfoil Design. 35th European Rotorcraft Forum, 22.-25. September 2009, Hamburg. Volltext nicht online. |
Klinkov, Konstantin V and Rein, Martin (2005) Spectral analysis of unsteady interactions between a supersonic jet and a plate. 12. STAB-Workshop, 2005-09-11, Göttingen. Volltext nicht online. |
Klinkov, Konstantin V and Rein, Martin (2006) Multi-exposure method for studying compressible multiphase flows. 12th Int. Symp. Flow Visualization, 2006-09-10 - 2006-09-14, Göttingen. (Unpublished) Volltext nicht online. |
Klinkov, Konstantin V. and Erdi-Betchi, Ali and Rein, Martin (2006) Behavior of Supersonic Overexpanded Jets Impinging on Plates. In: New Results in Numerical and Experimental Fluid Mechanics, 92 (V), 168-175-175. Springer. 14th STAB/DGLR Symposium, 2004-11-16 - 2004-18-11, Bremen. ISBN 3-540-33286-3. Volltext nicht online. |
Klinkov, Konstantin V. and Rein, Martin (2006) Luminescence induced by high-velocity impacts of metallic particles on metal surfaces. Journal of Applied Physics, 100, 013529-1-013529-5. doi: 10.1063/1.2209539. Volltext nicht online. |
Klinkov, Konstantin V. and Rein, Martin (2006) Spectral analysis of sound generation by supersonic impinging jets. ISSW26, 2007-07-15 - 2007-07-20, Göttingen. Volltext nicht online. |
Klinkov, Sergei V. and Kosarev, Vladimir F. and Rein, Martin (2005) Cold spray deposition: Significance of particle impact phenomena. Aerospace Science and Technology, 9 (7), pp. 582-591. doi: 10.1016/j.ast.2005.03.005. Volltext nicht online. |
Knopp, Tobias and Schanz, Daniel and Novara, Matteo and Schröder, Andreas and Schülein, Erich and Reuther, Nico and Kähler, Christian (2016) A new Experiment of a turbulent boundary layer flow at adverse pressure gradient for validation and improvement of RANS turbulence models. STAB Symposium 2016 in Braunschweig, 08.-09. Nov. 2016, Braunschweig, Deutschland. Volltext nicht online. |
Koch, Stefan (2004) Zeitliche und räumliche Turbulenzentwicklung in einem Rohrwindkanal und deren Einfluss auf die Transition an Profilmodellen. DLR-Forschungsbericht. 2004 - 19. Dissertation. 137 S. Volltext nicht online. |
Koch, Stefan (2009) Titel confidential. DLR-Interner Bericht. DLR-IB 224-2009 C 43. 48 S. Volltext nicht online. |
Koch, Stefan (2013) Experimente am integrierten Einlauf mit Grenzschichteintrag im DNW-KRG. 16. STAB-Workshop, Göttingen, Deutschland. Volltext nicht online. |
Koch, Stefan and Gardner, Anthony Donald (2011) Investigation of integrated engine intake designs for a UCAV using the DNW-KRG and DLR-TAU. “CFD and Experiment – Integration of Simulation” of the DGLR-Querschnittsbereich Thermo- and Fluiddynamics, 05.-06. Apr. 2011, Göttingen, Germany. Volltext nicht online. |
Koch, Stefan and Richter, Kai and Gardner, Anthony D. and Rosemann, Henning (2007) Confidential. DLR-Interner Bericht. DLR-IB 224-2007 C 19. 85 S. (Unpublished) Volltext nicht online. |
Koch, Stefan and Richter, Kai and Rosemann, Henning (2007) Confidential. DLR-Interner Bericht. DLR-IB 224-2007 C 18. 72 S. (Unpublished) Volltext nicht online. |
Koch, Stefan and Rosemann, Henning and Fey, Uwe and Egami, Yasuhiro (2010) Titel confidential. DLR-Interner Bericht. DLR-IB 224-2008 C 38. Deutsches Zentrum für Luft- und Raumfahrt e.V.. 67 S. Volltext nicht online. |
Koch, Stefan and Rütten, Markus and Rein, Martin (2015) Experimental and Numerical Investigations on Integrated Intakes for Agile and Highly Swept Aircraft Configurations. In: 64. Deutscher Luft- und Raumfahrtkongress (370173), pp. 1-10. 64. Deutscher Luft- und Raumfahrtkongress, 22. - 24. Sept. 2015, Rostock, Deutschland. Volltext nicht online. |
Koch, Stefan and Rütten, Markus and Rein, Martin (2016) Untersuchung zu Gesamtdruckverlusten in der Verdichtereintrittsebene eines integrierten Einlaufs mit eingetragenem Wirbel. 20. DGLR-Fachsymposium der STAB, 08.-09. Nov. 2016, Braunschweig, Deutschland. Volltext nicht online. |
Kovar, Anke (2005) Validation of computational fluid dynamics simulation methods for turbulent subsonic and transonic flows about missile configurations (GARTEUR AG42). Other. 2 S. Volltext nicht online. |
Kovar, Anke and Schülein, Erich (2005) Numerische Simulation von Querschubstrahlen zur Steuerung hochagiler Flugkörper. Other. 2 S. Volltext nicht online. |
Kovar, Anke and Schülein, Erich (2006) Comparison of experimental and numerical investigations on a jet in a supersonic cross-flow. The Aeronautical Journal, Volume 110 (Number 1108), pp. 353-360. Royal Aeronautical Society (RAeS). Volltext nicht online. |
Kovar, Anke and Schülein, Erich (2006) Study of Supersonic Flow Separation Induced by a Side Jet and its Control. Contributions to the 14th STAB/DGLR Symposium, Bremen, ZARM. Germany 2004, Volume 92, pp. 176-183. Springer. ISBN 3-540-33286-3. Volltext nicht online. |
Kovar, Anke and Schülein, Erich (2006) Effect of Side Jets in a Supersonic Flow Measured and Calculated on a Flat Plate and a Generic Missile Configuration. In: Innovative Missile Systems, 37-1-37-14. RTO-MP-AVT 135, 2006-05-15 - 2006-05-19, Amsterdam, NL. Volltext nicht online. |
Kovar, Anke and Schülein, Erich (2004) Numerische Modellierung von Querschubstrahlen an einer ebenen Platte. Other. 2 S. (Unpublished) Volltext nicht online. |
Kovar, Anke and Schülein, Erich (2003) Experimentelle und numerische Untersuchung der aerodynamischen Wechselwirkung der Querschubstrahlsteuerung. Other. 2 S. Volltext nicht online. |
Kovar, Anke and Schülein, Erich (2002) Untersuchung aerodynamischer Wechselwirkungen der Querschubstrahlsteuerung. Other. 2 S. Volltext nicht online. |
Kovar, Anke and Schülein, Erich (2008) Grundlagenexperimente zur Seitenstrahlsteuerung von Flugkörpern und ihre numerische Simulation. DLR-Interner Bericht. DLR-IB 224-2007A16. 40 S. Volltext nicht online. |
Kovar, Anke and Schülein, Erich and Emunds, Hans (2003) Untersuchungen zur aerodynamischen Wechselwirkung der Querschubsteuerung bei hochagilen Flugkörpern. DLR-IB (647-2003/22). Volltext nicht online. |
Kovar, Anke and Schülein, Erich and Emunds, Hans (2004) Numerische und experimentelle Untersuchungen zu Querschubstrahlen in Einzel- und Mehrfachanordnung. Symposium "Wirkung und Schutz, Explosivstoffe", 2004-11-08 - 2004-11-10, Mannheim. (Unpublished) Volltext nicht online. |
Kovar, Anke (2007) Validation of computational fluid dynamics simulation methods for turbulent subsonic and transonic flows about missile configurations. In: Jahresbericht 2007. 13. STAB-Workshop, 2007-11-14 - 2007-11-16, Göttingen, Deutschland. (Submitted) | ![]() |
Kovar, Anke and Hannemann, Volker and Karl, Sebastian and Schülein, Erich (2007) About the Assessment of Heat Flux and Skin Friction of the DLR TAU-code for Turbulent Supersonic Flows. In: 8th Onera - DLR Aerospace Symposium Conference Proceedings. 8th Onera - DLR Aerospace Symposium, 2007-10-17 - 2007-10-19, Göttingen. (Submitted) | ![]() |
Kovar, Anke and Schülein, Erich (2008) Visualisation and Prediction of Heat Flux Measured on the Example of Side Jet Control. In: 13th International Symposium on Flow Visualisation. 13th International Symposium on Flow Visualisation / 12th French Congress FLUVISU 12, 2008-07-01 - 2008-07-04, Nizza, Frankreich. (Submitted) Volltext nicht frei. | ![]() |
Kovar, Anke and Schülein, Erich and Hannemann, Volker and Karl, Sebastian (2007) About the Heat Flux and Skin Friction Prediction of the DLR TAU-code for Turbulent Supersonic Flows. ODAS 2007 8th ONERA-DLR Aerospace Symposium, 2007-10-17 - 2007-10-19, Göttingen, Germany. (Unpublished) Volltext nicht frei. | ![]() |
Krenkel, Lars (2012) Untersuchung des Einflusses von Wirbelgeneratoren auf die Stoß-/Grenzschicht-Wechselwirkung. DLR-Forschungsbericht. DLR-FB--2012-10. Dissertation. Rheinisch-Westfälischen Technischen Hochschule Aachen. 177 S. Volltext nicht frei. | ![]() |
Kreplin, Hans-Peter and Höhler, Gebhard and Koch, Stefan (2007) Surface hot film measurements on a swept airfoil model in PETW. DLR-Interner Bericht. DLR-IB 224-2007-C10. 25 S. Volltext nicht online. |
Kreplin, Hans-Peter and Höhler, Gebhard and Koch, Stefan (2007) Surface hot film measurements on the slat of the KH3Y high lift model in ETW. DLR-Interner Bericht. DLR IB 224-2007 C11. 26 S. Volltext nicht online. |
Krogmann, Paul and Schülein, Erich and Stanewsky, Egon (1996) Presentation of experimental facilities. Choice of test geometry and conditions // Preparatory activities for theoretical and experimental tasks in turbulence modeling of hypersonic air intake flows (edited by S.Wallin). Other. FFA TN 1996-46. 20 S. Volltext nicht online. |
Krüger, Wolf R. and Rosemann, Henning (2006) Die intelligentere Struktur gibt nach. DLR Nachrichten (115). Deutsches Zentrum für Luft- und Raumfahrt (DLR). ISSN 0937-0420. | ![]() |
König, Benedikt and Pätzold, Martin and Lutz, Thorsten and Krämer, Ewald and Rosemann, Henning and Richter, Kai and Uhlemann, Heiko (2009) Numerical and Experimental Validation of Three-Dimensional Shock Control Bumps. Journal of Aircraft, 46 (2), pp. 675-682. American Institute of Aeronautics and Astronautics (AIAA). Volltext nicht online. |
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Le Pape, Arnaud and Richter, Kai and Knopp, Tobias and Costes, Michel and Gleize, Vinvent and Gardner, Anthony Donald (2009) Validation of Structured and Hybrid Numerical Methods for Improved Two-Dimensional Dynamic Stall Prediction. ODAS 2009 - 10th ONERA-DLR Aerospace Symposium, 06.-08. Oktober 2009, Berlin. Volltext nicht online. |
Lichtmes, Martin (2015) Numerische Untersuchung zur Grenzschichtstabilität an der Atmosphäreneintrittskapsel des Mars Science Laboratory im hypersonischen Strömungsfeld. Master's, Hochschule Trier. Volltext nicht online. |
Lichtmes, Martin (2015) Numerische Untersuchung zur Grenzschichtstabilität an der Atmosphäreneintrittskapsel des Mars Science Laboratory im hypersonischen Strömungsfeld. DLR-Interner Bericht. DLR-IB 224-2015 A 109. 109 S. Volltext nicht online. |
Lindermeir, Erwin and Rütten, Markus (2014) MIRA: An IR Signature Model for Unmanned Aerial Vehicles (UAV). In: Proceedings of Optro 2014 - International Sypmposium on Optronics in Defence and Security, pp. 1-9. Optro 2014 - International Symposium on Optronics in Defence and Security, 28.-30. Jan. 2014, Paris, Frankreich. Volltext nicht online. |
Lindermeir, Erwin and Rütten, Markus (2014) The IR Signature Model MIRA. 10th International IR Target and Background Modeling and Simulation Workshop, 23.-26. Jun. 2014, Ettlingen, Germany. Volltext nicht online. |
Lindermeir, Erwin and Rütten, Markus (2015) Infrarotsignaturbewertung von agilen und hoch gepfeilten Flugzeugkonfigurationen. Deutscher Luft- und Raumfahrtkongress 2015, 22.-24.Sept. 2015, Rostock, Deutschland. | ![]() |
Lohse, Jakob and Barth, Hans Peter and Nitsche, Wolfgang (2016) Active control of crossflow-induced transition by means of in-line pneumatic actuator orifices. Experiments in Fluids, 57 (124), pp. 1-10. Springer Nature. doi: 10.1007/s00348-016-2213-x. ISSN 0723-4864. Volltext nicht online. |
Lunte, Jens and Schülein, Erich (2016) Skin friction measurements in three-dimensional flows by white-light oil-film interferometry. 20. DGLR-Fachsymposium der STAB, 08.11.2016, Braunschweig, Deutschland. Volltext nicht online. |
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Merz, Christoph B. and Wolf, Christian C. and Richter, Kai and Kaufmann, Kurt and Mielke, Alina and Raffel, Markus (2015) Spanwise Differences in Static and Dynamic Stall on a Pitching Rotor Blade Tip Model. In: 41st European Rotorcraft Forum 2015, ERF 2015 (77), pp. 1-14. European Rotorcraft Forum 2015, 01. – 04. September 2015, Munich, Germany. Volltext nicht online. |
Merz, Christoph B. and Wolf, Christian C. and Richter, Kai and Kaufmann, Kurt and Raffel, Markus (2016) Experimental Investigation of Dynamic Stall on a Pitching Rotor Blade Tip. In: New Results in Numerical and Experimental Fluid Mechanics X Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 132. Springer International Publishing Switzerland 2016. pp. 339-348. doi: 10.1007/978-3-319-27279-5_30. ISBN 978-3-319-27278-8. ISSN 1612-2909. Volltext nicht online. |
Mey, Tobias and Rein, Martin and Großmann, Peter and Mann, Klaus (2012) Brilliance improvement of laser-produced soft x-ray plasma by a barrel shock. New Journal of Physics, 14 (7), pp. 1-15. Institute of Physics (IOP) Publishing. doi: 10.1088/1367-2630/14/7/073045. ISSN 1367-2630. Volltext nicht online. |
Mulleners, Karen and Rütten, Markus (2016) Analysis of intermittent trailing edge vortex shedding using recurrence plots. 18th International Symposium on the Applications of Laser and Imaging Techniques to Fluid Mechanics, 04.-07. Juli 2016, Lisbon, Portugal. Volltext nicht online. |
Muñoz, Frederico and Radespiel, Rolf and Theiss, Alexander and Hein, Stefan (2014) Experimental and Numerical Investigation of Instabilities in Conical Boundary Layers at Mach 6. American Institute of Aeronautics and Astronautics. AIAA Aviation and Aeronautics Forum and Exposition (AVIATION 2014), 16. – 20. June 2014, Atlanta, GA, USA. doi: 10.2514/6.2014-2778. Volltext nicht online. |
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Pallek, Dieter and Becker, Uwe and Otter, Dirk (2007) Title confidential. DLR-Interner Bericht. DLR-IB 224-2006 C 37. 73 S. Volltext nicht online. |
Paul, Michael (2015) Low Speed Experimental and Numerical Investigations on Unconventional Control Concepts for Agile and Highly Swept Aircraft Configurations. 17. STAB-Workshop, 10.-11. November 2015, Göttingen, Deutschland. Volltext nicht online. |
Paul, Michael and Rein, Martin (2016) Transonic Numerical and Experimental Investigation into Unconventional Lambda Wing Control Surfaces. SciTech 2016 - 54th AIAA Aerospace Sciences Meeting, 4-8 January 2016, San Diego, CA, USA. doi: 10.2514/6.2016-0799. Volltext nicht online. |
Paul, Michael and Rütten, Markus and Rein, Martin (2015) Low Speed Experimental and Numerical Investigations on Unconventional Control Concepts for Agile and Highly Swept Aircraft Configurations. DGLR Kongress 2015, 22. - 24. Sept. 2015, Rostock, Deutschland. Volltext nicht online. |
Perez, Jose Miguel and Franco, Juan Alberto and Paredes, Pedro and Hein, Stefan and Hannemann, Volker and Theofilis, Vassilios (2015) Stability analysis of hypersonic flow over a backstep in chemical equilibrium. 3rd TRR40 Summer Research Program, 20. Juli - 14. Aug. 2015, München. Volltext nicht online. |
Perraud, Jean and Archambaud, Jean-Pierre and Schrauf, Geza and Donelli, Raffaele and Hanifi, Ardeshir and Quest, Jürgen and Hein, Stefan and Streit, Thomas and Fey, Uwe and Egami, Yasuhiro (2010) High Reynolds number transition experiments in ETW (TELFONA project). In: IUTAM Bookseries, Vol. 18. Springer, Dordrecht Heidelberg London New York. pp. 553-556. doi: 10.1007/978-90-481-3723-7_98. ISBN 978-90-481-3722-0 (Print), 978-90-481-3723-7 (Online). ISSN 1875-3507. Volltext nicht online. |
Prananta, Bimo B and Deck, Sebastian and d'Espiney, Paulo and Jirasek, Adam and Kovar, Anke and Leplat, Michel and Nottin, Christophe and Petterson, Kristian and Wrisdale, Ian (2008) Numerical simulations of turbulent subsonic and transonic flows about missile configurations Final report of the GARTEUR (AD) AG42 Missile Aerodynamics. Project Report. NLR-TR-2007-704 GARTEUR TP-166. Volltext nicht online. |
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Rabe, Katharina and Rosemann, Henning and Schülein, Erich (2011) Titel confidential. DLR-Interner Bericht. DLR-IB 224-2011 C 94. 26 S. Volltext nicht online. |
Raffel, Markus and Bauknecht, André and Bertsch, Lothar and Gardner, Anthony and Richter, Kai (2016) Hubschrauberaerodynamik. [Other] Volltext nicht online. |
Raffel, Markus and Gardner, Anthony and Klein, Christian and Richter, Kai and Bauknecht, Andre and Henning, Arne (2016) Vorlesung: Strömungsmesstechnik. Universität Hannover Vorlesung, 30.Mai - 03.Juni 2016, Göttingen, Deutschland. Volltext nicht online. |
Rein, Martin (2005) Wechselwirkung von Überschallfreistrahlen mit einer ebenen Wand. Kolloquium über neuere Arbeiten auf dem Gebiete der Mechanik und Strömungsmechanik, 2005-05-31, Wien. (Unpublished) Volltext nicht online. |
Rein, Martin (2006) Experimental simulation of maneuvers in a wind-tunnel. UC Davis. [Other] (Unpublished) Volltext nicht online. |
Rein, Martin (2006) Experimental simulation of maneuvers in a wind-tunnel. [Other] (Unpublished) Volltext nicht online. |
Rein, Martin (2007) Konzept für Tests der Abrasivwirkung partikelbeladener Innenströmungen an Wandmaterialien. DLR-Interner Bericht. DLR-IB 224-2007 C03. Volltext nicht online. |
Rein, Martin (2007) Manöver Simulation im Windkanal. Kolloquium über neuere Arbeiten auf dem Gebiet der Mechanik und Strömungslehre, 2007-03-28, Wien. Volltext nicht online. |
Rein, Martin (2007) From low velocity droplet impact to high velocity particle impact. CIRF Seminar Series, 2007-10-10, Santa Barbara, CA (USA). Volltext nicht online. |
Rein, Martin (2007) Cold spray deposition: A study of supersonic jet impingement. Mechanical and Aerospace Engineering Seminar Series, 2007-10-17, Irvine, CA (USA). Volltext nicht online. |
Rein, Martin (2007) Simple and two-phase supersonic jets impinging on plates. GALCIT Colloquium, 2007-10-26, Pasadena, CA (USA). Volltext nicht online. |
Rein, Martin (2008) Experimental simulation of maneuvers in a wind-tunnel. Center of Excellence for Research and Education on Complex Functional Mechanical Systems Seminar, 2008-02-13, Kyoto (Japan). (Unpublished) Volltext nicht online. |
Rein, Martin (2008) Cold spray deposition: A study of supersonic jet impingement. Center of Excellence for Research and Education on Complex Functional Mechanical Systems Seminar, 2008-02-20, Kyoto (Japan). (Unpublished) Volltext nicht online. |
Rein, Martin (2008) Wirbel, Spritzer und Gaseintrag beim Tropfenaufprall. Seminar, Lehrstuhl für Strömungsmechanik, Universität Dortmund, 2008-05-28, Dortmund. Volltext nicht online. |
Rein, Martin (2009) Droplet impact: compressibility and wetting effects. Opening Symposium: Christian Doppler Laboratory for Cavitation and Microerosion, 19. Oktober - 19. Oktober 2009, Göttingen, Deutschland. Volltext nicht online. |
Rein, Martin (2010) Wind tunnel investigations of the effectiveness of leading-edge flow control devices on non-slender delta wings. Seminar, 24. March 2010, Bath, United Kingdom. Volltext nicht online. |
Rein, Martin (2011) Measurements of aerodynamic forces and moments on the DLR-F17E model in low- and high-speed flows. DLR-Interner Bericht. DLR-IB 224-2011 A 61. Deutsches Zentrum für Luft- und Raumfahrt. 52 S. Volltext nicht online. |
Rein, Martin (2013) Tests of the effectiveness of elevons and split flaps for the DLR-F17E model in high-speed flows. DLR-Interner Bericht. DLR-IB 917-2013 A 85. DLR. 48 S. Volltext nicht online. |
Rein, Martin (2013) On physical aspects of splashing. Mathematics of splashing, 28. - 30. Mai 2013, Edinburgh, Great Britain. Volltext nicht online. |
Rein, Martin and Delplanque, Jean-Pierre (2008) On the splashing threshold of droplets impinging on solid surfaces. 79th Annual Meeting of the International Association of Applied Mathematics and Mechanics, 2008-03-31 - 2008-04-04, Bremen. Volltext nicht online. |
Rein, Martin and Delplanque, Jean-Pierre (2008) The Role of Air Entrainment on the Outcome of Drop Impact on a Solid Surface. Acta Mechanica, 201, pp. 105-118. doi: 10.1007/s00707-008-0076-9. Volltext nicht online. |
Rein, Martin and Gardner, Anthony and Rütten, Markus (2012) Study of the influence of a highly integrated flow-through intake on compressible flows about the lambda wing configuration SACCON. 30th AIAA Applied Aerodynamics Conference, 25.-28. Juni 2012, New Orleans, USA. doi: 10.2514/6.2012-3324. Volltext nicht online. |
Rein, Martin and Höhler, Gebhard (2007) Vergleichende Untersuchungen zum Einfluss des Supports bei statischen Messungen an X-31 Modellen im DNW-NWB. DLR-Interner Bericht. IB 224 - 2007 A 35. 47 S. Volltext nicht online. |
Rein, Martin and Höhler, Gebhard (2011) Control of leading-edge vortices on non-slender delta wings. 82nd Annual Meeting of the International Association of Applied Mathematics and Mechanic, 18.-21. April 2011 , Graz, Österreich. Volltext nicht online. |
Rein, Martin and Höhler, Gebhard and Schütte, Andreas and Bergmann, Andreas and Löser, Thomas (2006) Ground-based simulation of complex maneuvers of a delta-wing aircraft. In: AIAA paper, AIAA Paper (2006-3149), 1--7. 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2006-06-05 - 2006-06-08, San Francisco. Volltext nicht online. |
Rein, Martin and Höhler, Gebhard and Schütte, Andreas and Bergmann, Andreas and Löser, Thomas (2006) Simulation of flight maneuvers in a wind-tunnel. 15. DGLR-Fach-Symposium der STAB, 2006-11-29 - 2006-12-01, Darmstadt. (Unpublished) Volltext nicht online. |
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. |
Rein, Martin and Klinkov, Konstantin (2007) On oscillating shock layers of supersonic impinging jets. In: 60th Annual Meeting of the Division of Fluid Dynamics. 60th Annual Meeting of the Division of Fluid Dynamics, [2007-11-18 - 2007-11-20], Salt Lake City (USA). (Unpublished) Volltext nicht online. |
Rein, Martin and Rosemann, Henning and Schülein, Erich (2007) Wave drag reduction by means of aerospikes on transonic wings. In: Shock Waves . 26th International Symposium on Shock Waves, 15. Juli - 20. Juli 2007, Göttingen, Deutschland. Volltext nicht online. |
Rein, Martin and Rosemann, Henning and Schülein, Erich (2005) Aerospikes on Transonic Wings. [Other] Volltext nicht online. |
Rein, Martin and Rosemann, Henning and Schülein, Erich (2006) Wave drag reduction by means of aerospikes on transonic wings. ISSW26, 2007-07-15 - 2007 - 07 - 20, Göttingen. Volltext nicht online. |
Rein, Martin (2016) Einführung in die Strömungsmechanik. [Other] Volltext nicht online. |
Rein, Martin (2016) Strömungen von Flüssigkeiten mit freien Oberflächen. [Other] Volltext nicht online. |
Rein, Martin (2016) Nonsteady Gasdynamics. [Other] Volltext nicht online. |
Rein, Martin (2016) Generic lambda wing configuration with classical and novel control surfaces and highly integrated intakes. [Other] Volltext nicht online. |
Rein, Martin (2016) Wind-tunnel tests of leading edge modifications for controlling delta wings. [Other] Volltext nicht online. |
Rein, Martin (2016) Generic lambda wing configuration with classical and novel control surfaces and highly integrated intakes. Seminar in Davis, USA, 28.11.2016, Davis, CA, USA. Volltext nicht online. |
Rein, Martin and Gardner, Anthony Donald (2015) Generic Lambda Wing Configuration in Compressible Flow: Effect of Highly Integrated Intakes. Journal of Aircraft, 52 (3), pp. 972-980. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C033177. ISSN 0021-8669. Volltext nicht online. |
Rein, Martin and Hannemann, Monika and Gardner, Anthony and Koch, Stefan (2009) Design of a generic subsonic S-duct intake for studies on the effect of boundary layer ingestion. DLR-Interner Bericht. DLR-IB 224-2009 A28. DLR, Institute of Aerodynamics and Flow Technology. 30 S. Volltext nicht online. |
Rein, Martin and Irving, Jonathan and Rigby, Glyn and Birch, Trevor J. (2014) High speed static experimental investigations to estimate control device effectiveness and S&C capabilities. American Institute of Aeronautics and Astronautics. AIAA Aviation and Aeronautics Forum and Exposition (AVIATION 2014), 16. – 20. June 2014, Atlanta, GA, USA. doi: 10.2514/6.2014-2004. Volltext nicht online. |
Rein, Martin and Koch, Stefan (2015) Experimental Study of Boundary-Layer Ingestion into a Diverterless S-Duct Intake. AIAA Journal, 53 (11), pp. 3487-3491. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J053902. ISSN 0001-1452. Volltext nicht online. |
Rein, Martin and Koch, Stefan and Rütten, Markus (2014) Experimental Investigations on the Influence of Ingesting Boundary Layers into a Diverterless S‐Duct Intake. 52nd Aerospace Sciences Meeting - AIAA SciTech, 13. - 17. Jan. 2014, National Harbor, Maryland, USA. doi: 10.2514/6.2014-0373. Volltext nicht online. |
Rein, Martin and Rosemann, Henning and Schülein, Erich (2009) Wave drag reduction by means of aerospikes on transonic wings. In: Shock Waves Springer Verlag, Berlin Heidelberg. pp. 1309-1313. doi: 10.1007/978-3-540-85181-3. ISBN 978-3-540-85180-6. Volltext nicht online. |
Reynier, Phillipe and Longo, Jose M.A. and Schülein, Erich (2006) Simulation of Missiles with Grid Fins Using an Actuator Disk. Journal of Spacecraft and Rockets, 43 (1), pp. 84-91. Volltext nicht online. |
Richard, Hughes and Geissler, Wolfgang and Raffel, Markus (2001) Simultaneous density and velocity measurement for rotorcraft research in a transonic wind tunnel. In: CD: 27th European Rotorcraft -Forum, 29.1-29.10. 27th European Rotorcraft -Forum, Moscow, September 2001., 2001-10-29, Moscow. Volltext nicht online. |
Richter, K. (2003) Vertraulich. DLR-Interner Bericht. 224 - 2003 C 01. 375 S. Volltext nicht online. |
Richter, Kai (2001) Einsatz von Mini-Klappen am Profil VC-Opt bei transsonischen Geschwindigkeiten. Aerodynamisches Seminar der RWTH Aachen, 2001-07-09, Aachen. Volltext nicht online. |
Richter, Kai (2002) Experimentelle und numerische Untersuchungen an transsonischen Flügelprofilen mit MiniTEDs. Aerodynamisches Seminar der RWTH Aachen, 2002-11-18, Aachen. Volltext nicht online. |
Richter, Kai (2005) Re-Effect on MiniTED Performance in High Speed: Validation and Prediction. AWIATOR Technical Workshop, 2005-11-05, Bremen. Volltext nicht online. |
Richter, Kai (2007) Confidential. DLR-Interner Bericht. DLR-IB 224-2007 C 06. 38 S. Volltext nicht online. |
Richter, Kai (2009) Untersuchungen zur Aerodynamik von Miniature Trailing-Edge Devices in transsonischen Strömungen. Dissertation, Rheinisch-Westfälischen Technischen Hochschule Aachen. Volltext nicht online. |
Richter, Kai (2010) Untersuchungen zur Aerodynamik von Miniature Trailing-Edge Devices in transsonischen Strömungen. DLR-Forschungsbericht. DLR-FB 2010-15. Dissertation. 194 S. Volltext nicht online. |
Richter, Kai (2009) Aerodynamische Aspekte von Hochgeschwindigkeitszügen. Promotionsvortrag RWTH Aachen, 12. Okt. 2009, Aachen. Volltext nicht online. |
Richter, Kai and Dargel, Georg and Koch, Stefan and Rosemann, Henning (2007) Confidential. DLR-Interner Bericht. DLR-IB 224-2007 C 17. 14 S. Volltext nicht online. |
Richter, Kai and Koch, Stefan and Gardner, Anthony Donald (2013) Influence of oscillation amplitude and Mach number on the unsteady transition on a pitching rotor blade airfoil. AHS 69th Annual Forum and Technology Display "Advancing Vertical Flight Technology in Demanding Environments", 21. - 23. May 2013, Phoenix, Arizona, USA. Volltext nicht online. |
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 Rosemann, Henning (2006) High-Reynolds-Number Design of a Wing Section Including Control of Boundary Layer Properties. Springer Berlin Heidelberg New York. 15. DGLR-Fach-Symposium der STAB, 2006-11-29 - 2006-12-01, Darmstadt. Volltext nicht online. |
Richter, Kai and Krause, Udo (2004) Confidential. DLR-Interner Bericht. 224 - 2004 C 20. 85 S. Volltext nicht online. |
Richter, Kai and Le Pape, Arnaud and Knopp, Tobias and Costes, Michel and Gleize, Vincent and Gardner, Anthony Donald (2009) Improved Two-Dimensional Dynamic Stall Prediction with Structured and Hybrid Numerical Methods. In: American Helicopter Society 65th Annual Forum Proceedings. American Helicopter Society 65th Annual Forum, 27.-29. Mai 2009, Grapevine, Texas (USA). Volltext nicht online. |
Richter, Kai and Pennecot, Julien (2005) Confidential. DLR-Interner Bericht. DLR-IB 224-2005 C 19. 144 S. Volltext nicht online. |
Richter, Kai and Rosemann, Henning (2002) Experimental investigation of trailing-edge devices at transonic speeds. The Aeronautical Journal, 106 (1058), pp. 185-193. Volltext nicht online. |
Richter, Kai and Rosemann, Henning (2006) Numerical Investigation on the Aerodynamic Effect of Mini-TEDs on the AWIATOR Aircraft at Cruise Conditions. 25th Congress on International Council of the Aeronautical Sciences (ICAS 2006), 2006-09-03 - 2006-09-08, Hamburg, Germany. Volltext nicht online. |
Richter, Kai and Rosemann, Henning (2011) Steady Aerodynamics of Miniature Trailing-Edge Devices in Transonic Flows. 29th AIAA Applied Aerodynamics Conference, 27. - 30. Juni 2011, Honolulu, Hawaii, USA. Volltext nicht online. |
Richter, Kai and Rosemann, Henning (2013) Numerical Simulation of Wind Tunnel Wall Effects on the Transonic Flow around an Airfoil Model. In: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 121. Springer Verlag, Heidelberg New York Dordrecht London. pp. 525-532. doi: 10.1007/978-3-642-35680-3_62. ISBN 978-3-642-35679-7. ISSN 1612-2909. Volltext nicht online. |
Richter, Kai and Rosemann, Henning (2012) Steady Aerodynamics of Miniature Trailing-Edge Devices in Transonic Flows. Journal of Aircraft, 49 (3), pp. 898-910. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.C031563. ISSN 0021-8669. Volltext nicht online. |
Richter, Kai (2005) Numerische Simulation eines Airbus A340 mit MiniTEDs im EU-Projekt AWIATOR. Aerodynamisches Seminar der RWTH Aachen, 2005-11-21, Aachen. Volltext nicht frei. | ![]() |
Richter, Kai (2016) STELAR - wissenschaftlicher Ergebnisbericht. DLR-Interner Bericht. DLR-IB-AS-GO-2016-356. Volltext nicht online. |
Richter, Kai and Gardner, Anthony Donald and Mai, Holger and Koch, Stefan (2015) Title confidential. DLR-Interner Bericht. IB 224-2015 C 171. 191 S. 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. American Helicopter Society. doi: 10.4050/JAHS.59.012001. ISSN 0002-8711. Volltext nicht online. |
Richter, Kai and Koch, Stefan and Goerttler, Andreas and Lütke, Benjamin and Wolf, Christian C. and Benkel, Andreas (2015) Unsteady Boundary Layer Transition on the DSA-9A Rotor Blade Airfoil. European Rotorcraft Forum 2015, 01. – 04. September 2015, Munich, Germany. Volltext nicht online. |
Richter, Kai and Schülein, Erich (2014) Boundary-layer transition measurements on hovering helicopter rotors by infrared thermography. Experiments in Fluids, 55 (7), pp. 1-13. Springer Nature. doi: 10.1007/s00348-014-1755-z. ISSN 0723-4864. Volltext nicht online. |
Richter, Kai and Schülein, Erich (2014) Boundary Layer Transition Measurements on Hovering Helicopter Rotors by Infrared Thermography. 70th Annual Forum of the American Helicopter Society, 20. - 22. Mai 2014, Montreal, Canada. Volltext nicht online. |
Richter, Kai and Schülein, Erich and Ewers, Benjamin and Raddatz, Jochen and Klein, Alexander (2016) Boundary Layer Transition Characteristics of a Full-Scale Helicopter Rotor in Hover. 72nd Annual Forum of the American Helicopter Society, 17.-19. May 2016, West Palm Beach, Florida, USA. Volltext nicht online. |
Richter, Kai and Wolf, C. Christian and Gardner, Anthony D. and Merz, Christoph B. (2016) Detection of Unsteady Boundary Layer Transition Using Three Experimental Methods. AIAA Science and Technology Forum and Exposition 2016, 04. - 08. Jan. 2016, San Diego, CA, USA. doi: 10.2514/6.2016-1072. Volltext nicht online. |
Ritz, Robert and Schomberg, Thomas and Wünsch, Olaf and Rütten, Markus and Kessler, Roland (2015) Numerical Investigation of the Detaching Vortical Flow at Rotating Cylinders with Thom Discs. AIAA-Aviation - 22nd AIAA Computational Fluid Dynamics Conference, 22. - 26. June 2015, Dallas, TX, USA. doi: 10.2514/6.2015-2289. ISBN 978-1-62410-355-1. Volltext nicht online. |
Rosemann, Henning (2007) Vertraulich. DLR-Interner Bericht. DLR-IB 2007 C 07. Volltext nicht online. |
Rosemann, Henning and Richter, Kai (2003) GURNEY FLAPS IN TRANSONIC FLOWS. In: IUTAM Symposium Transsonicium IV, 73, pp. 165-170. Kluwer Academic Publishers. Symposium Transsonicum IV, IUTAM International Union of Theoretical and Applied Mechanics, Göttingen, DLR, 2.-6. Sept. 2002, 2002-09-02, Göttingen. ISBN 1-4020-1608-5. Volltext nicht online. |
Rütten, Markus and Krenkel, Lars and Kessler, Roland (2012) Secondary Flow Effects as Physical Mechanism of Molecular Species Transport in Highly Oscillating Generic-Trachea Flows. 83rd Annual Scientific Conference of the International Association of Applied Mathematics and Mechanics, 26.-30. März 2012, Darmstadt, Germany. Volltext nicht online. |
Rütten, Markus and Saalfeld, Birgit and Künemund, Jens and Saalfeld, Stefan and Rein, Martin (2012) Numerical Flow Investigation of Morphing Leading Edges for the Enhancement of Maneuverability of Unmanned Combat Air Vehicles. AIAA Fluid Dynamics and Co-located Conferences and Exhibit, 25.-28. Juni 2012, New Orleans, Louisiana, USA. doi: 10.2514/6.2012-3326. Volltext nicht online. |
Rütten, Markus and Trenker, Markus and Rosemann, Henning (2012) Formation Flight Aerodynamics of Oblique Flying Wing Type Aircrafts. 6th European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2012), 10. - 14. Sept. 2012, Vienna, Austria. Volltext nicht online. |
Rütten, Markus (2016) Enhancement of Engine Onow Conditions Using Vortex Generators within Curved Intake Channels. AIAA SciTech 2016 - 54th AIAA Aerospace Sciences Meeting, 04. – 08. Jan. 2016, San Diego, California, USA. Volltext nicht online. |
Rütten, Markus (2016) Enhancement of Engine Onflow Conditions Using Vortex Generators within Curved Intake Channels. 54th AIAA Aerospace Sciences Meeting, AIAA SciTech Forum, 08. Jan. 2016, San Diego, CA, USA. doi: 10.2514/6.2016-1305. Volltext nicht online. |
Rütten, Markus and Dölle, Birgit and Künemund, Jens and Saalfeld, Stefan and Rein, Martin (2012) Numerical Flow Investigation of Morphing Leading Edges for the Enhancement of Maneuverability of Unmanned Combat Air Vehicles. 30th AIAA Applied Aerodynamics Conference, 25. - 28. Jun. 2012, New Orleans, Louisiana, USA. doi: 10.2514/6.2012-3326. Volltext nicht online. |
Rütten, Markus and Karl, Sebastian and Lindermeir, Erwin (2014) Numerical Investigation of Engine Exhaust Plume Characteristics of Unmanned Combat Air Vehicles. In: AIAA Aviation 2014, pp. 1-18. AIAA AVIATION Conference, 16.-20. Juni 2014, Atlanta, GA, USA. doi: 10.2514/6.2014-2838. Volltext nicht online. |
Rütten, Markus and Kuckenburg, Steffen and Koch, Stefan and Rein, Martin (2013) Investigation of the Flow within Partially Submerged Scoop Type Air Intakes. 31st AIAA Applied Aerodynamics Conference, 24. - 27. June 2013, San Diego, California, USA. doi: 10.2514/6.2013-2912. Volltext nicht online. |
Rütten, Markus and Wendland, Holger (2012) Performance Enhancement of Auxiliary Air Intakes by Using Vortex Generators. 50th AIAA Aerospace Science Meeting Fluid Dynamics Conference, 09. - 12. Jan. 2012, Nashville, Tennesee, USA. doi: 10.2514/6.2012-57. Volltext nicht frei. | ![]() |
Rütten, Markus and Woldegiorgis, Fithawi (2016) Vortical Flow Structure Genesis of Lobed Nozzle Flows. AIAA Conference 2016, 16.Juni 2016, Washington DC, USA. Volltext nicht online. |
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Saalfeld, Birgit and Rütten, Markus and Künemund, Jens and Saalfeld, Stefan (2012) Improved Mesh Morphing Based on Radial Basis Functions. 6th European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS 2012) , 10. - 14. Sept. 2012, Vienna, Austria. Volltext nicht online. |
Sandham, Neil and Schülein, Erich and Wagner, Alexander and Willems, Sebastian and Steelant, Johan (2014) Transitional shock-wave/boundary-layer interactions in hypersonic flow. Journal of Fluid Mechanics, 752 (6), pp. 349-382. Cambridge University Press. doi: 10.1017/jfm.2014.333. ISSN 0022-1120. Volltext nicht online. |
Schenk, Manuel (2015) Zur Vorderkante eines Überschalllufteinlaufs - Numerische Untersuchung des Einflusses der Vorderkantenausführung auf die Start-Machzahl eines generischen Überschalllufteinlaufs. Master's, TU Ilmenau. Volltext nicht online. |
Schenk, Manuel (2015) Numerische Untersuchung des Einflusses der Vorderkantenausführung auf die Start-Machzahl eines generischen Überschalllufteinlaufs. DLR-Interner Bericht. DLR-IB 224-2014 A 106. 115 S. Volltext nicht online. |
Schnepf, Christian and Wysocki, Oliver and Schülein, Erich (2013) Numerische Untersuchung zum Effekt einer leicht gebogenen Nase auf die Wirbelbildung an einem Flugkörper. 16. STAB-Workshop, Göttingen, Deutschland. Volltext nicht online. |
Schnepf, Christian (2012) Flow control on slender bodies at high angle of attack. 22nd Liepmann-Ludwieg Seminar, 16. - 21. Sept. 2012, Santa Barbara, USA. Volltext nicht online. |
Schnepf, Christian and Schülein, Erich (2009) Untersuchung eines innovativen Konzepts zur Reduzierung des Wellenwiderstands eines transsonischen Tragflügels. Deutscher Luft- und Raumfahrtkongress 2009, 2009-09-08 - 2009-09-10,, Aachen. Volltext nicht online. |
Schnepf, Christian and Schülein, Erich (2010) Numerische und experimentelle Untersuchung an einem Überschallflugkörper mit Nasenspike im Hochanstellwinkelbereich. 17. DGLR-Fach-Symposium der STAB, 09.-10. Nov. 2010, Berlin, Deutschland. Volltext nicht online. |
Schnepf, Christian and Schülein, Erich and Wysocki, Oliver (2012) Entstehung von Wirbelasymmetrien am Flugkörper durch Nasendeformation. 18. DGLR-Fach-Symposium der STAB, 06. - 07. Nov. 2012, Stuttgart, Deutschland. Volltext nicht online. |
Schnepf, Christian and Wysocki, Oliver and Schülein, Erich (2013) Wave drag reduction due to self aligning Aerodisk. 5th European Conference for Aeronautics and Space Sciences , 01. - 05. Juli 2013, Munich, Germany. Volltext nicht online. |
Schnepf, Christian and Wysocki, Oliver and Schülein, Erich (2013) Numerical investigation on the Phantom Yaw Effect induced due to small nose deflection. American Institute of Aeronautics and Astronautics. 31rd Applied Aerodynamics Conference, 24. - 27. Juni 2013, San Diego, USA. doi: 10.2514/6.2013-3034. Volltext nicht online. |
Schnepf, Christian and Schülein, Erich (2011) Nickmanöversimulation eines generischen Flugkörpers mit Hilfe der URANS-Gleichungen. STAB Workshop 2011, 10. - 11. Nov. 2011, Göttingen, Deutschland. Volltext nicht frei. | ![]() |
Schnepf, Christian (2016) CFD study on secondary injection thrust vectoring and side jet control. 20. DGLR STAB-Symposium 2016, 08. Nov. 2016, Braunschweig, Deutschland. Volltext nicht online. |
Schnepf, Christian and Schülein, Erich (2014) Numerische Studie zur Reduzierung des Phantom Yaw Effekts an manövrierenden Flugkörpern mittels Aerostrakes. 19. DGLR-Fachsymposium der STAB, 04. - 05. Nov. 2014, München, Deutschland. Volltext nicht online. |
Schnepf, Christian and Schülein, Erich (2016) CFD study on a missile in pitching motion with respect of reducing the Phantom Yaw Effect. In: New Results in Numerical and Experimental Fluid Mechanics X Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 132. Springer International Publishing Switzerland. pp. 833-842. doi: 10.1007/978-3-319-27279-5_73. ISBN 978-3-319-27278-8. ISSN 1612-2909. Volltext nicht online. |
Schnepf, Christian and Schülein, Erich (2015) Numerische Untersuchung zum Einsatz von Querschubstrahlen in Flugkörperschubdüsen zur Triebwerkstrahlbeeinflussung. STAB Workshop 2015, 10. - 11. Nov. 2015, Göttingen, Deutschland. Volltext nicht online. |
Schnepf, Christian and Wysocki, Oliver and Schülein, Erich (2015) Wave drag reduction due to a self aligning aerodisk. EUCASS Flight Physics, 7. Torus Press. doi: 10.1051/eucass/201507475. ISBN 978-5-94588-165-5. Volltext nicht online. |
Schnepf, Christian and Wysocki, Oliver and Schülein, Erich (2014) Numerical investigation on the development of the Phantom Yaw Effect on a maneuvering missile. American Institute of Aeronautics and Astronautics. AIAA Aviation and Aeronautics Forum and Exposition (AVIATION 2014), 16. – 20. June 2014, Atlanta, GA, USA. doi: 10.2514/6.2014-3097. Volltext nicht online. |
Schnepf, Christian and Wysocki, Oliver and Schülein, Erich (2015) Wave drag reduction with a self-aligning aerodisk on a missile configuration. 6th European Conference for Aeronautics and Space Sciences - EUCASS -, 29. Jun. - 03. Jul. 2015, Kraków, Poland. Volltext nicht online. |
Schojda, Lukas (2014) Shock Control Bump and Cruise Flap for a NLF Aerofoil. DLR-Interner Bericht. DLR-IB 224-2012 A 73. 39 S. Volltext nicht online. |
Schomberg, Thomas and Ritz, Robert and Wünsch, Olaf and Rütten, Markus and Kessler, Roland (2015) Flow Control of a Rotating Cylinder by the Use of a Structured Surface: A Visualization of Flow Structures. AIAA-Aviation - 22nd AIAA Computational Fluid Dynamics Conference, 22. - 26. June 2015, Dallas, TX, USA. doi: 10.2514/6.2015-2608. ISBN 978-1-62410-355-1. Volltext nicht online. |
Schwermer, Till and Richter, Kai and Raffel, Markus (2016) Development of a Rotor Test Facility for the Investigation of Dynamic Stall. In: New Results in Numerical and Experimental Fluid Mechanics X Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 132. Springer International Publishing Switzerland 2016. pp. 663-673. doi: 10.1007/978-3-319-27279-5_58. ISBN 978-3-319-27278-8. ISSN 1612-2909. Volltext nicht online. |
Schülein, Erich (2007) Wave Drag Reduction Concept for Blunt Bodies at High Angles of Attack. In: 26th International Simposium on Shock Waves, CD ROM Proceedings, pp. 1-6. ISSW 26, 2007-07-15 - 2007-07-20, Göttingen (Germany). Volltext nicht online. |
Schülein, Erich (2007) Experimental Investigation of Laminar Flow Control on a Supersonic Swept Wing by Suction. 4th AIAA Flow Control Conference, 2008-06-23 - 2008-06-26,, Seattle, Washington (USA). Volltext nicht online. |
Schülein, Erich (2007) Wave Drag Reduction Approach for Blunt Bodies at High Angles of Attack: Proof-of-Concept Experiments. 4th AIAA Flow Control Conference, 2008-06-23 - 2008-06-26,, Seattle, Washington (USA). Volltext nicht online. |
Schülein, Erich (2008) Wave Drag Reduction Approach for Blunt Bodies at High Angles of Attack. DLR-Interner Bericht. DLR-IB 224 - 2008 A 18. 19 S. Volltext nicht online. |
Schülein, Erich (2010) Shock-wave control by permeable wake generators. 5th AIAA Flow Control Conference, 28. Jun. - 01. Jul. 2010 , Chicago, Illinois, USA. ISBN 978-1-60086-745-3 . Volltext nicht online. |
Schülein, Erich (2011) Investigation of steady and pulsed energy addition into supersonic flow. 2011 Aerospace Thematic Workshop "Fundamentals of Aerodynamic Flow and Combustion Control by Plasmas", 27. Mar. - 01. Apr. 2011, Les Houches Physics School, France. Volltext nicht online. |
Schülein, Erich (2012) Method for Optical Skin Friction Measurements on Fast Rotating Propeller Blades. 18. DGLR-Fach-Symposium der STAB, 06. – 07. Nov. 2012, Stuttgart, Deutschland. Volltext nicht online. |
Schülein, Erich (2012) Optical Method for Skin Friction Measurements on Fast Rotating Propeller Blades. DLR-Interner Bericht. DLR-IB 224-2012 A 65. 19 S. Volltext nicht online. |
Schülein, Erich and Bornhöft, Erik (2011) Potential of localized flow heating for wave drag reduction. 28th International Symposium on Shock Waves (ISSW28), 17. - 22. July 2011, Manchester, UK. Volltext nicht online. |
Schülein, Erich and Bornhöft, Erik (2012) Potential of localized flow heating for wave drag reduction. In: 28th International Symposium on Shock Waves Shock Waves , 1. Springer Verlag, Heidelberg New York Dordrecht London. pp. 615-621. doi: 10.1007/978-3-642-25688-2_93. ISBN 978-3-642-25687-5. Volltext nicht online. |
Schülein, Erich and Guyot, Daniel (2006) Wave Drag Reduction Approach for Lattice Wings at High-Speeds. Springer-Verlag Berlin Heidelberg. 15. DGLR-Fach-Symposium der STAB, 2006-11-29 - 2006-12-01, Darmstadt. Volltext nicht online. |
Schülein, Erich and Rosemann, Henning (2012) Title confidential. DLR-Interner Bericht. DLR-IB 224-2012 C 117. 35 S. Volltext nicht online. |
Schülein, Erich and Rosemann, Henning and Schaber, Sven (2012) Transition Detection and Skin Friction Measurements on Rotating Propeller Blades. 28th AIAA Aerodynamic Measurement Technology, Ground Testing, and Flight Testing Conference, 25.-28. Jun. 2012, New Orleans, Louisiana, USA. Volltext nicht online. |
Schülein, Erich and Trofimov, Victor (2011) Steady longitudinal vortices in supersonic turbulent separated flows. Journal of Fluid Mechanics, Vol. 672, pp. 451-476. Cambridge University Press. doi: 10.1017/S0022112010006105. Volltext nicht online. |
Schülein, Erich and Wagner, Alexander (2012) Ludwieg-Tube Experiments on the Effects of Laminar-Turbulent Transition on the SWBLI at Mach 6. DLR-Interner Bericht. DLR-IB 224-2011 A 64. 72 S. Volltext nicht online. |
Schülein, Erich and Zheltovodov, Alexander (2011) Effects of steady flow heating by arc discharge upstream of non-slender bodies. Shock Waves, Vol. 21 (4), pp. 383-396. Springer. doi: 10.1007/s00193-011-0307-1. ISSN 0938-1287. Volltext nicht online. |
Schülein, Erich and Zheltovodov, Alexander A. (2009) Effects of Localized Flow Heating by DC-Arc Discharge Ahead of Non-Slender Bodies. In: AIAA (AIAA-2009-7346), pp. 1-16. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 19.-22. Oct. 2009, Bremen (Germany). Volltext nicht online. |
Schülein, Erich and Zheltovodov, Alexander A. and Pimonov, E. A. and Loginiv, M.S. (2007) Experimental and Numerical Investigation of Electric-Arc Airspikes for Blunt and Sharp Bodies at Mach 5. ICMAR 2008 (14th International Conference on Methods of Aerophysical Research), 2008-06-30 - 2008-07-06,, Novosibirsk (Russia). Volltext nicht online. |
Schülein, Erich and Zheltovodov, Alexander A. and Pimonov, Evgeny A. and Loginov, Maxim S. (2010) Experimental and Numerical Modeling of the Bow Shock Interaction with Pulse-Heated Air Bubbles. International Journal of Aerospace Innovations, Vol. 2 (3), pp. 165-188. Sage Publications. doi: 10.1260/1757-2258.2.3.165. ISSN 1757-2258. Volltext nicht online. |
Schülein, Erich (2005) Experimental Investigation of Boundary Layer Transition on a Supersonic Swept Wing. DLR-Interner Bericht. DLR-IB 224 - 2005 A 15. 25 S. Volltext nicht online. |
Schülein, Erich (2006) Skin Friction and Heat Flux Measurements in Shock Boundary Layer Interaction Flows. AIAA Journal, 44 (8), pp. 1732-1741. Volltext nicht online. |
Schülein, Erich (2002) Development and Application of the Thin Oil Film Technique for Skin Friction Measurements in the Ludwieg-Tube at DLR. 97th Meeting of the Supersonic Tunnel Association International, 2002-04-14 - 2002-04-16, University of Notre Dame, Notre Dame, Indiana (USA). Volltext nicht online. |
Schülein, Erich (2003) Aerodynamisches Auslegungs- und Optimierungstool für isolierte Gitterflügel "FastGRIDS". 11.STAB-Workshop, 2003.11.04 - 2003.11.05, DLR Göttingen. Volltext nicht online. |
Schülein, Erich (2006) Neue Konzepte zur Widerstandsreduzierung im Überschall. In: Wirkung und Schutz, Explosivstoffe. Bundesakademie für Wehrverwaltung und Wehrtechnik. Wehrtechnisches Symposium 2006, 2006-11-13 - 2006-11-15, Mannheim. Volltext nicht online. |
Schülein, Erich (2007) Confidential. DLR-Interner Bericht. DLR-IB 224-2007C15. 54 S. Volltext nicht online. |
Schülein, Erich (2007) Untersuchungen zur Reduzierung des Bugwiderstands von hochagilen Flugkörpern im Rahmen des DLR-Projekts FFT. 13.STAB-Workshop, 2007-11-14 - 2007-11-15, Göttingen (Germany). Volltext nicht online. |
Schülein, Erich (2008) Untersuchungen zur Steigerung der aerodynamischen Leistungsfähigkeit von Flugkörpern. In: Wirkung und Schutz, Explosivstoffe. Bundesakademie für Wehrverwaltung und Wehrtechnik. Wehrtechnisches Symposium 2008, 2008-11-10 - 2008-11-12, Mannheim. Volltext nicht online. |
Schülein, Erich and Guyot, Daniel (2006) Experimentelle und numerische Untersuchungen zu Zahngitterflügeln. Sitzung der Kommission des Wiss.Beirats SP-Aufgabe 2.14 Steuerung von Geschossen, 2006-01-31 - 2006-02-01, Saint-Louis (Frankreich). Volltext nicht online. |
Schülein, Erich and Guyot, Daniel (2006) Novel High-Performance Grid Fins for Missile Control at High Speeds: Preliminary Numerical and Experimental Investigations. In: Innovative Missile Systems, 35-1-35-26. NATO RTA. Meeting Proceedings RTO-MP-AVT-135, 2006-05-15 - 2006-05-19, Amsterdam, The Netherlands. Volltext nicht online. |
Schülein, Erich and Henckels, Andreas and Kovar, Anke and Psolla-Bress, Hartmut and Reynier, Phillipe (2003) Aktueller Stand der Untersuchungen zur Steuerung mit Gitterflügeln. Volltext nicht online. |
Schülein, Erich and Henckels, Andreas and Psolla-Bress, Hartmut (2004) Instationäre Strömungsvorgänge an Gitterflügeln. Wehrtechnisches Symposium „Explosivstoffe, Wirkung und Schutz“, 2004-11-08 - 2004-11-10, BAKWVT, Mannheim. Volltext nicht online. |
Schülein, Erich and Krogmann, Paul and Stanewsky, Egon (1996) Documentation of two-dimensional impinging shock/turbulent boundary layer interaction flow. DLR-Interner Bericht. DLR-IB 223 - 96 A 49. 69 S. Volltext nicht online. |
Schülein, Erich and Rosemann, Henning (2013) Title confidential. DLR-Interner Bericht. DLR-IB 224-2012 C 127. 33 S. Volltext nicht online. |
Schülein, Erich and Rosemann, Henning (2013) Title confidential. DLR-Interner Bericht. DLR-IB 224-2013 C 161. 21 S. Volltext nicht online. |
Schülein, Erich and Tomek, Dominik and Schnepf, Christian (2013) Stoß- und Transitionsbedingte Lasten an Flugkörperkomponenten. 16. STAB-Workshop, 12. – 13. Nov. 2013, Göttingen, Deutschland. Volltext nicht online. |
Schülein, Erich and Trofimov, Victor (2005) Experimental Investigation of Longitudinal Vortices in Separated Turbulent Flows. 12. STAB-Workshop, 2005-11-08 - 2005-11-09, DLR Göttingen. Volltext nicht online. |
Schülein, Erich and Trofimov, Victor (2004) Modelling of Streamwise Structures in Experiments on Compression Corners in a Turbulent Boundary Layer: Natural Scale. 12th INTERNATIONAL CONFERENCE ON METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2004), 2004-06-28 - 2004-07-04, Akademgorodok, Novosibirsk (Russia). Volltext nicht online. |
Schülein, Erich and Trofimov, Victor (2006) Longitudinal vortices in separated turbulent flows. DLR-Interner Bericht. DLR-IB 224-2005A17. 57 S. Volltext nicht online. |
Schülein, Erich and Trofimov, Victor (2007) Steady Longitudinal Vortices in Separated Turbulent Flows. DGLR. 1st CEAS European Air & Space Congress, 2007-09-10 - 2007-09-13, Berlin, Germany. ISSN 0700-4083. Volltext nicht online. |
Schülein, Erich and Zheltovodov, Alexander A. and Loginov, M. S. and Pimonov, E. A. (2008) Experimental and Numerical Study of Shock Wave Transformation by Laser-Induced Energy Deposition. ICMAR 2008 (14th International Conference on Methods of Aerophysical Research), 2008-06-30 - 2008-07-06,, Novosibirsk (Russia). Volltext nicht online. |
Schülein, Erich (2014) Optical method for skin-friction measurements on fast-rotating blades. Experiments in Fluids, 55 (1672), pp. 1-10. Springer Nature. doi: 10.1007/s00348-014-1672-1. ISSN 0723-4864. Volltext nicht online. |
Schülein, Erich (2014) Effects of Laminar-Turbulent Transition on the Shock-Wave/Boundary-Layer Interaction. AIAA Aviation and Aeronautics Forum and Exposition (AVIATION 2014), 16. - 20. June 2014, Atlanta, Georgia, USA. doi: 10.2514/6.2014-3332. Volltext nicht online. |
Schülein, Erich (2014) Simplified Model for Flow-heating Effect on Wave-drag Reduction of Blunt Bodies. 19. DGLR-Fachsymposium der STAB, 04. – 05. Nov. 2014, München, Deutschland. Volltext nicht online. |
Schülein, Erich (2015) Simplified model for flow-heating effect on wave drag of blunt bodies and its validation. AIAA AVIATION 2015, 22. – 26. June 2015, Dallas, Texas, USA. doi: 10.2514/6.2015-2778. Volltext nicht online. |
Schülein, Erich (2009) Wave drag reduction concept for blunt bodies at high angles of attack. In: Shock Waves Springer Verlag, Berlin Heidelberg. pp. 1315-1320. doi: 10.1007/978-3-540-85181-3. ISBN 978-3-540-85180-6. Volltext nicht online. |
Schülein, Erich (2016) Simplified model for flow-heating effect on wave drag and its validation. AIAA Journal, 54 (3), pp. 1030-1039. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J054604. ISSN 0001-1452. | ![]() |
Schülein, Erich and Schenk, M. and Buchmann, B. (2015) Studie zur Start-Machzahl eines generischen Überschalllufteinlaufs. 17. STAB-Workshop, 10.-11. November 2015, Göttingen, Deutschland. Volltext nicht online. |
Schülein, Erich and Wagner, Alexander (2015) Title confidential. DLR-Interner Bericht. DLR-IB 224-2015 C 169. 59 S. Volltext nicht online. |
Schülein, Erich and Zheltovodov, Alexander A. and Pimonov, E. A. and Loginov, M. S. (2009) Study of the Bow Shock Interaction with Laser-Pulse-Heated Air Bubbles. 39th AIAA Fluid Dynamics Conference and Exhibit, 2009-06-22 - 2009-06-25,, San Antonio (TX), USA. Volltext nicht frei. | ![]() |
Schütte, Andreas and Huber, Kerstin Claudie and Liersch, Carsten M. 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. DLR. 190 S. Volltext nicht online. |
Schütte, Andreas and Rein, Martin and Höhler, Gebhard (2009) Experimental and numerical aspects of simulating unsteady flows around the X-31 configuration. Proceedings of the Institution of Mechanical Engineers Part G-Journal of Aerospace Engineering, 223 (4), pp. 309-321. SAGE Publications. doi: 10.1243/09544100JAERO387. ISSN 0954-4100. Volltext nicht online. |
Siegel, Lars (2013) Experimentelle Analyse der Strömung am schwach gepfeilten Deltaflügel mit unterschiedlichen Vorderkantengeometrien unter dem Gesichtspunkt der Strömungssteuerung. DLR-Interner Bericht. DLR-IB 224-2013 A 79. Master's. Universität Göttingen. 75 S. Volltext nicht online. |
Sobieczky, Helmut (2005) Flow Boundary Conditions Modeling in 4D for Optimized, Adaptive and Unsteady Configurations. In: Frontiers of Computational Fluid Dynamics 2006 World Scientific, Singapore. pp. 97-104. ISBN 981-256-527-2. Volltext nicht online. |
Sobieczky, Helmut (2005) Educational Value of Analyticaly Described Flow Fields. In: AIAA 4th Theoretical Fluid Mechanics Conference (AIAA-2005-4806), p. 8. AIAA 4th Theoretical Fluid Mechanics Conference, 2005-06-06, Toronto, Canada. Volltext nicht online. |
Sorokin, A.M. and Boiko, A.V and Dovgal, A.V. and Gorev, V.N. and Hein, Stefan and Wilke, Bastian (2010) Application of particle image velocimetry for velocity measurements in subsonic near-wall shear flows. International Conference on the Methods of Aerophysical Research – ICMAR 2010, 01. - 06. Nov. 2010, Novosibirsk, Russia. ISBN 978-5-98901-085-1. Volltext nicht online. |
Stanewsky, Egon and Schülein, Erich (1995) Review of available validation experiments // Critical review of prediction methods for compressible turbulent attached and separated flows (edited by I.Lindblad). Other. FFA TN 1995-43. FFA TN 1995-43. 20 S. Volltext nicht online. |
Stapel, Waldemar (2013) Aerodynamic shape optimisation of a displacement body with a discrete adjoint method. Diploma, Universität Kassel. Volltext nicht online. |
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