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

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Number of items at this level: 420.

B

  Banuti, Daniel (2007) Entwurf von Vorköpermodifikationen und Einfluß auf das Drucknahfeld eines Hyperschalltransportflugzeuges. 13. STAB-Workshop, 2007-11-14 - 2007-11-15, Göttingen. (Unpublished) Volltext nicht online.

  Banuti, Daniel (2008) Interfacial Area Modeling for Eulerian Spray Simulations in Liquid Rocket Engines. In: 2008 AIAA Conference Proceedings. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2008-07-21 - 2008-07-23, Hartfort, Connecticut, USA. Volltext nicht online.

  Banuti, Daniel (2012) High Pressure Propellant Injection in Liquid Rocket Engines. 22nd Liepmann Ludwieg Seminar, 16. - 21. Sept. 2012, Santa Barbara, USA. Volltext nicht online.

  Banuti, Daniel and Hannemann, Klaus (2010) Flow control by energy deposition in hypersonic flow - some fundamental considerations. Conference Proceedings. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 19. - 22. Oct. 2009, Bremen, Germany. ISBN 978-1-60086-740-8. Volltext nicht online.

  Banuti, Daniel and Hannemann, Klaus (2010) Interfacial Area Transport Equation in Statistical-Eulerian-Eulerian Simulations of Multiphase Flow. In: New Results in Numerical and Experimental Fluid Mechanics VII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 112. Springer-Verlag, Berlin Heidelberg. pp. 1-8. ISBN 978-3-642-14242-0. ISSN 1612-2909 Volltext nicht online.

  Banuti, Daniel and Hannemann, Klaus and Knab, Oliver (2008) Interfacial Area Transport Equation in Statistical-Eulerian-Eulerian Simulations of Multiphase Flow. 16. DGLR/STAB Symposium, 2008-11-3 - 2008-11-04, Aachen. (Submitted) Volltext nicht online.

  Banuti, Daniel and Hannemann, Klaus and Longo, Jose (2010) Aspects of thermal flow control in hypersonic flight. CEAS Air and Space Conference, 26. - 29. Oct. 2009, Manchester, Great Britain. ISBN 1 85768 213 8. Volltext nicht online.

  Banuti, Daniel and Grabe, Martin and Hannemann, Klaus (2011) Steady Shock Refraction in Hypersonic Ramp Flow. Conference Proceedings online. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 11. - 14. Apr. 2011, San Francisco, USA. file

  Banuti, Daniel and Hannemann, Klaus (2010) Effect of Injector Wall Heat Flux on Cryogenic Injection. 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 25 - 28 Jul 2010, Nashville, USA. ISBN 978-1-60086-747-7. file

  Banuti, Daniel and Hannemann, Klaus (2011) Thermodynamic Interpretation of Cryogenic Injection Experiments. 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 21.-23. Jul. 2011, San Diego, USA. file

  Banuti, Daniel and Hannemann, Klaus (2013) Real Gas Library in Continuous Phase Propellant Injection Model for Liquid Rocket Engines. 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 14. - 17. July 2013, San Jose, CA, USA. Volltext nicht online.

  Barth, Tarik (2006) Auslegung und numerische Simulation von strömungs- und thermodynamischen Aspekten einer Untersuchungsanlage zur Gasbeschleunigung mittels des Magnet-Gas-Dynamik-Effektes. Master's. Volltext nicht online.

  Barth, Tarik (2010) Aerothermodynamische Untersuchung facettierter Raumfahrzeuge unter Wiedereintrittsbedingungen. Dissertation, Universität Stuttgart. file

  Barth, Tarik and Eggers, Thino and Dittrich, Robert and Otto, Hannes (2011) Analysis of the Hypersonic Flow Field around the Skylon Vehicle. DLR-Interner Bericht. DLR-IB 124-2011/907, 71 S. Volltext nicht frei. file

  Barth, Tarik and Gehre, Rolf and Eggers, Thino and Schramm, M. and Wagner, Alexander and Hannemann, Klaus and Kaufmann, Rene and Böhrk, Hannah (2013) Experimental and Numerical Analysis of SHEFEX-II. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics VIII, Vol. 121. Springer Verlag. pp. 75-83. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht online.

  Barth, Tarik (2009) Aerothermodynamische Voruntersuchung der REX - Free Flyer Konfiguration. DLR-Interner Bericht. (Unpublished) Volltext nicht frei. file

  Barth, Tarik and Dankert, Carl and Roden, Günter von and Martinez Schramm, Jan (2010) Investigations to the Response Time of a Glued Thermocouple on the Basis of Experimental and Numerical Analyses. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 1. Springer Verlag, Berlin Heidelberg. pp. 355-363. ISBN 978-3-642-14242-0. ISSN 1612-2909 Volltext nicht frei. file

  Barth, Tarik and Longo, Jose (2010) Advanced Flight Analysis of SHEFEX-I. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 1. Springer Verlag, Berlin Heidelberg. pp. 431-439. ISBN 978-3-642-14242-0. ISSN 1612-2909 Volltext nicht frei. file

  Barth, Tarik and Longo, Jose (2010) Advanced Aerothermodynamic Analysis of SHEFEX I. Aerospace Science and Technology, 14 (8), pp. 587-593. DOI: 10.1016/j.ast.2010.05.005. ISSN 1270-9638. file

  Bartolome Calvo, Javier and Eggers, Thino (2011) Numerical Flight Mechanics Analysis of the SHEFEX I Ascent and Re-entry Phases. European Space Agency. 7th European Symposium on Aerothermodynamics, 9-12 May 2011, Brugge, Belgium. ISBN 978-92-9221-256-8. ISSN 1609-042X Volltext nicht frei. file

  Bartolome Calvo, Javier and Eggers, Thino (2011) Application of a Coupling of Aerodynamics and Flight Dynamics to the SHEFEX I Flight Experiment. In: AIAA-2011-2323 . 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 11-14 April 2011, San Francisco, United States of America. Volltext nicht online.

  Bartolome Calvo, Javier and Eggers, Thino (2011) Numerical Study of the SHEFEX I Flight. Volltext nicht frei. file

  Bartolome Calvo, Javier and Esser, Burkard and Gülhan, Ali and Haupt, Matthias and Kowollik, Daniel and Mischke, Robert (2011) Numerical Analysis of Heat Transfer to Supercritical Water for Liquid Rocket Engine Cooling Experiments. 15. STAB Workshop, 9-10 Nov 2011, Göttingen, Germany. Volltext nicht online.

  Bartolome Calvo, Javier and Hannemann, Klaus (2008) Analysis of Heat Transfer in Liquid Rocket Engine Cooling Channels. Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Volltext nicht online.

  Bartolome Calvo, Javier and Hannemann, Klaus (2008) Numerical Simulation of Liquid Rocket Engine Cooling Channels. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Denver, USA. Volltext nicht online.

  Bartolome Calvo, Javier and Hannemann, Klaus (2010) On the Modelling of the Flow and Heat Transfer in Cooling Channels. Volltext nicht frei. file

  Bartolome Calvo, Javier and Lüdeke, Heinrich (2007) Multidisciplinary Simulation of the Ariane-5 Nozzle Section. In: First CEAS Conference. Fisrt CEAS Conference, 2007-09-04, Berlin. Volltext nicht online.

  Bartolome Calvo, Javier and Mack, Andreas (2006) Study of Hypersonic Heating. Aerospace Science and Technology. (Submitted) Volltext nicht online.

  Bartolome Calvo, Javier and Mack, Andreas (2008) A Study of the Heating of a Hypersonic Vehicle Launched by a Lorentz Rail Accelerator. International Review of Aerospace Engineering, 1 (3), pp. 269-276. Praise Worthy Prize S.r.l.. ISSN 1973-7459. Volltext nicht online.

  Bartolome Calvo, Javier (2010) Numerical Simulation of Liquid Rocket Engine Cooling Channels. Dissertation, Universitat Politecnica de Catalunya. Volltext nicht frei. file

  Bauer, Maria and Birken, Philipp and Hannemann, Volker and Oßwald, Kai (2011) Accuracy in a Finite Volume Godunov Type Method. 17. DGLR-Fach-Symposium der STAB, 09. - 10. Nov. 2010, Berlin, Deutschland. Volltext nicht online.

  Beck, Walter and Fey, Uwe and Henne, Ulrich and Klein, Christian and Sachs, Werner and Jünemann, Mario and Laurence, Stuart and Martinez Schramm, Jan and Schwendtke, Ingo and Wagner, Alexander (2011) Pressure and temperature measurements on an inclined ramp in HEG using PSP and TSP. MOTAR-Workshop 2011, 30.-31. March 2011, Lampoldshausen, Germany. Volltext nicht online.

  Beck, Walter and Fey, Uwe and Henne, Ulrich and Sachs, Werner and Jünemann, Mario and Laurence, Stuart and Martinez Schramm, Jan and Schwendtke, Ingo and Wagner, Alexander (2012) PSP Measurements on a Ramp in the High Enthalpy Shock Tunnel HEG. Deutsch/Japanischer Workshop "Leuchten in der Aerodynamik", 03. - 05. Sept. 2012, Chofu (Tokio), Japan. Volltext nicht online.

  Beck, Walter and Hannemann, Klaus and Weiland, Matthias (2001) Modifications to the DLR High Enthalpy Shock Tunnel HEG for Measurements on Supersonic Combustion. American Institute of Aeronautics & Astronautics. 10th International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan, 24. - 27. Apr. 2001. DOI: 10.2514/6.2001-1860. Volltext nicht online.

  Beck, Walter and Klein, Christian and Henne, Ulrich and Sachs, Werner and Fey, Uwe and Jünemann, Mario and Martinez Schramm, Jan and Schwendtke, Ingo and Laurence, Stuart and Wagner, Alexander (2011) Unsteady PSP: III. PSP and TSP Measurements on a Ramp in the High Enthalpy Shock Tunnel HEG. Seminar National Aerospace Laboratories (NAL), Indian, 15. Dec. 2011, Bangalore, Indien. Volltext nicht online.

  Beck, Walter and Klein, Christian and Henne, Ulrich and Sachs, Werner and Fey, Uwe and Jünemann, Mario and Martinez-Schramm, Jan and Schwendtke, Ingo and Laurence, Stuart and Wagner, Alexander (2013) Unsteady PSP: II. PSP and TSP Measurements on a Ramp in the High Enthalpy Shock Tunnel HEG. Seminar China Academy of Aerospace Aerodynamics (CAAA), 13. Aug. 2013, Beijing, P.R. China. Volltext nicht online.

  Beck, Walter and Klein, Christian and Martinez Schramm, Jan (2013) TSP Measurements on a Ramp in HEG at Low Enthalpy. MOTAR - Measurement and Optical Techniques for Aerospace Research, 10. - 11. Apr. 2013, Lampoldshausen, Germany. Volltext nicht online.

  Beck, Walter and Klein, Christian and Wagner, Alexander and Martinez Schramm, Jan (2013) TSP Measurements on a Ramp in HEG at Low Enthalpy. 4th German-Japanese Seminar, Munich, Germany, 23. - 25. Sept. 2013. Volltext nicht online.

  Belmont, J.P. and Starke, J. and Longo, J. and Novelli, Ph. and Kordulla, W. (2008) Reflections on Conditions for Commericail Air-launched Suborbital Flight in Europe - Selected Results of a Study Funded by the European Community (EC). 1st Symposium on Private Human Access to Space, 2008-05, Arcachon (France). file

  Birkenkampf, Peter (2011) Systemtest der Implementierung einer domänenspezifischen Sprache zur Messdatenauswertung. Bachelor's, Duale Hochschule Baden-Württemberg. Volltext nicht frei. file

  Bode, Christoph and Eggers, Thino and Smart, M. (2013) Numerical Generation of a Flush Air Data System for the Hypersonic Flight Experiment HIFiRE 7. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics VIII, Vol. 121. Springer Verlag. pp. 101-108. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht frei. file

  Boehrk, Hannah and Wartemann, Viola and Martinez Schramm, Jan and Wagner, Alexander and Hannemann, Klaus and Eggers, Thino (2012) Shock Tunnel Testing of the Transpiration-Cooled Heat Shield Experiment AKTiV. 18th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 24. - 28. Sept. 2012, Tours, France. DOI: 10.2514/6.2012-5935. Volltext nicht online.

  Boettcher, Rolf-Detlef and Dettleff, Georg (2007) Design Issues of Spacecraft Constellation: Mutual Interaction Final Report. DLR-Interner Bericht. DLR-IB 224-2006 C 41, 132 S. Volltext nicht online.

  Boyce, Russell and Martinez Schramm, Jan and Oberg, Daniel and Hannemann, Klaus and Brown, Laurie (2012) Shock tunnel and numerical studies of a large inlet-fuelled inward turning axisymmetric scramjet. 18th AIAA International Space Planes and Hypersonic Systems and Technologies Conference , 24. - 28. Sept. 2012, Tours, France. DOI: 10.2514/6.2012-5901. Volltext nicht online.

  Bozic, O. and Lancelle, D. and May, S. and Porrmann, D. (2013) Experimental Evaluation of a High Test Peroxide Catalyst Chamber for a Hybrid Rocket Engine. EUCASS, 1.-5. Juli 2013, München, Deutschland. Volltext nicht frei. file

  Bozic, O. and Porrmann, D. and Lancelle, D. and Hartwig, A. (2012) Program AHRES and its Contribution to Assess Features and Current Limitations of Hybrid Rocket Propulsion. IAC-12-C4.2.8 , 1.-5. October 2012, Naples, Italy. Volltext nicht frei. file

  Bozic, O. and Schneider , M. and Porrmann, D. (2010) Conceptual Design of "SILVER EAGLE" - Combined Electromagnetic and Hybrid Rocket System for Suborbital Investigations. In: CD ROM IAF: Paper IAC-10-C4.6.1. 61st International Astronautical Congress (IAC), C4.6. Special Session on "Missions Enabled by New Propulsion Technologies and, 27th September – 1st October 2010, Prague, Czech Republic . Volltext nicht frei. filefile

  Bozic, Ognjan and Longo, Jose M. A. (2007) Moon 2016 - Technology Platform for Extraterrestrial Investigations. In: Proceeding CD (02). machtwissen.de AG. DGLR International Symposium “To Moon and beyond”, 2007-03-14 - 2006-03-16, Bremen, Germany. ISSN 978-3-932182-52-9 Volltext nicht online.

  Bozic, Ognjan and Longo, Jose M. A. (2007) Moon Sample Return Mission 2016. 58th International Astronautical Congress - A3. Space Exploration Symposium - Session A3.6: Moon Exploration, 2007-09-24 - 2007-09-28, Hyderabad, India. (Submitted) Volltext nicht online.

  Bozic, Ognjan and Longo, José M.A. and Giese, Peter and Behrens, Jörg (2004) High-End Concept to Launch Micro-Satellites into Low-Earth-Orbit based on Combination of a Two-Stage Rocket and a Railgun System. Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer Verlag. (In Press) Volltext nicht online.

  Bozic, Ognjan and Behrens, Jorg (2006) Railgun assisted Launches of Projectiles with Sub- and Low - Earth - Orbit – Payloads (The European View). ESA Student Technical Education Conference, STEC 2006, 2006-05-09 - 2006-05-12, Braunschweig, Niedersachsen, Germany. Volltext nicht frei. file

  Bozic, Ognjan and Behrens, Jörg (2004) Per Schienenkanone ins All (Teil I): Einsatz einer "Electromagnetic Railgun" für suborbitale Höhenforschung. Raumfahrt Concret, 4-5 (34-35). file

  Bozic, Ognjan and Behrens, Jörg (2005) Per Schienenkanone ins All (Teil 2): Blitzschnell und günstig in den Orbit. Raumfahrt Concret, 2 (37). file

  Bozic, Ognjan and Giese, Peter (2006) Aerothermodynamic Aspects of Railgun assisted Launches of Projectiles with Sub- and Low – Earth -Orbit – Payloads. IEEE Transactions of Magnetics, 43 (1), pp. 474-479. IEEE Magnetics Society. Volltext nicht frei. file

  Bozic, Ognjan and Longo, Jose M. A. (2007) Technology driven Robotic-Moon-Mission 2016. In: 7th International Symposium on Launcher Technologies - Proceeding CD. 7th International Symposium on Launcher Technologies - Opening New Ways to Space Prospective, 2007-04-02 - 2007-04-05, Barcelona, Spain. (In Press) file

  Bozic, Ognjan and Longo, Jose M. A. and Otto, Hannes (2006) Shock-Wave-Boundary-Layer Interaction (SWBLI) around open Flaps of EXPERT Capsule and their Consideration on Heat and Mechanical Loads under critical Re-Entry Flow Conditions. 57th International Astronautical Congress - Space Transportation Symposium (D2 - 5.), [2006-10-02 - 2006-10-06], Valencia, Spain. file

  Božić, Ognjan and Porrmann, Dennis (2009) Estimation of Flow Field Properties and Thrust Performances of Axisymmetric Plug - Nozzles using CFD Simulations. In: Turbulence, Heat and Mass Transfer 6, 6, pp. 599-602. Begell House, Inc , New York, Wallingford (UK). 6th International Symposium on Turbulence, Heat and Mass Transfer (THMT´09), 14-18 Sept. 2009, Rom, Italy. ISBN 978-1-56700-262-1. Volltext nicht frei. file

  Božić , Dr. Ognjan and Leithner, Dr. Reinhard (2009) Mineralumwandlung (Kapitel 5),. In: Simulation von Kraftwerken und Wärmetechnischen Anlagen Springer-Verlag/ Wien. pp. 369-406. ISBN 978-3-211-29695-0 Springer Wien - New York. Volltext nicht frei. file

  Božić, Dr. Ognjan (2008) Possibilities of Lorentz Electromagnetic Accelerators for Launch of Payloads in Low-Earth-Orbit. 59. International Astronautical Congress, 29 Sept. – 3 Okt. 2008, Glasgow, Scotland, GB. Volltext nicht frei. file

  Božić, Ognjan and Eggers, Thino and Wiggen, Stefan (2009) Aerothermal and Flight Mechanic Considerations by Development of Small Launchers for Low Orbit Payloads Started from Lorentz Rail Accelerator. 3rd European Conference for Aero-Space Sciences - EUCASS, 6.-9. Juli 2009, Versailles-Paris, France. Volltext nicht frei. file

  Brandes, Julia (2010) Herleitung und Analyse eines Finite-Volumen-Verfahrens für reibungsfreie Strömungen. Bachelor's, Universität Kassel. Volltext nicht online.

  Buanga, Björn and Hannemann, Volker and Lüdeke, Heinrich and You, Yancheng (2009) Modeling of the interaction between a space vehicle’s external flow and it’s plume. In: Deutsche Forschungsgemeinschaft (DFG). file

  Buffetti, Barbara (2014) Title confidential. Project Report. DLR-IB 124-2014/901, 19 S. Volltext nicht online.

  Böhrk, Hannah and Barth, Tarik and Dietlein, Ingrid and Elsäßer, Henning and Eggers, Thino and Eßmann, Olaf and Koch , Aaron and Kopp, Alexander and Reimer, Thomas and Sippel, Martin and Weihs, Hendrik (2010) REX-Free Flyer: Re-Entry to Earth Experiment - Machbarkeitsstudie. DLR-Interner Bericht. DLR-IB 435-2010/35, 15 S. Volltext nicht online.

  Bérend, Nicolas and Calabro, Max and Božić, Dr. Ognjan and Bonnal, Cristophe and Matloff, Dr. Gregory. L. and Valentian, Dominique (2009) Non-chemical, non-nuclear advanced propulsion for space applications: Panorama and Roadmap. 60th International Astronautical Congress, 12.-16. Okt. 2009, Daejon, Korea. Volltext nicht frei. file

  Böttcher, Carmen (2009) A Numerical Study of Magnetohydrodynamic Flows with Respect to the Hall Effect. 16th AIAA/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 2009-10-19 - 2009-10-22, Bremen, Germany. Volltext nicht frei. filefile

  Böttcher, Carmen and Hannemann, Volker and Lüdeke, Heinrich (2007) Simulation of Magnetohydrodynamic Effects on an Ionised Hypersonic Flow by Using the TAU Code. In: New Results in Numerical and Experimental Fluid Mechanics VI, 96. Springer. pp. 300-308. ISBN 978-3-540-74458-0. Volltext nicht frei. filefile

  Böttcher, Carmen and Longo, Jose M. (2008) Simulation and Analysis of Magnetohydrodynamic Flows Using the DLR TAU Code - Mediums Air and Argon. 2nd International ARA Days, 2008-10-21 - 2008-10-23, Arcachon, France. (Unpublished) Volltext nicht frei. filefile

  Böttcher, Carmen and Longo, Jose Maria (2009) Simulation magnetohydrodynamischer Strömungen in Argon unter Verwendung des DLR TAU-Codes. Other. file

C

  Chapuis, M. and Fedina, E. and Fureby, Christer and Hannemann, Klaus and Karl, Sebastian and Martinez Schramm, Jan (2013) A Computational Study of the HySHOT II Combustor Performance. Proceedings of the Combustion Institute, Vol. 34 (2), pp. 2101-2109. Elsevier. DOI: 10.1016/j.proci.2012.07.014. ISSN 1540-7489. Volltext nicht online.

  Ciezki, Helmut and Friess, Martin and Dankert, Carl and Kanka, Bernhard and Scheiffele, Matthias and Schmücker, Martin (2008) Flugkörper-Werkstoffe für den extremen Heißgaseinsatz. Tagungsband Symposium WSE 2008. Volltext nicht online.

D

  Dankert, Carl and Clauss, Walter and Grisch, Frédéric (2008) Applying CARS to HEG at Mach 6 Conditions. DLR-Interner Bericht. DLR-IB 224-2007 A11, 17 S. Volltext nicht online.

  Dankert, Carl and Millan, Pierre (2012) Next Steps in MOTAR / Task Leader Discussion / Brainstorming on Cooperation. MOTAR scientific workshop, 05. - 06.Juni.2012, Toulouse, Frankreich. Volltext nicht online.

  Dankert, Carl and Otto, Hannes (2008) Experimental Investigation and Numerical Simulation on a Missile Radome at Mach 6. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design Notes, Vol. 96. Springer Verlag Berlin, Heidelberg, New York. pp. 317-323. ISBN 978-3-540-74458-0. Volltext nicht online.

  Dettleff, Georg (2006) Thruster Contamination Shield Testing Test Report. DLR-Interner Bericht. DLR-IB 224-2005 A23, 123 S. Volltext nicht online.

  Dettleff, Georg (2006) Cover Glass Contamination Tests. DLR-Interner Bericht. DLR-IB 224-2005 A20, 76 S. Volltext nicht online.

  Dettleff, Georg and Grabe, Martin (2011) Basics of Plume Impingement Analysis for Small Chemical and Cold Gas Thrusters. In: AVT/VKI Lecture Series RTO Educational Notes, Models and Computational Methods for Rarefied Flows (CD-ROM, Paper 12). RTO/NATO. pp. 1-40. ISBN 978-92-837-0129-3. Volltext nicht online.

  Dettleff, Georg and Hannemann, Klaus and Walter, Bernd and Ziegenhagen, Stefan (2005) Determination of a price information for the upgrade of the SISP 76 km altitude facility with a liquid helium driven cryopump for plume analysis. DLR-Interner Bericht. DLR-IB 224-2005 C 15, 42 S. Volltext nicht online.

  Dittrich, R. (2010) D2.4.1 Report on DLR MDO Tool for High-Speed Design. Project Report. file

  Dittrich, R. (2010) D2.4.2 Report on the Application of MDO Approaches for a Mach 6 SST. Project Report. file

  Dittrich, Robert (2013) Multidisziplinärer Vorentwurf einer Mach 6 - Hyperschalltransport-Konfiguration mit Hilfe eines Optimierungsverfahrens. Dissertation. DLR-Forschungsbericht. DLR-FB-2013-10, 142 S. Volltext nicht online.

  Dittrich, Robert and Eggers, Thino and Otto, Hannes (2010) Analysis of the Hypersonic Flow Field around the Skylon Vehicle. DLR-Interner Bericht. DLR-IB 124-2010/912. (Unpublished) Volltext nicht online.

  Dittrich, R. and Longo, J.M.A (2010) Preliminary Design of a Mach 6 Configuration using MDO. In: Springer. ISBN 978-3-642-14242-0. ISSN 1612-2909 file

  Dittrich, R. and Longo, J.M.A. and Carrier, G. and Duveau, P. and Salah El Din, I. and Thepot, R. (2008) Multi-Disciplinary Analysis and Optimization of Hypersonic Transport Aircrafts. Sixth European Symposium on Aerothermodynamics for Space Vehicles, 3.-6. Nov. 2008, Versailles, Frankreich. file

  Dumont, Etienne and Mierheim, Olaf and Chrupalla, David and Klevanski, J. and Bozic, Ognjan and Kopp, Alexander and Karl, Sebastian and Johannsson, Magni and Stief, Malte and David, Emmanuelle and Ludwig, Carina and Keiderling, David and Saile, Dominik and Poppe, Georg and Koch, Patrick and Schnepper, K. and Kirschner, Michael and Degenhardt, Richard and Schmidt, Volker and Manfletti, C. (2014) Ariane 6 PPH architecture: Critical Analysis - First iteration loop. DLR-Interner Bericht. X-TRAS TN-002/2013, 228 S. Volltext nicht online.

E

  Eggers, Th. and Longo, J.M.A. and Gülhan, A. and Hörschgen, M. and Stamminger, A. and Turner, J. (2006) Preliminary Post-Flight Data Analysis of the SHEFEX Experiment. In: 1st International ARA Days, "Atmospheric Reentry Systems, Missions and Vehicles". 1st International ARA Days, "Atmospheric Reentry Systems, Missions and Vehicles", 2006-07-03 - 2006-07-05, Arcachon. Volltext nicht online.

  Eggers, Thino (2012) Numerical Investigation on the potential of steam cooling for the skylon spaceplane in hypersonic flow. In: Procceedings of the 28th International Congress of the Aeronautical Science, ICAS 2012. 28th international congress of the aeronautical science, 23.-28. Sep. 2012, Brisbane. Volltext nicht frei. file

  Eggers, Thino and Bartolome Calvo, Javier and Wolkow, S. (2013) Application of a Coupling of Flight Mechanics and Aerodynamics to predict the SHEFEX I Ascent Phase. In: Notes in Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics VIII, Vol. 121. Springer Verlag. pp. 67-74. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht online.

  Eggers, Thino and Dittrich, Robert and Varvill, Richard (2011) Numerical Analysis of the SKYLON Spaceplane in Hypersonic Flow. In: AIAA Proceedings. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 11-14 April 2011, San Francisco, United States of America. Volltext nicht frei. file

  Eggers, Th. and Barth, T. (2006) Aerodynamic Analysis of the DLR Flight Experiment SHEFEX. In: 14th Int. Space Planes and Hypersonic Systems and Technologies Conference. 14th Int. Space Planes and Hypersonic Systems and Technologies Conference, 2006-11-08, Canberra (Australia). Volltext nicht frei. file

  Eggers, Thino (2012) The Shefex II experimental re-entry vehicle: Presentation of flight test results. 28th International Congress of the Aeronautical Science, 23.-28. Sep. 2012, Brisbane, Australien. file

  Eggers, Thino and Gräßlin, Michael (2008) LAYOUT OF HYPERSONIC VEHICLES BY COUPLING OF AERODYNAMICS AND FLIGHTMECHANICS. In: Tagungsband. 2nd International ARA Days “10 YEARS AFTER ARD”, 21–23 October 2008, Arcachon, Fance. Volltext nicht frei. file

  Eggers, Thino and Longo, José M. A. and Turner, John and Jung, Wolfgang and Hörschgen, Marcus and Stamminger, Andreas and Gülhan, Ali and Siebe, Frank and Requardt, G. and Laux, Thorsten and Reimer, T. and Weihs, Hendrik (2006) The SHEFEX Flight Experiment - Pathfinder Experiment for a Sky Based Test Facility. In: Proceedings AIAA 14th Spaceplane Systems and Technologies Conference. 14th Spaceplane Systems and Technologies Conference, 2006-11-08, Canberra, Australia. Volltext nicht frei. file

  Eggers, Thino and Stamminger, Andreas and Hörschgen, Marcus and Jung, Wolfgang and Turner, John (2005) The Hypersonic Experiment SHEFEX - Aerotheromdynamic Layout, Vehicle Development and First Flight Results. In: Proceedings 6th International Launcher Symposium on Launcher Technologies. 6th International Symposium on Launcher Technologies, 2005-11-08 - 2005-11-11, München, Deutschland. file

  Eichert, Florian (2002) Untersuchung der Einflüsse von scharfkantigen Oberflächenübergängen auf die Wärmelasten des Thermalschutzsystems von Wiedereintrittsfahrzeugen. Other. Volltext nicht online.

  Eisel, Matthias (2011) Erprobung eines Messverfahrens zur Charakterisierung von Freistrahlen aus Kleintriebwerken. Diploma, DLR. Volltext nicht online.

F

  Felix, Langfeldt (2011) Modellierung und Simulation von einphasigen, turbulenten Freistrahlen in unter- und transkritischen Umgebungen für Raketenanwendungen. Bachelor's, Hochschule für Angewandte Wissenschaften Hamburg. Volltext nicht online.

  Fertig, M and Eggers, T (2011) DLR-CFD Activities Synthesis Report :EXM-DM-TNO-DLR-0002. DLR-Interner Bericht. DLR-IB 124-2011/915, 40 S. Volltext nicht frei. file

  Fertig, M and Neeb, D and Gülhan, A (2011) Windtunnel Rebuilding and Extrapolation to Flight at Transonic Speed for Exomars. ESA Comminications. 7th European Symposium on Aerothermodynamics for Space Vehicles, 09.-12. Mai 2011, Brügge, Belgien. ISBN 978 92 9092 256 8. ISSN 1609-042X Volltext nicht frei. file

  Filimon, Alexander and Lüdeke, Heinrich (2007) TRANSONIC AFTERBODY SIMULATION. In: Proceedings of the ATAC-FSCD WORKSHOP « AFTER-BODY AND NOZZLE FLOWS » November 15-16 at ESA/Estec, Noordwijk, The Netherlands. ATAC-FSCD WORKSHOP: « AFTER-BODY AND NOZZLE FLOWS », 2006-11-15 - 2006-11-16, ESA/Estec, Noordwijk, The Netherlands. (In Press) file

  Franze, Marius (2013) Bestimmung der dynamischen Derivative scharfkantiger Raumfahrzeuge. Diploma, Technische Universität Dresden. Volltext nicht online.

  Funck, Alexander (2010) Fluguntersuchungen zur Kurzzeitfestigkeit an Raumfahrtwerk- und Treibstoffen. Diploma, Technische universität Braunschweig. Volltext nicht online.

  Funck, Alexander (2008) Auslegung eines Projektils mit chemischem Hybridantrieb. Other. Volltext nicht online.

  Funk, Alexander (2007) Strömungsmechanische Untersuchung eines Ariane 5 Liquid-Fly-Back-Boosters in transsonischer Anströmung. Diploma, Hochschule Bremen. Volltext nicht online.

  Fureby, C. and Chapuis, M. and Fedina, E. and Karl, Sebastian (2011) CFD Analysis of the HyShot II scramjet combustor. Proceedings of the Combustion Institute, Vol. 33 (2), pp. 2399-2405. Elsevier. DOI: 10.1016/j.proci.2010.07.055. ISSN 1540-7889. Volltext nicht online.

G

  Gardner, Anthony and Hannemann, Klaus and Paull, Alan and Steelant, Johan (2004) Ground Testing of the HyShot Supersonic Combustion Flight Experiment in HEG. 24th International Symposium on Shock Waves, 2004-07-11 - 2004-07-16, Beijing, CHINA. ISBN 3-540-22497-1. Volltext nicht online.

  Gardner, Anthony Donald (2007) HyShot scramjet testing in the HEG. Dissertation. DLR-Forschungsbericht. FB 2007-14, 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 and Hannemann, Klaus (2004) Evaluation of full engine scramjet technology. DLR-Interner Bericht. DLR-IB 224-2004 A 11, 64 S. Volltext nicht online.

  Gardner, Anthony Donald and Hannemann, Klaus (2004) Evaluation of full -engine scramjet technology. Executive Summary. DLR-Interner Bericht. DLR-IB 224-2004 A 12, 9 S. Volltext nicht online.

  Gardner, Anthony Donald and Hannemann, Klaus and Steelant, Johan and Paull, Allan (2004) Ground Testing of the HyShot Supersonic Combustion Flight Experiment in HEG and Comparison with Flight Data (AIAA 2004–3345). 40th AIAA Joint Propulsion Conference, July 11–14, 2004., Fort Lauderdale, Florida. Volltext nicht online.

  Gardner, Anthony Donald and Jacobs, Peter A. and Hannemann, Klaus (2004) End-to-end modelling and design of a new operating condition for HEG. New results in experimental fluids IV, 87. Springer-verlag. DOI: TL570.S65.2004. Volltext nicht online.

  Gauer, Markus (2009) Implementation of the VOF method in the DLR TAU code. In: JPC 2009 Proceedings. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 02.-05.08.2009, Denver, USA. Volltext nicht online.

  Gauer, Markus (2013) Simulation of the sloshing behaviour of two-phase flows in cryogenic rocket upper stages. DLR-Forschungsbericht. DLR-FB--2013-07, 149 S. Bibliotheks- und Informationswesen. Volltext nicht online.

  Gauer, Markus and Hannemann, Klaus (2010) Interface advection with the TAU code and the CICSAM method on arbitrary grids. 7th International Conference on Multiphase Flow, May 30-June 4, 2010, Tampa, FL, USA. Volltext nicht online.

  Gauer, Markus and Lambert , Markus and Hannemann, Klaus (2012) Two-phase flow modeling combining the CICSAM with the projection method. 48th AIAA/ASME/SAE/SAE/ASEE Joint Propulsion Conference & Exhibit, 29. Jul. - 01. Aug. 2012, Atlanta, Georgia, USA. Volltext nicht online.

  Gauer, Markus and Paull, Allan (2008) Numerical Investigation of a Spiked Blunt Nose Cone at Hypersonic Speeds. Journal of Spacecraft and Rockets, Vol. 45 (3, May-June 2008), pp. 459-471. DOI: 10.2514/1.30590. ISSN 0022-4650. Volltext nicht online.

  Gauer, Markus and Telitschkin, D. and Gotzig, U. and Battoneau, Y. and Johansson, H. and Ivanov, M. and Palmer, P. and Wiegerink, R. (2012) PRECISE - First Results of the Development of a MEMS-based Monopropellant Micro Chemical Propulsion System. 8th ESA Round Table on Micro and Nano Technologies for Space Applications, 15. 18. Oct. 2012, Noordwijk, The Netherlands. Volltext nicht online.

  Gauer, Markus and Telitschkin, Dimitri and Gotzig, Ulrich and Batonneau, Yann and Johansson, Hakan and Ivanov, Mikhail and Palmer, Phil and Wiegerink, Remco (2013) First results of PRECISE—Development of a MEMS-based monopropellant micro chemical propulsion system. Acta Astronautica (Volume 93), pp. 77-83. Elsevier. DOI: 10.1016/j.actaastro.2013.06.010. ISSN 0094-5765. Volltext nicht online.

  Gauer, Markus and Telitschkin, Dimitri and Gotzig, Ulrich and Batonneau, Yann and Johansson, Håkan and Ivanov, Mikhail and Palmer, Phil and Wiegerink, Remco J. (2012) PRECISE - development of a MEMSbased monopropellant micro Chemical Propulsion System. 48th AIAA/ASME/SAE/SAE/ASEE Joint Propulsion Conference & Exhibit, 29. Jul. - 01. Aug. 2012, Atlanta, Georgia, USA. Volltext nicht online.

  Gauer, Markus and Telitschkin, D. and Gotzig, U. and Battoneau, Y. and Johansson, H. and Ivanov, M. and Palmer, P. and Wiegerink, R. (2012) PRECISE - First Results of the Development of a MEMS-based Monopropellant Micro Chemical Propulsion System. 63rd International Astronautical Congress, 01. - 05. Oktober 2012, Naples, Italy. Volltext nicht frei. file

  Gehre, Rolf Michael (2010) Aerothermodynamische Untersuchung zu Shefex-II unter HEG-Bedingungen. Diploma, Univervität Stuttgart. Volltext nicht online.

  Gerstmann, Jens and van Foreest, Arnold and Dittrich, Lutz and Gauer, Markus (2009) German Research Cooperation Upper Stage. In: Conference proceedings. CEAS 2009 European Air and Space Conference, 26.10. - 29.10.2009, Manchester, UK. Volltext nicht online.

  Giese, Tobias (2013) Kalibrierung der Anströmungsbedingungen und Charakterisierung der Störgrößen am Hochenthalpiekanal Göttingen (HEG). Diploma, Technische Hochschule Berlin. Volltext nicht online.

  Giese, Tobias (2012) Numerische Untersuchung von Transitionsbeeinflussung mittels passiver poröser Oberflächen. Other, Technische Universität Berlin. Volltext nicht frei. file

  Gnemmi, Patrick and Adeli, Reza and Longo, José Maria (2008) Computational Comparison of the Interaction of a Lateral Jet on a Supersonic Generic Missile. AIAA Atmospheric Flight Mechanics Conference and Exhibit, 2008-18-08 - 2008-21-08, Honolulu, Hawaii (USA). file

  Gotor, Maria del Pilar Gonzales and Merino, Alejandro Ruiz and Astorg, Jean-Marc and Louaas, Eric and Talbot, Christophe and Longo, José Maria and Sippel, Martin and Froebel, Ludger (2008) Aldebaran: A "System" Demonstrator Project for new Generations of Space Transportation. IAC-08-D2.6 59th International Astronautical Congress, 2008-09-29 - 2008-10-03, Glasgow, Scotland. file

  Grabe, Martin (2009) Modellierung der Strömung in Satellitensteuerdüsen mit der DSMC-Methode. 124. Norddeutsches Mechanik-Kolloquium, Clausthal-Zellerfeld. (Unpublished) Volltext nicht online.

  Grabe, Martin (2010) Characterization of a free molecular pressure probe employing gas-kinetic simulation. 21st Liepmann-Ludwieg-Seminar, 01.-07. May 2010, Santa Barbara, USA. Volltext nicht frei. file

  Grabe, Martin (2012) Response of the Patterson Probe in the Transition Flow Regime. 28th International Symposium on Rarefied Gas Dynamics, RGD28, 09. - 13. Jul. 2012, Zaragoza, Spain. Volltext nicht online.

  Grabe, Martin and Hannemann, Klaus and Fasoulas, Stefanos (2008) Numerical Simulation of Nozzle Flow into High Vacuum Using Kinetic and Continuum Approaches. 16. DGLR/STAB Symposium, 2008-11-3 - 2008-11-04, Aachen. (Submitted) Volltext nicht online.

  Grabe, Martin (2008) Numerische Simulation einer Stickstoff-Düsenströmung mit gaskinetischen und kontinuumsmechanischen Verfahren. Diploma, TU Dresden. file

  Grabe, Martin (2008) Numerical Simulation of Nitrogen Nozzle Expansion Using Kinetic and Continuum Approaches. 59th International Astronautical Conference, 2008-09-28, Glasgow. file

  Grabe, Martin and Dettleff, Georg and Boettcher, Rolf-Detlef and Hannemann, Klaus (2010) Characterization of a Free-Molecular Pressure Probe employing Gas-Kinetic Simulation. 17. DGLR-Fachsymposium der STAB, 09.-10. Nov. 2010, Berlin, Deutschland. file

  Grabe, Martin and Dettleff, Georg and Boettcher, Rolf-Detlef and Hannemann, Klaus (2013) Characterization of the Free-Molecular Pressure Probe Employing Gas-Kinetic Simulation. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical axperimental Fluid Mechanics VIII, Vol. 1. Springer Verlag, Heidelberg New York Dordrecht London. pp. 109-116. ISBN 978-3-642-35679-7. ISSN 1612-2909 file

  Grabe, Martin and Fasoulas, Stefanos and Hannemann, Klaus (2010) Numerical Simulation of Nozzle Flow into High Vacuum Using Kinetic and Continuum Approaches. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 112. Springer. pp. 423-430. ISBN 978-3-642-14242-0. ISSN 1612-2909 file

  Génin, Chloe and Stark, Ralf and Karl, Sebastian and Schneider, Dirk (2012) Numerical investigation of Dual Bell Nozzle Flow Field. 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 29. Jul. - 1. Aug 2012, Atlanta, GA, USA. DOI: 10.2514/6.2012-4164. Volltext nicht frei. file

H

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

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

  Hannemann, Klaus (2005) Ground testing of the HYShot supersonic combustion flight experiment in HEG. 5th European Symposium on Aerothermodynamics for Space Vehicles, 2004-11-08 - 2004-11-11, Köln. Volltext nicht online.

  Hannemann, Klaus (2006) Design of a Flight Configuration for High Speed Airbreathing Propulsion Identification of the Flight Test Programm. DLR-Interner Bericht. DLR-IB 224-2006 C31, 46 S. Volltext nicht online.

  Hannemann, Klaus (2006) Design of a Flight Test Configuration for High-Speed Airbreathing Propulsion - Intermediate Review Phase 1. DLR-Interner Bericht. DLR-IB 224-C-2006 C33, 29 S. Volltext nicht online.

  Hannemann, Klaus (2008) Report on the 26th international symposium on shock waves. Shock Waves, 17 (6), pp. 457-460. Springer-Verlag. DOI: 10.1007/s00193-008-0120-7. ISSN 0938-1287. Volltext nicht online.

  Hannemann, Klaus (2008) Experimental investigation of different scramjet hydrogen injection systems. Sixth European Symposium on Aerothermodynamics for Space Vehicles, 2008-11-3 - 2008-11-6, Versailles, Frankreich. (In Press) Volltext nicht online.

  Hannemann, Klaus (2008) Hypersonics in Germany. 15th AIAA Int. Space Planes and Hypersonic Systems and Technology Conference, 2008-04-28 - 2008-05-01, Dayton, OH (USA). Volltext nicht online.

  Hannemann, Klaus (2009) Germany National Report. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 29. Okt. - 22. Okt. 2009, Bremen. (Unpublished) Volltext nicht online.

  Hannemann, Klaus (2009) Ground based testing and numerical modelling of supersonic combustion flow paths. In: Shock Waves. Springer. 27th International Symposium on Shock Waves, St. Petersburg. (Submitted) Volltext nicht online.

  Hannemann, Klaus (2009) Scramjet Research Related to the High Enthalpy Shock Tunnel Göttingen. 75th Birthday Symposium and Dinner Celebration for Hans Hornung, 20.03.2009, Pasadena, USA. Volltext nicht online.

  Hannemann, Klaus (2011) Hypersonic Flight and (Re)-Entry in Germany - Overview and Selected Projects. 17th AIAA International Space Planes and Hypersonic Systems and Technology Conference, 11. April - 14. April 2011, San Francisco, USA. Volltext nicht online.

  Hannemann, Klaus (2012) Title confidential. DLR-Interner Bericht. DLR-IB 224-2012 C 123, 22 S. Volltext nicht online.

  Hannemann, Klaus and Eggers, Thino (2011) The DLR Spacecraft Department – An Overview. Postgraduate Seminar , 02.11.2011, Hsinchu, Taiwan. Volltext nicht online.

  Hannemann, Klaus and Karl, Sebastian and Martinez Schramm, Jan and Laurence, Stuart (2011) Methodology of a Combined Ground Based Testing and Numerical Modelling Analysis of Supersonic Combustion Flow Paths. Conference of Aeronautical Society of the Republic of China & Aerospace Research Program of National Science Council, 05.11.2011, Taichung, Taiwan. Volltext nicht online.

  Hannemann, Klaus and Karl, Sebastian and Martinez Schramm, Jan and Laurence , Stuart (2011) Methodology of a Combined Ground Based Testing and Numerical Modelling Analysis of Supersonic Combustion Flow Paths. Seminar in Fluid Mechanics, 19.04.2011, Stanford, USA. Volltext nicht online.

  Hannemann, Klaus and Karl, Sebastian and Martinez Schramm, Jan and Steelant, Johan (2010) Methodology of a combined ground based testing and numerical modelling analysis of supersonic combustion flow paths. Shock Waves, Vol. 20 (5), pp. 353-366. Springer Verlag. DOI: 10.1007/s00193-010-0269-8. ISSN 0938-1287. Volltext nicht online.

  Hannemann, Klaus and Longo, José (2011) Aerothermodynamik und Wiedereintritt. In: Handbuch der Raumfahrttechnik Carl Hanser Verlag München. pp. 102-117. ISBN 978-3-446-42406-7. Volltext nicht online.

  Hannemann, Klaus and Longo, José Maria (2009) Aerothermodynamics and Reentry. In: Handbook of Space Technology John Wiley & Sons Ltd.. ISBN 978-0-470-69739-9. Volltext nicht online.

  Hannemann, Klaus and Longo, José (2007) Aerothermodynamik und Wiedereintritt. In: Handbuch der Raumfahrttechnik Hanser Verlag. ISBN 978-3-446-41185-2. Volltext nicht online.

  Hannemann, Klaus and Lüdecke, Heinrich and Pallegoix, Jean-Francois and Ollivier, Arnaud and Lambaré, Hadrien and Maseland, Hans and Geurts, E. G. M. and Frey, Manuel and Deck, Sebastien and Schrijer, F.F.J. and Scarano, F. and Schwane, Richard (2011) Launch Vehicle Base Buffeting - Recent Experimental and Numerical Investigations. 7th European Symposium on Aerothermodynamics for Space Vehicles, 9. Mai - 12. Mai 2011, Brugge, Belgien. Volltext nicht online.

  Hannemann, Klaus and Martinez Schramm, Jan (2007) High Enthalpy, High Pressure Short Duration Testing of Hypersonic Flows. In: Springer Handbook of Experimental Fluid Mechanics Springer-Verlag Berlin Heidelberg. pp. 1081-1125. ISBN 978-3-540-25141-5. Volltext nicht online.

  Hannemann, Klaus and Martinez Schramm, Jan and Karl, Sebastian (2008) Recent Extensions to the High Enthalpy Shock Tunnel Göttingen (HEG. 2nd International ARA Days, 2008-10-20 - 2008-10-23, Arcachon, Frankreich. (Submitted) Volltext nicht online.

  Hannemann, Klaus and Martinez Schramm, Jan and Wagner, Alexander and Karl, Sebastian and Hannemann, Volker (2010) A Closely Coupled Experimental and Numerical Approach for Hypersonic and High Enthalpy Flow Investigations Utilising the HEG Shock Tunnel and the DLR TAU Code - Part 1. In: NATO Research and Technology Organisation. Aerothermodynamic Design, Review on Ground Testing andCFD, 29 March - 1 April 2010, Rhode St. Genese, Belgium. ISBN 978-92-837-0121-7. Volltext nicht online.

  Hannemann, Klaus and Martinez Schramm, Jan and Wagner, Alexander and Karl, Sebastian and Hannemann, Volker (2010) A Closely Coupled Experimental and Numerical Approach for Hypersonic and High Enthalpy Flow Investigations Utilising the HEG Shock Tunnel and the DLR TAU Code - Part 2. In: NATO Research and Technology Organisation. Aerothermodynamic Design, Review on Ground Testing andCFD, 29 March - 1 April 2010, Rhode St. Genese, Belgium. ISBN 978-92-837-0121-7. Volltext nicht online.

  Hannemann, Klaus and Martinez Schramm, Jan and Wagner, Alexander and Karl, Sebastian and Hannemann, Volker (2011) A Closely Coupled Experimental and Numerical Approach for Hypersonic and High Enthalpy Flow Investigations Utilising the HEG Shock Tunnel and the DLR TAU Code. In: NATO Research and Technology Organisation (AVT 186), 8-1-8-66. Aerothermodynamic Design, Review on Ground Testing andCFD, 29 March - 1 April 2010, Rhode St. Genese, Belgium. ISBN 978-92-837-0121-7. Volltext nicht online.

  Hannemann, Klaus and Seiler, Friedrich (2009) 26th International Symposium on Shock Waves. Springer. 800 S. ISBN 978-3-540-85182-0. Volltext nicht online.

  Hannemann, Volker (2006) Numerical investigation of an effusion cooled thermal protection material. ICCFD4, 2006-07-10 - 2006-07-14, Ghent (Belgien). (Unpublished) Volltext nicht online.

  Hannemann, Volker and Mack, Andreas (2008) Chemical Non-Equilibrium Model of the Martian Atmosphere. Sixth European Symposium on Aerothermodynamics for Space Vehicles, 2008-11-3 - 2008-11-6, Versailles, Frankreich. (In Press) Volltext nicht online.

  Hannemann, Klaus (2013) Ausgewählte Phänomene der Raumfahrtaerodynamik. Physik im Weltraum, 10. Sept. 2013, Bad Honnef, Germany. Volltext nicht online.

  Hannemann, Volker and Siegmund, Alexander and Oßwald, Kai and Birken, Philipp and Weinman, Keith and Meister, Andreas (2012) Dissipation of upwind schemes at high wave numbers. International Conference on Computational Fluid Dynamics, ICCFD7, 09.-13. Jul. 2012, Hawaii, USA. file

  Hartwig, Alex (2011) Metallhaltige Brennstoffe für Hybrid-Raketentriebwerke. Other, Technische Universität Braunschweig. Volltext nicht online.

  Hashimoto, Tokitada and Rowan, Scott and Komuro, Tomoyuki and Sato, Kazuo and Itoh, Katsuhiro and Robinson, Matthew and Martinez Schramm, Jan and Hannemann, Klaus (2009) Application of HEG static pressure probe in HIEST. In: Shock Waves Springer. pp. 421-426. ISBN 978-3-540-85182-0. Volltext nicht online.

  Heumüller, Philipp (2012) Numerische Simulation von Wiedereintrittskörpern im Übergangsbereich zwischen Freimolekular- und Kontinuumsströmung. Other, Institut für Aerodynamik und Strömungstechnik. Volltext nicht online.

  Hink, R. and Hannemann, Volker and Eggers, Thino (2013) Extension of the Spalart-Allmaras One-Equation Turbulence Model for Effusion Cooling Problems. Deutscher Luft- und Raumfahrtkongress 2013, 10.-12. Sept. 2013, Stuttgart, Deutschland. Volltext nicht frei. file

  Hock, Stephan (2013) Heat Flux Determination in the High-Enthalpy Shock Tunnel G�ottingen Using the Temperature-Sensitive Paint Method. Master's. DLR-Interner Bericht. DLR-IB 224-2013 A 95, 106 S. Volltext nicht online.

  Hoffie, Andreas Frank (2008) Computational Fluid Dynamics Analysis of the Flap Efficiency of a Reentry Vehicle. Diploma, Universität Stuttgart. Volltext nicht online.

  Holz, André (2012) Experimentelle Untersuchungen zur Abgasstrahl-Wechselwirkung von zwei Kleintriebwerken unter weltraumähnlichen Hochvakuumbedingungen. Dissertation, Universität Stuttgart. file

  Holz, André and Dettleff, Georg and Hannemann, Klaus and Ziegenhagen, Stefan (2012) Experimental Investigation of Two Interacting Thruster-Plumes Downstream of the Nozzles. Space Propulsion 2012, 07. - 10. Mai 2012, Bordeaux, Frankreich. file

  Horchler, Tim (2011) Numerische Analyse des Wärmetransports durch Gasstrahlung beim atmosphärischen Wiedereintritt. Diploma, Geor-August Universität Göttingen. Volltext nicht online.

  Hurst, Jakob (2013) Implementation and testing of a time dependent acceleration model for the numerical simulation of sloshing. Diploma. DLR-Interner Bericht. DLR-IB 224-2013 A 91, 94 S. Volltext nicht online.

I

  Illi, Sebastian (2008) Aerothermodynamische Charakterisierung des aktiv gekühlten keramischen TPS - Experiments für SHEFEX II. Diploma, Universität Stuttgart. Volltext nicht online.

  Ivancic, B. and Riedmann, H. and Frey, M. and Knab, O. and Karl, Sebastian and Hannemann, Klaus (2013) Investigation of different modeling approaches for CFD simulation of high pressure rocket combustors. In: Proceedings of the 5th European Conference for Aerospace Sciences (P94), pp. 1-15. 5th European Conference for Aerospace Sciences (EUCASS), 01 .- 05. Juli 2013, München, Germany. Volltext nicht online.

J

  Jacobs, Peter A. and Gardner, Anthony Donald and Buttsworth, David R and Martinez-Schramm, Jan and Karl, Sebastian and Hannemann, Klaus (2004) End-to-End Modelling of the HEG Shock Tunnel. ISSW 24, 2004, Beijing. Volltext nicht online.

K

  Karl, Sebastian (2007) CFD Analysis of the HyShot Scramjet Configuration. 13. STAB-Workshop, 2007-11-14 - 2007-11-15, Göttingen. (Unpublished) Volltext nicht online.

  Karl, Sebastian (2007) Numerische Modellierung von turbulenten Verbrennungsprozessen in Raumfahrtantriebssystemen. 119. Norddeutsches Mechanik-Kolloquium, 2007-02-17, Göttingen. Volltext nicht online.

  Karl, Sebastian (2008) CFD Analysis of the HyShot II Scramjet Experiments in the HEG Shock Tunnel. 15th AIAA Int. Space Planes and Hypersonic Systems and Technology Conference, 2008-04-28 - 2008-05-01, Dayton, OH (USA). Volltext nicht online.

  Karl, Sebastian (2011) Numerical Investigation of a Generic Scramjet Configuration. Dissertation, Technische Universität Dresden. Volltext nicht online.

  Karl, Sebastian and Hannemann, Klaus (2006) Application of the DLR TAU-Code to the RCM-1 Test Case: Penn State Preburner Combustor. In: Proceedings of the 3rd International workshop on Rocket Combustion Modeling Snecma 2006. 3rd International Workshop on Rocket Combustion Modeling, 2006-03-13 - 2006-03-15, Paris. Volltext nicht online.

  Karl, Sebastian and Hannemann, Klaus (2006) Application of the DLR TAU-Code to the RCM-4 Test Case: Microcombustor Ignition. In: Proceedings of the 3rd International workshop on Rocket Combustion Modeling Snecma 2006. 3rd International Workshop on Rocket Combustion Modeling, 2006-03-13 - 2006-03-15, Paris. Volltext nicht online.

  Karl, Sebastian and Hannemann, Klaus (2006) Extension of the DLR TAU Code with finite rate supersonic combustion modelling. [Other] Volltext nicht online.

  Karl, Sebastian and Hannemann, Klaus (2006) Extension of the DLR TAU Code with finite rate super-sonic combustion modelling. Other. Volltext nicht online.

  Karl, Sebastian and Hannemann, Klaus (2006) LAPCAT Deliverable 6.5.2: Survey and implementation of turbulent supersonic combustion models. Project Report. Volltext nicht online.

  Karl, Sebastian and Hannemann, Klaus (2006) FSCD Testcase 2b: ONERA Planar Nozzle fed by Hot Gases in Mascotte. Numerical Investigation with the DLR TAU Code. In: Proceedings, FSCD-ATAC Workshop, p. 4. FSCD-ATAC Workshop, 2006-11-15 - 2006-11-16, Noordwijk, The Netherlands. Volltext nicht online.

  Karl, Sebastian and Hannemann, Klaus and Hans G., Hornung (2012) Bluntness Effects in Hypersonic FLow over Slender Cones and Wedges. In: 28th International Symposium on Shock Waves Shock Waves 2, Vol. 2. Springer Verlag, Berlin Heidelberg. pp. 691-696. ISBN 978-3-642-25684-4. Volltext nicht online.

  Karl, Sebastian and Hannemann, Klaus and Mack, Andreas and Steelant, Johan (2006) CFD Analysis of the HyShot Supersonic Combustion Flight Experiment Configuration. In: Proceedings of the 14th AIAA Space Planes and Hypersonic Systems Conference 2006 (AIAA 2006-8041). American Institute of Aeronautics and Astronautics. 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006-11-6 - 2006-11-9, Canberra (Australien). Volltext nicht online.

  Karl, Sebastian and Hannemann, Klaus and Steelant, Johan (2008) CFD Investigation of Scaling Laws for Hydrogen Fuelled Scramjet Combustors. Sixth European Symposium on Aerothermodynamics for Space Vehicles, 2008-11-3 - 2008-11-6, Versailles, Frankreich. (In Press) Volltext nicht online.

  Karl, Sebastian and Hannemann, Klaus and Steelant, Johan and Mack, Andreas (2006) CFD Analysis of the HyShot Supersonic Combustion Flight Experiment Configuration. In: Conference Proceedings. American Institute of Aeronautics and Astronautics. 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, 2006-11-06 - 2006-11-09, Canberra. Volltext nicht online.

  Karl, Sebastian and Lambert, Markus (2009) CFD Analysis of radiative heat loading on hypervelocity re-entry vehicles. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 19.-22. Okt. 2009, Bremen. Volltext nicht online.

  Karl, Sebastian and Lambert, Markus (2011) CFD Modelling of Re-entry Flows including Gas Radiation. 7th European Aerothermodynamics Symposium, 09.-12. May 2011, Brugge, Belgium. Volltext nicht online.

  Karl, Sebastian and Laurence, Stuart and Martinez, Jan and Hannmann, Klaus (2012) CFD Analysis of Unsteady Combustion Phenomena in the HyShot-II Scramjet Configuration. American Institute of Aeronautics and Astronautics. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, 24. - 28. Sep. 2012, Tours, France. DOI: 10.2514/6.2012-5912. Volltext nicht online.

  Karl, Sebastian and Lüdeke, Heinrich (2012) Application of the DLR Tau Code to predict acoustic damping rates in generic combustion chamber configurations. DLR-Interner Bericht. DLR-IB 224-2012 A 67, 11 S. Volltext nicht online.

  Karl, Sebastian and Lüdeke, Heinrich (2008) Application of the DLR Tau code to predict acoustic damping rates in generic combustion chamber configurations. 1st REST Modelling Workshop, 2008-10-1 - 2008-10-2, Paris, Frankreich. (In Press) Volltext nicht online.

  Karl, Sebastian and Markus, Lambert (2009) CFD modeling of hypervelocity re-entry flows including gas radiation. 27th International Symposium on Shock Waves, 19.-24. Juli 2009, St. Petersburg (Russia). Volltext nicht online.

  Karl, Sebastian and Martinez Schramm, Jan and Hannemann, Klaus (2004) Experimental and Numerical Investigation of High Enthalpy Flow Past a Cylinder in HEG. 24th International Symposium on Shock Waves, 2004-07-11 - 2004-07-16, Beijing, CHINA. ISBN 3-540-22497-1. Volltext nicht online.

  Karl, Sebastian and Martinez Schramm, Jan and Hannemann, Klaus (2004) High Enthalpy Shock Tunnel Flow Past a Cylinder: A Basis for CFD Validation. In: Notes on Numerical Fluid Mechanics and Multidisziplinary Design IV Springer. Volltext nicht online.

  Karl, Sebastian and Martinez Schramm, Jan and Hannemann, Klaus (2003) High Enthalpy Cylinder Flow in HEG: A Basis for CFD Validation. In: Conference Proceedings. American Institute of Aeronautics and Astronautics. 33rd AIAA Fluid Dynamics Conference, 2003-06-23 - 2003-06-26, Orlando, FL (USA). Volltext nicht online.

  Karl, Sebastian and Martinez Schramm, Jan and Hannemann, Klaus (2011) CFD Analysis of Unstart Characteristics of the HyShot-II Scramjet Configuration in the HEG Shock Tunnel. 17th AIAA International Space Planes and Hypersonic Systems and Technology Conference, April 2011, San Francisco, USA. Volltext nicht online.

  Karl, Sebastian and Martinez Schramm, Jan and Hannemann, Klaus (2012) High Enthalpy Non-Equilibrium Shock Layer Flows: Selected Practical Applications. In: Shock Wave Science and Technology Reference Library Springer Verlag. pp. 299-336. ISBN 978-3-642-25118-4. Volltext nicht online.

  Karl, Sebastian and Potter, Daniel and Lambert, Markus and Hannemann, Klaus (2013) CFD Analysis of radiative heat loading on hypervelocity re-entry vehicles. American Institute of Aeronautics and Astronautics. 21st AIAA Computational Fluid Dynamics Conference, 24. - 27. Juni 2013, San-Diego, USA. Volltext nicht online.

  Keiderling, David and Hannemann, Klaus (2013) Test Case Results and Comparison for 1st ESA Workshop on the Physics of Microgravity Cryogenic Sloshing Motions. 1st ESA Workshop on the Physics of Microgravity Cryogenic Sloshing Motions, 18. - 19. Dez. 2013, Noordwijk, Niederlande. Volltext nicht frei. filefile

  Kersken, Hans-Peter and Schreiber, Andreas and Heinrich, Ralf and Kügeler, Edmund and Mack, Andreas and Neumann, Jens and Schäfer, Roger (2002) TENT - Eine Softwareintegrationsumgebung für multidisziplinäre Simulationen. In: Tagungsband Deutscher Luft- und Raumfahrtkongress 2002. Deutscher Luft- und Raumfahrtkongress 2002, 2002-09-26, Stuttgart. Volltext nicht online.

  Kießling, André and Wagner, Alexander (2012) Design of a Hot Wall Wind Tunnel Model for Investigation of the Shock-Wave / Boundary-Layer Interaction in the High Enthalpy Shock Tunnel Göttingen (HEG). Diploma, Hochschule Coburg, Coburg University of Applied Sciences. Volltext nicht frei. file

  Kirmse, Tania and Agocs, Janos and Schröder, Andreas and Martinez Schramm, Jan and Karl, Sebastian and Hannemann, Klaus (2011) Application of Particle Image Velocimetry and the Background Oriented Schlieren Technique in the High-Enthalpy Shock Tunnel Göttingen. Shock Waves. Springer Verlag. DOI: 10.1007/s00193-011-0314. Volltext nicht online.

  Kirmse, Tania and Schröder, Andreas and Kompenhans, Jürgen and Martinez Schramm, Jan and Karl, Sebastian and Hannemann, Klaus (2010) Application of Particle Image Velocimetry and the Background Oriented Schlieren Technique in the High Enthalpy Shock Tunnel Göttingen (HEG). Seminar an der Nanjing University of Aeronautics and Astronautics (NUAA), 16. Sept. 2010, Nanjing, China. Volltext nicht online.

  Kirmse, Tania and Schröder, Andreas and Martinez Schramm, Jan and Karl, Sebastian and Hannemann, Klaus (2009) Application of Particle Image Velocimetry and the Background Oriented Schlieren Technique in the High Enthalpy Shock Tunnel Göttingen HEG. 27th International Symposium on Shock Waves, 2009-07-19 - 2009-07-24, St. Petersburg (Russia). ISBN 978-593634-047-5. Volltext nicht online.

  Klein, Christian and Henne , Ulrich and Sachs, Werner and Hock, Stephan and Falk, Nora and Ondrus, Vladimir and Beifuß, Uwe and Schaber, Sven (2013) Pressure Measurement on Rotating Propeller Blades by means of the Pressure-Sensitive Paint Lifetime method. Seminar China Academy of Aerospace Aerodynamics (CAAA), 13. Aug. 2013, Beijing, P.R. China. Volltext nicht online.

  Koch, Patrick (2013) Abbrandrate von festen Brennstoffen bei Hybridraketentriebwerken. Other. Volltext nicht online.

  Koch, Patrick (2014) Optimierung der Geometrie fester Brennstoffblöcke bei Hybrid- und Feststoffraketentriebwerken. Diploma, Technische Universität Carolo-Wilhelmina zu Braunschweig. Volltext nicht online.

  Kopp, Alexander and Dietlein, Ingrid and Barth, Tarik (2009) Systemanalyse für scharfkantige Wiedereintrittsfahrzeuge. Deutscher Luft- und Raumfahrtkongress 2009, 08.-10. Sep. 2009, Aachen, Deutschland. file

  Korfanty, Marius (2006) Einfluss des Rumpfendes eines Hyperschallvehikels auf die Klappenwirksamkeit. Diploma, Universität Stuttgart. Volltext nicht online.

  Korfanty, Marius and Longo, José Maria (2008) CFD based Dynamic Analysis of Atmospheric Re-Entry Vehicles. 2nd International ARA Days, 2008-21-10 - 2008-23-10, Arcachon (France). file

  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) file

  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. file

  Kramer, Timo (2014) Verbrennungskinetik von AL - Partikeln in einem Hybridraketentriebwerk. Diploma, Technische Universität Braunschweig. Volltext nicht online.

  Kuchi-Ishi, Shigeru (2005) The Development of a New Viscous Shock-Layer Code for Computing Hypersonic Flows around Blunted Body and its Applications. DLR-Interner Bericht. DLR-IB 224-2005 A19, 58 S. Volltext nicht online.

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  Lancelle, Daniel and Bozic, Ognjan (2013) Simulation of an Ablative Thermal Protection System for the Hypersonic Ascend of an Electromagnetically Launched Payload Carrier. 5th European Conference for Aeronautics and Space Sciences (EUCASS) 2013, 01.-05. Jul. 2013, München, Deutschland. file

  Lancelle, Daniel and Bozic, Ognjan and Köke, Hardy (2012) Flight Test Results of Investigation of Acceleration Effects on a Gun Launched Rocket Engine. 16th EML Symposium, 15.-19. Mai 2012, Peking, China. Volltext nicht frei. file

  Lancelle, Daniel and Bozic, Ognjan and Köke, Hardy (2013) Flight Test Results of Investigation of Acceleration Effects on a Gun Launched Rocket Engine. IEEE Transactions on Plasma Science, 41 (5), pp. 1-6. IEEE Nuclear and Plasma Sciences Society. ISBN 978-1-4673-0306-4. ISSN 0093-3813. Volltext nicht frei. file

  Langener, Tobias and Steelan, Johan and Karl, Sebastian and Hannemann, Klaus (2012) Design and Optimization of a Small Scale M=8 Scramjet Propulsion System. Space Propulsion 2012, 07. - 10. Mai 2012, Bordeaux, Frankreich. Volltext nicht online.

  Laurence, Stuart and Deiterding, Ralf (2010) Shock-wave surfing and the separation of meteoroid fragments in the atmosphere. 63rd Meeting of the APS Division of Fluid Dynamics, 21.-23. Nov. 2010, Long Beach, USA. Volltext nicht online.

  Laurence, Stuart and Karl, Sebastian and Martinez Schramm, Jan and Hannemann, Klaus (2013) Transient Fluid-Combustion Phenomena in a Model Scramjet. Journal of Fluid Mechanics, Vol. 722, pp. 85-120. Cambridge Universita Press. DOI: 10.1017/jfm.2013.56. ISSN 0022-1120. file

  Laurence, Stuart and Martinez Schramm, Jan (2010) High precision image-based tracking of a rigid body moving within a fluid. 63rd Annual Meeting of the APS Division of Fluid Dynamics, 21.-23. Nov. 2010, Long Beach, USA. file

  Laurence, Stuart and Martinez Schramm, Jan and Hannemann, Klaus (2012) Force and Moment Measurements on a Free-Flying Capsule Model in a High-Enthalpy Shock Tunnel. 28th Aerodynamic Measurement Technology,Ground Testing, and Flight Testing Conference, 25. - 28. Jun. 2012, New Orleans, Louisiana, USA. file

  Laurence, Stuart and Martinez Schramm, Jan and Karl, Sebastian and Hannemann, Klaus (2011) An Experimental Investigation of Steady and Unsteady Combustion Phenomena in the HyShot II Combustor. 17th International Space Planes and Hypersonics Systems and Technologies Conference, 11. - 14. April 2011, San Fransisco, USA. file

  Laurence, Stuart and Martinez Schramm, Jan and Karl, Sebastian and Hannemann, Klaus (2011) Ground-Based Testing of The Hyshot II Combustor Using OH Chemiluminescence. 7th European Symposium on Aerothermodynamics for Space Vehicles, 09. Mai - 12. Mai 2011, Brügge, Belgien. Volltext nicht online.

  Laurence, Stuart J and Karl, Sebastian (2010) An improved visualization-based force-measurement technique for short-duration hypersonic facilities. Experiments in Fluids, Vol. 48 (6), pp. 949-965. Springer Verlag Berlin, Heidelberg. DOI: 10.1007/s00348-009-0780-9. ISSN 0723-4864 (Print), 1432-1114 (Online). Volltext nicht online.

  Laurence, Stuart (2012) On tracking the motion of rigid bodies through edge detection and least-squares fitting. Experiments in Fluids, Vol. 5 (2), pp. 387-401. Springer Verlag. DOI: 10.1007/s00348-011-1228-6. ISSN 0723-4864 (Print), 1432-1114 (electronic Version). file

  Laurence, Stuart and Deiterding, Ralf (2011) Shock-wave surfing. Journal of Fluid Mechanics, pp. 1-36. Cambrigde University Press. DOI: 10.1017/S0022112011000577. file

  Laurence, Stuart and Karl, Sebastian and Hannemann, Klaus (2013) Experimental and numerical investigation of the HyShot II flight experiment. 29th International Symposium on Shock Waves (ISSW 29), 14. -19. July 2013, Madison, Wi, USA. Volltext nicht online.

  Laurence, Stuart and Ozawa, Hiroshi and Lieber, Damien and Martinez Schramm, Jan and Hannemann, Klaus (2012) Investigation of Unsteady/Quasi-Steady Scramjet Behavior using High-Speed Visualization Techniques. 18th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 24. - 28. Sept. 2012, Tours, France. DOI: 10.2514/6.2012-5913. file

  Laurence, Stuart and Parziale, N. J. and Deiterding, R. (2012) Dynamical separation of spherical bodies in supersonic flow. Journal of Fluid Mechanics, Vol. 7 (Decemb), pp. 159-182. Cambridge University Press. DOI: 10.1017/jfm.2012.453. filefile

  Laurence, Stuart and Wagner, Alexander and Hannemann, Klaus (2013) Investigation of hypersonic boundary-layer transition using high speed visualization techniques. 29th International Symposium on Shock Waves (ISSW 29), 14. -19. July 2013, Madison, Wi, USA. Volltext nicht online.

  Laurence, Stuart and Wagner, Alexander and Hannemann, Klaus and Wartemann, Viola and Lüdeke, Heinrich and Tanno, Hideyuki and Itoh, Katsuhiro (2012) Time-Resolved Visualization of Instability Waves in a Hypersonic Boundary Layer. AIAA Journal, Vol. 5 (1), pp. 243-246. The American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.J051112. filefile

  Laurence, Stuart and Wagner, Alexander and Ozawa, Hiroshi and Hannemann, Klaus (2014) Visualization of a hypersonic boundary layer on a transition cone. American Institute of Aeronautics and Astronautics. AIAA Aviation Technology, Integration, and Operations Conference, 16. – 20. June 2014, Atlanta, GA, USA. Volltext nicht online.

  Lehmann, Pascale and Bozic, Ognjan and Grobusch, H. and Behrens, Jörg (2007) Electromagnetic Railgun Technology for the Deployment of Small Sub- /Orbital Payloads. In: Proceedings CD/ Band 2007 (Paper ). 7th International Symposium on Launcher Technologies - Opening New Ways to Space Prospective, 2007-04-02 - 2007-04-05, Barcelona, Spain. (In Press) Volltext nicht frei. file

  Lerpe, Alexander (2007) Implementierung einer Software für die Messdatenauswertung der Versuchsanlage CCG/STG und ihre Integration in die Datenmanagementinfrastruktur. Diploma, Berufsakademie Mannheim. Volltext nicht frei. file

  Li, Yi and Eggers, Thino and Reimann, Bodo (2012) A Dynamics Study for the Hot Stage Separation of a Multistage Rocket with a Coupled CFD Flight Mechanics Approach. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, 24. - 28. Sep. 2012, Tours, Frankreich. Volltext nicht online.

  Li, Yi and Reimann, Bodo and Eggers, Thino (2013) Numerical investigations on the aerodynamics of Shefex-III Launcher. 64th International Astronautical Congress, Beijing, China, 23.-27. Okt. 2013, Beijing, China. Volltext nicht online.

  Li, Yi and Reimann, Bodo and Eggers, Thino (2014) Numerical investigations on the aerodynamics of SHEFEX-III launcher. Acta Astronautica (97), pp. 99-108. Elsevier Ltd.. ISSN 0094-5765. Volltext nicht frei. file

  Li, Yi and Reimann, Bodo and Eggers, Thino (2014) Coupled Simulation of CFD and Flight Mechanics with a Two-Species-Gas-Model for the Hot Staging of a Multistage Rocket. 19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 16-20 June 2014, Atlanta, GA. Volltext nicht online.

  Longo, J.M.A. and Dittrich, R. and Banuti, D. and Sippel, M. and Klevanski, J. and Atanassov, U. and Carrier, G. and Duveau, Ph. and Salah El Din, I. and Thepot, R. and Loubeau, A. and Coulouvrat, F. and Jarlas, R. and Rabia, H. and Perigo, D. and Steelant, J. (2009) Concept Study for a Mach 6 Transport Aircraft. 47th AIAA Aerospace Sciences Meeting, 2009-01-05 - 2009-01-08, Orlando, Florida (USA). file

  Longo, J.M.A. and Hannemann, K. and Hannemann, V. (2007) The Challenge of Modeling High Speed Flows. ISBN 978-3-901608-32-2. file

  Longo, Jose Maria and Barth, Tarik and Eggers, Thino (2008) Aerothermodynamics issues of the DLR hypersonic flight experiment SHEFEX-I. 38th Fluid Dynamic Conference & Exhibits, 2008-06, Seattle (USA). file

  Longo, Jose Maria and Hannemann, Klaus (2008) Technological Step Stones in Support to Future Space Transportation Systems. 2nd International ARA Days, 2008-10-21 - 2008-10-23, Arcachon (France). file

  Longo, José Maria and Reimann, Bodo and Strom, Silvia and Radespiel, Rolf and Esdorf, Malte and Wolf, Torsten (2008) ELEVON-ELEVON GAP FLOW IMPINGEMENT. 6th European Symposium on Aerothermodynamics for Space Vehicles, 2008-11-03 - 2008-11-06, Versailles (France). file

  Longo, José Maria and Turner, John and Weihs, Hendrik (2008) SHEFEX II - Aerodynamic Re-Entry Controlled Sharp Edge Flight Experiment. 6th European Symposium on Aerothermodynamics for Space Vehicles, 2008-11-03 - 2008-11-06, Versailles (France). file

  Lüdeke, H. (2009) CFD investigations of Axi-symmetric steady state nozzle plume flow for the Volvo S6 and Vulcain2 nozzle. DLR-Interner Bericht. 124-2009/913, 25 S. Volltext nicht online.

  Lüdeke, Heinrich (2005) Simulation of the Ariane-5 Nozzle Section by DES. In: Proceedings of the European Conference for Aerospace Sciences (EUCASS). European Conference for Aerospace Scinece (EUCASS), 2005-07-04 - 2005-07-07, Moscow, Russia. Volltext nicht frei. file

  Lüdeke, Heinrich and Calvo, Javier B. (2010) A Fluid Structure Coupling of the Ariane-5 Nozzle Section During Start Phase by Detached Eddy Simulation. CEAS Space Journal, 1 (1). Council of European Aerospace Societies. DOI: 10.1007/s12567-010-0002-6. Volltext nicht online.

  Lüdeke, Heinrich and Mulot, Jean (2012) Simulation of Unsteady, Turbulent Base Flow for Ariane-5 Wind Tunnel Configurations by Detached Eddy Simulation. DLR-Interner Bericht. Volltext nicht online.

  Lüdeke, Heinrich and Neil D., Sandham (2010) Direct Numerical Simulation of the Transition Process in a Separated Supersonic Ramp Flow. 40th AIAA Fluid Dynamics Conferenece and Exhibit 2010, 28 June - 1 July 2010, Chicago, IL, USA. Volltext nicht online.

  Lüdeke, Heinrich and Viola, Wartemann (2011) DNS of Mack-Mode Damping on Porous Coated Cones. 4th European Conference for Aerospace Sciences, 4.-8. Jul. 2011, St. Petersburg, Russland. Volltext nicht online.

  Lüdeke, Heinrich and Viola, Wartemann (2013) DNS of Mack-Mode Damping on Porous Coated Cones. In: Progress in Flight Physics Eucass Book Series, Vol. 5. Torus Press. pp. 57-68. ISBN 978-2-7598-0877-9. Volltext nicht online.

  Lüdeke, H. and Oswald, J. and Longo, J.M.A. and Thivet, F. and Hylkema, J. and Spel, M. and Dieudonne, W. (2005) DLR-ONERA accurate CFD support for the Pre-X project. In: Proceedings of the 6th Launcher Symposium, Munich, Germany. 6th International Symposium on Launcher Technologies, 2005-11-8.-11., Munich, Germany. file

  Lüdeke, H. and Sandham, N.D. (2009) Calculations of Shock-Boundary Layer Interaction for a Supersonic Ramp Flow by DNS, Using a Fourth order Finite Difference Method. DLR-Interner Bericht. 124-2009/9, 35 S. file

  Lüdeke, Heinrich (2005) Investigation of Unsteady Loads due to Turbulent Supersonic Wake Flow. In: Proceedings of the RTO AVT-123 Syposium: Flow Induced Unsteady Loads and the Impact on Military Applications. RTO AVT-123 Syposium: Flow Induced Unsteady Loads and the Impact on Military Applications, 2005-04-25 - 2005-04-28, Budapest. file

  Lüdeke, Heinrich (2005) Detached Eddy Simulation of the Ariane-5 Buffeting Coupling Phenomenon. In: Proceedings of the 6th International Symposium on Launcher Technologies. 6th international Symposium on Launcher Technologies, 2005-11-08 - 2005-11-11, Munich, Germany. Volltext nicht frei. file

  Lüdeke, Heinrich (2007) AXISYMMTERIC INVESTIGATION OF THE VAC S6 SHORT NOZZLE WITH FORCED EXTERNAL FLUCTUATION. In: Proceedings of the ATAC-FSCD WORKSHOP « AFTER-BODY AND NOZZLE FLOWS » November 15-16 at ESA/Estec, Noordwijk, The Netherlands. ATAC-FSCD WORKSHOP: « AFTER-BODY AND NOZZLE FLOWS », 2006-11-15 - 2006-11-16, ESA/Estec, Noordwijk, The Netherlands. (In Press) file

  Lüdeke, Heinrich (2007) UNSTEADY INVESTIGATION OF THE DLR TIC NOZZLE BY DIFFERENT TURBULENCE MODELS. In: Proceedings of the ATAC-FSCD WORKSHOP « AFTER-BODY AND NOZZLE FLOWS » November 15-16 at ESA/Estec, Noordwijk, The Netherlands. ATAC-FSCD WORKSHOP: « AFTER-BODY AND NOZZLE FLOWS », 2006-11-15 - 2006-11-16, ESA/Estec, Noordwijk, The Netherlands. (In Press) file

  Lüdeke, Heinrich and Calvo, Javier B. (2011) A Fluid Structure Coupling of the Ariane-5 Nozzle Section During Start Phase by Detached Eddy Simulation. CEAS Space Journal, 1 (1), pp. 33-44. Council of European Aerospace Societies. DOI: 10.1007/s12567-010-0002-6. Volltext nicht frei. file

  Lüdeke, Heinrich and Calvo, Javier B. and Filimon, Alexander (2006) Fluid Structure Interaction at the ARIANE-5 Nozzle section by Advanced Turbulence Models. In: Proceedings of the European Conference on Computational Fluid Dynamics. European Conference on Computational Fluid Dynamics, 2006-09-05 - 2006-09-08, Egmond aan Zee, The Netherlands. Volltext nicht frei. file

  Lüdeke, Heinrich and Calvo, Javier, B. (2008) A Fluid Structure Coupling of the Ariane-5 During Start Phase by DES. 6th European Symposium on Aerothermodynamics for Space Vehicles, 3.-6. Nov. 2008, Versailles, France. file

  Lüdeke, Heinrich and Sandham, Neil (2010) Direct Numerical Simulation of the Transition Process in a Separated Supersonic Ramp Flow. 40th AIAA Fluid Dynamics Conferenece and Exhibit 2010, 28 June - 1 July 2010, Chicago, IL, USA. Volltext nicht frei. file

  Lüdeke, Heinrich and Sandham, Neil D. and Wartemann, Viola (2010) Numerical Investigation of Transition Control by Porous Surfaces in Hypersonic Boundary Layers. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design New Results in Numerical and Experimental Fluid Mechanics VII, Vol. 1. Springer Verlag, Berlin-Heidelberg-New York. pp. 289-296. ISBN 978-3-642-14242-0. ISSN 1612-2909 file

  Lüdeke, Heinrich and Togiti, Vamshi (2006) Detached Eddy Simulation of Supersonic Shear Layer Wake Flows. In: Int. Conference on Boundary and Interior Layers. Int. Conference on Boundary and Interior Layers, 2006-07-24 - 2006-07-28, Göttingen, Germany. file

  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, Vol. 1. Springer Verlag. pp. 227-234. ISBN 978-3-642-35679-7. ISSN 1612-2909 file

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  Mack, Andreas and Steelant, Johan and Hannemann, Klaus (2009) Extrapolation of a generic scramjet model to flight scale by experiments, flight data and CFD. In: Shock Waves Springer. pp. 619-624. ISBN 978-3-540-85182-0. Volltext nicht online.

  Mack, Andreas and Steelant, Johan and Martinez Schramm, Jan and Hannemann, Klaus (2007) Sensitivity Analysis for the HyShot Generic Supersonic Combustion Configuration using CFD. In: Proceedings of XVIII Symposium on Air Breathing Engines. XVIII International Symposium on Airbreathing Engines (ISABE), 2007-09-02 - 2007-09-07, Peking, (China). Volltext nicht online.

  Marineau, Eric C. and Laurence, Stuart J. and Hornung, Hans G. (2011) Apollo-Shaped Capsule Boundary Layer Transition at High-Enthalpy in T5. In: AIAA conference proceedings on disc, Vol. 15, No. 1 (ASM). 48th AIAA Aerospace Sciences Meeting , 04.-07. Januar 2010, Orlando, USA. ISBN 1600867391. Volltext nicht online.

  Martinez Schram, Jan and Wagner, Alexander and Wolfram, Jeremy and Hannemann, Klaus and Barth, Tarik and Mulot, Jean-Daniel (2009) Post Flight Experiments of the SHEFEX I Configuration in the High Enthalpy Shock Tunnel Göttingen (HEG). 27th International Symposium on Shock Waves, 19.-24. Juli 2009, St. Petersburg. (Unpublished) Volltext nicht online.

  Martinez Schramm, Jan (2005) Experimental and numerical investigation of high enthalpy flow past a cylinder in HEG. In: ESA Scientific Publications. 5th European Symposium on Aerothermodynamics for Space Vehicles, Köln, 08.11.04-11.11.04, 2004-11-04 - 2004-11-11, Köln. ISBN 92-9092-874-3. ISSN 1609-042X Volltext nicht online.

  Martinez Schramm, Jan (2008) Aerothermodynamic Study of a Generic Flap Configuration with Slit in the High Enthalpy Shock Tunnel Göttingen (HEG). Sixth European Symposium on Aerothermodynamics for Space Vehicles, 2008-11-3 - 2008-11-6, Versailles, Frankreich. (In Press) Volltext nicht online.

  Martinez Schramm, Jan and Boutry, Amaury and Vital Durand, Matthieu (2004) Time Resolved Holographic Interferometry for Short Duration Hypersonic High Enthalpy Test Facilities. 24th International Symposium on Shock Waves, 2004-07-11 - 2004-07-16, Beijing, CHINA. ISBN 3-540-22497-1. Volltext nicht online.

  Martinez Schramm, Jan and Karl, Sebastian and Hannemann, Klaus and Steelant, Johan (2008) Ground testing of the HyShot II Scramjet Configuration in HEG. 15th AIAA Int. Space Planes and Hypersonic Systems and Technology Conference, 2008-04-28 - 2008-05-01, Dayton, OH (USA). Volltext nicht online.

  Martinez Schramm, Jan and Reimann, Bodo (2006) Aerothermodynamic Investigation of the Pre-X Configuration in HEG. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design Notes, Vol. 96. Springer Verlag Berlin, Heidelberg, New York. pp. 284-290. ISBN 978-3-540-74458-0. Volltext nicht online.

  Martinez Schramm, Jan and Sunami, Tesuji and Itoh, Katsuhiro and Hannemann, Klaus (2010) Experimental Investigation of Supersonic Combustion in the HIEST and HEG Free Piston Driven Shock Tunnels. 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 25.-28. Juli 2010, Nashville, USA. ISBN 978-1-60086-747-7. Volltext nicht online.

  Martinez Schramm, Jan and Wagner, Alexander and Reimann, Bodo and Fertig, Markus and Viguier, Paul and Verant, Jean-Luc (2011) Measurements on the EXOMARS Configuration in the High Enthalpy Shock Tunnel Göttingen (HEG). 7th European Symposium on Aerothermodynamics for Space Vehicles, 9. Mai - 12. Mai 2011, Brugge, Belgien. Volltext nicht online.

  Martinez Schramm, Jan and Wagner, Alexander and Wolfram, Jeremy and Hannemann, Klaus and Barth, Tarik and Mulot, Jean-Daniel and Schröder, Andreas (2009) Post flight analysis of SHEFEX I: Shock tunnel testing and related CFD analysis. 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 19. - 22. Okt. 2009, Bremen, Germany. DOI: 10.2514/6.2009-7216. ISBN 978-1-60086-968-6. Volltext nicht frei. file

  May, Stefan (2011) Wasserstoffperoxid-Katalysatorkammer eines Hybridraketentriebwerks. Bachelor's. Volltext nicht online.

  May, Stefan (2013) Mathematical Modeling of a High Test Peroxide Catalyst Chamber for Hybrid Rocket Engines. ODAS 2013, 13th ONERA-DLR Aerospace Syposium , 27.-29. Mai 2013, Palaiseau, Frankreich. Volltext nicht online.

  May, Stefan (2014) Numerische Simulation der Strömung und Verbrennung in der Brennkammer des AHRES-Hybridraketentriebwerks. Master's, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR). Volltext nicht online.

  Miermeister, Iko (2013) Aerodynamische Untersuchung eines Flugkörpers im Übergangsbereich von freier Molekülströmung und Kontinuumsströmung. Diploma, Technische Universität Carolo-Wilhelmina zu Braunschweig. Volltext nicht online.

  Mundt, Christian and Boyce, Russell and Jacobs, Peter and Hannemann, Klaus (2006) VALIDATION STUDY OF NUMERICAL SIMULATIONS BY COMPARISON TO MEASUREMENTS IN PISTON-DRIVEN SHOCK-TUNNELS. Aerospace Science and Technology, Volume 11 (Issues 2-3), pp. 100-109. Elsevier. Volltext nicht online.

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  Neoding, Peter and Martinez Schramm, Jan (2014) Numerical Rebuilding of Shock Tube Experiments in CO2 Flow under Conditions Relevant for Mars Entry Probes. American Institute of Aeronautics and Astronautics. 44th AIAA Fluid Dynamics Conference, 16. - 20. June 2014, Atlanta, GA, USA. Volltext nicht online.

  Neumann, Andreas (2012) DLR’s Test Facility STG-ET. 4th Russian-German Electric Propulsion Conference, 25. - 30. Juni 2012, Moskau, Russland. Volltext nicht online.

  Neumann, Andreas (2013) DLR's Test Facility STG-ET. Trudy MAI (original: Труды МАИ), Vol. 60, pp. 1-8. Moskauer Staatliches Luftfahrt-Institut (nationale Forschungsuniversität). Volltext nicht online.

  Neumann, Andreas (2013) EP Testanlage in Göttingen: Messungen am RIT. Workshop "Oberflächentechnologie mit Plasma- und Ionenstrahlprozessen", 05. - 08. März 2013, Mühlleithen. Volltext nicht online.

  Neumann, Andreas and Holz, André and Dettleff, Georg and Hannemann, Klaus and Harmann, Hans-Peter (2011) The New DLR High Vacuum Test Facility STG-ET. In: Konferenz Tagungsband (IEPC-2011-093). Universität Gießen. 32nd International Electric Propulsion Conference, IEPC 2011, 11.-15. Sept. 2011, Wiesbaden, Germany. Volltext nicht frei. file

  Neumann, Andreas and Sinske, Julian and Harmann, Hans-Peter (2013) The 250mN Thrust Balance for the DLR Goettingen EP Test Facility. 33rd International Electric Propulsion Conference (IEPC2013), 6. Okt. - 10. Okt. 2013, Washington DC, USA. Volltext nicht online.

  Neumann, Rudolf (2011) Modellierung von turbulenten Verbrennungsprozessen in Scramjet-Brennkammern. Diploma, Universität Kassel. Volltext nicht online.

O

  Odam, Judith and Paull, Allan (2006) Radical Farming in Scramjets. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design Notes, Vol. 96. Springer Verlag Berlin, Heidelberg, New York. pp. 276-283. ISBN 978-3-540-74458-0. Volltext nicht online.

  Ozawa, Hiroshi and Laurence, Stuart and Wagner, Alexander and Martinez Schramm, Jan and Hannemann, Klaus (2012) TSP Development for the High Enthalpy Shock Tunnel Göttingen (HEG). Deutsch/Japanischer Workshop "Leuchten in der Aerodynamik", 03. - 05. Sept. 2012, Chofu (Tokio), Japan. Volltext nicht frei. file

  Oßwald, Kai and Hannemann, Volker and Hannemann, Klaus and Stephan, Sören and Radespiel, Rolf (2013) Numerical and Experimental Investigations of a Generic Rocket Launcher Configuration with Cold Plume in Hypersonic Flow. In: Proceedings of the 5th European Conference for Aerospace Sciences (p95), pp. 1-12. 5th European Conference for Aerospace Sciences (EUCASS), 01. - 05. Juli 2013, München, Germany. file

  Oßwald, Kai and Hannemann, Volker and Birken, Philipp (2013) Implementing a time-accurate implicit-explicit method with error estimation for compressible flow. 2nd TRR40 Summer Research Program, 09. Aug. 2013, Munich, Germany. Volltext nicht frei. file

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  Palma, Phillip C. and Gardner, Anthony Donald and Beck, Walter H. (2002) Freestream Velocity in a Shock-Tunnel Nozzle Flow using Diode Laser Absorption Spectroscopy. 3rd Australian Conference on Laser Diagnostics in Fluid Mechanics and Combustion, Dec. 2-3, 2002, Brisbane, Australia. Volltext nicht online.

  Pegemanyfar, Nima (2003) Optische Messung der Wandtemperatur in einer H2/O2-keramischen Raketenbrennkammer. Other, Universität Stuttgart. Volltext nicht online.

  Philipp, Florian (2010) Semantische Analyse und automatische Taskparallelisierung einer domänenspezifischen Sprache zur Messdatenverarbeitung. Bachelor's, Duale Hochschule Baden-Württemberg Mannheim. Volltext nicht frei. file

  Poppe, Georg and Bozic, Ognjan (2013) Charakterisierung der Innenballistik und der Wärmeübertragung in der Brennkammer von Feststoff- und Hybridraketentriebwerken. 16. STAB-Workshop, 12.-13. Nov. 2013, Göttingen, Deutschland. Volltext nicht frei. file

  Porrmann, Dennis (2009) Vorentwurf und Numerische Simulation der Pilzdüse eines Chemischen Hybridtriebwerks unter Flugbedingungen. Diploma, Technische Universität Braunschweig. Volltext nicht online.

  Porrmann, Dennis and May, Stefan and Bozic, Ognjan and Lancelle, Daniel (2013) REGRESSION RATE MODELS VERSUS EXPERIMENTAL RESULTS FOR HYBRID ROCKET ENGINES BASED ON H2O2 AND HTPB/AL. IAC 2013, 23.-27. Sep. 2013, Peking, China. Volltext nicht frei. file

  Potter, Daniel (2012) "Numerical prediction of nonequilibrium radiative emission from shock heated CO2-N2". 5th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry , 15. Okt. - 18. Okt. 2012, Barcelona, Spanien. Volltext nicht online.

  Potter, Daniel and Karl, Sebastian and Lambert, Markus (2012) Simulation of a Mars aerocapture vehicle on flow adapted unstructured grids with the DLR TAU code. 5th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry, 15. Okt. - 18. Okt. 2012, Barcelona, Spanien. Volltext nicht online.

  Potter, Daniel and Karl, Sebastian and Lambert, Markus (2012) Numerical rebuilding of Viking afterbody radiative heating with the DLR TAU code. 5th International Workshop on Radiation of High Temperature Gases in Atmospheric Entry , 15. - 18. Okt. 2012, Barcelona, Spanien. ISBN 978-92-9092-278-0. ISSN 1609-042X Volltext nicht online.

  Potter, Daniel and Karl, Sebastian and Lambert, Markus and Hannemann, Klaus (2014) Computation of radiative and convective contributions to Viking afterbody heating. 44th AIAA Thermophysics Conference, 24. - 27. June 2013, San Diego, USA. Volltext nicht online.

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  Raddatz, J. and Dittrich, R. and Korfanty, M. and Longo, J.M.A. (2007) Project PRE-X Phase B DLR Contribution to Damping Coefficients Assessment. DLR-Interner Bericht. DLR-IB 124-2006/914. Volltext nicht online.

  Razzaqi, S. A. and Bode, C. and Eggers, Thino and Smart, Michael K. (2012) Development of Functional Relationships for Air-Data Estimation using Numerical Simulations. 18th Australasian Fluid Machanics Conference, 3-7 December 2012, Launceston, Australia. Volltext nicht frei. file

  Reimann, Bodo (2006) DLR contribution to the FLPP IXV aeroshape. DLR-Interner Bericht. DLR-IB 124-2006/909. Volltext nicht online.

  Reimann, Bodo and Hannemann, Volker (2010) Numerical Investigation of Double-Cone and Cylinder Experiments in High Enthalpy Flows using the DLR TAU code. 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 04.-07. January 2010, Orlando, USA. ISBN 978-1600-86739-2. Volltext nicht online.

  Reimann, Bodo and Hannemann, Volker and Hannemann, Klaus (2008) Computations of shock wave propagation with local mesh adaptation. 26th International Symposium on Shock Waves, 2007-07-15 - 2007-07-20, Göttingen (D). Volltext nicht online.

  Reimann, Bodo and Hannemann, Volker and Hannemann, Klaus (2009) Computations of shock wave propagation with local mesh adaptation. In: Shock Waves Springer. pp. 1383-1388. ISBN 978-3-540-85182-0. Volltext nicht online.

  Reimann, Bodo and Johnston, Ian and Hannemann, Volker (2003) DLR τ-Code for High Enthalpy Flows. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 87. Springer. Volltext nicht online.

  Reimann, Bodo and Martinez Schramm, Jan (2006) Aerodynamic and Aerothermodynamic Shape Characterisation of a Re-entry Demonstrator. The 1st International ARA Days, Atmospheric Reentry Sytems, Missions and Vehicles, 2006-07-03 - 2006-07-05, Arcachon (France). Volltext nicht online.

  Reimann, Bodo and Martinez Schramm, Jan (2007) Numerical and Experimental Investigation of a Hypersonic Glider. 37th AIAA Fluid Dynamics Conference and Exhibit, 2007-06-25 - 2007-06-28, Miami, FL (USA). Volltext nicht online.

  Reinke, Nico (2009) Numerische Analyse kompressibler turbulenter Strömungsfelder. Diploma, Georg August Universität Göttingen. 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.

  Robinson, Matthew (2005) Development and Testing of a New Three Component Short Duration Internal Force Balance for HEG. In: Proceedings. 5th European Symposium on Aerothermodynamics for Space Vehicles, 2004-11-08 - 2004-11-11, Köln. Volltext nicht online.

  Robinson, Matthew (2005) An internal stress wave force balance for use in a shock tunnel. In: Conference Proceedings. 21st International Congress on Instrumentation in Aerospace Simulation Facilities, 2005-08-29 - 2005-09-01, Sendai, Japan. Volltext nicht online.

  Robinson, Matthew and Hannemann, Klaus (2006) Short duration force measurements in impulse facilities. In: AIAA Conference Proceedings (AIAA-2006-3439), p. 15. American Institute of Aeronautics and Astronautics. 25th AIAA Aerodynamic Measurement Technology and Ground Testing, 2006-06-05 - 2006-06-08, San Francisco, CA (USA). Volltext nicht online.

  Robinson, Matthew and Martinez Schramm, Jan and Hannemann, Klaus (2006) An investigation into internal and external force balance configurations for short duration wind tunnels. In: Notes on Numerical Fluid Mechanics and Multidisciplinary Design Notes, Vol. 96. Springer Verlag Berlin, Heidelberg, New York. pp. 129-136. ISBN 978-3-540-74458-0. Volltext nicht online.

  Robinson, Matthew and Martinez Schramm, Jan and Hannemann, Klaus (2011) Design and implementation of an internal stress wave force balance in a shock tunnel. CEAS Space Journal, Vol. 1 (1-4), pp. 45-57. Springer Verlag Vienna. DOI: 10.1007/s12567-010-0003-5. ISSN 1868-2502. Volltext nicht online.

  Robinson, Matthew and Odam, Judith and Hannemann, Klaus (2006) LAPCAT Long-Term Advanced Propulsion Concepts and Technologies. Description of Model Geometry, Test Plan, Operating Conditions. Other. Volltext nicht online.

  Rochlitz, Henrik (2011) Verbrennungsinstabilitäten bei Hybridraketentriebwerken. Bachelor's, Technische Universität Braunschweig. Volltext nicht online.

  Rudolph, Martin (2013) Kopplung ABAQUS und TAU mit User Subroutinen. DLR-Interner Bericht, Project Report. DLR-IB 124-2013/902, 53 S. Volltext nicht frei. file

  Rutschmann, Sabrina and Martinez Schramm, Jan (2011) Stagnation-Point Heat Flux on Spheres in Hypersonic High Temperature Flows. STAB Workshop, 09. - 10. Nov. 2011, Göttingen, Deutschland. Volltext nicht frei. file

  Rutschmann, Sabrina (2009) Experimentelle Untersuchungen zur Anwendbarkeit einer Kraftmesstechnik basierend auf optischer Objektverfolgung in CCD-Kameraaufnahmen. Bachelor's, DLR Göttingen und Georg-August-Universität Göttingen. file

  Rutschmann, Sabrina (2011) Stagnation-Point Heat Flux on Spheres in Hypersonic High Temperature Flows. Master's, DLR Göttingen und Georg-August-Universität Göttingen. Volltext nicht frei. file

  Rutschmann, Sabrina and Martinez Schramm, Jan and Wolfram, Jeremy and Laurence, Stuart (2009) Untersuchungen einer Kraftmesstechnik basierend auf optischer Objektverfolgung. AG-STAB 2009, 11.-12.11.2009, Göttingen, Deutschland. file

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  Sandham, N.D. and Lüdeke, H. (2009) A numerical study of Mach 6 boundary layer stabilization by means of a porous surface. 47th AIAA Aerospace Sciences Meeting , 5.-8. Jan 2009, Orlando, Florida. Volltext nicht online.

  Sandham, N.D. and Lüdeke, H. (2009) Numerical Study of Mach 6 Boundary Layer Stabilization by Means of a Porous Surface. AIAA Journal, Vol. 4 (No. 9), pp. 2243-2252. Volltext nicht frei. file

  Sandham, Neil and Schülein, Erich and Wagner, Alexander and Willems, Sebastian and Stellant, Johan (2014) Transitional shock-wave/boundary-layer interactions in hypersonic flow. Journal of Fluid Mechanics, 752 (6), pp. 349-382. Cambridge University Press 2014. DOI: 10.1017/jfm.2014.333. ISSN 0022-1120. Volltext nicht online.

  Sarma, G. S. R. (2005) Electric Thruster Plume Characterization. DLR-Interner Bericht. DLR-IB 224-2004 A09, 88 S. Volltext nicht online.

  Schmidt, Moritz (2008) Konstruktion eines Magnetohydrodynamik-Windkanalmodells für den Hochenthalpiekanal Göttingen. Diploma, Hochschule für Angewandte Wissenschaft und Kunst Göttingen. Volltext nicht online.

  Schneider, Markus and Bozic, Ognjan and Eggers, Thino (2010) Some Aspects concerning the Design of Multistage Earth Orbit Launchers using Electromagnetic Acceleration. 15th Elektromagnetic Launch (EML) Symposium, 17. - 20. May, 2010 , Brussels, Belgium. Volltext nicht frei. file

  Schneider, Markus and Bozic, Ognjan and Eggers, Thino (2011) Some Aspects concerning the Design of Multistage Earth Orbit Launchers using Electromagnetic Acceleration. IEEE Transactions on Plasma Science, Vol. 39 (2), pp. 794-801. IEEE. DOI: 10.1109/TPS.2010.2091971. ISSN 0093-3813. Volltext nicht online.

  Schrijer, F.F.J. and Sciacchitano, A. and Scarano, Fluvio and Hannemann, Klaus and Pallegoix, Jean-Francois and Maseland, J.E.J. and Schwane, Richard (2011) Experimental Investigation of Base Flow Buffeting on the ARIANE 5 Launcher Using High Speed PIV. 7th European Symposium on Aerothermodynamics for Space Vehicles, 9.Mai - 12. Mai 2011, Brugge, Belgien. Volltext nicht online.

  Schulz, Oliver (2010) Beheizbare Modelle für den Einsatz am HEG. Bachelor's, Technische Universität Berlin / DLR. 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.

  Sinske, Julian (2013) Entwicklung und Erprobung einer Steuerungseinheit für ein Radiofrequenz-Ionentriebwerk. Master's. DLR-Interner Bericht. DLR-IB 224-2013 A 94, 93 S. Volltext nicht online.

  Sippel, Martin and Weihs, Hendrik and Barth, Tarik (2009) Systematic Assessment of Advanced "Sharp-Edged" Lifting Body Re-entry Configurations. 60th International Astronautical Congress (IAC), Okt. 2009, Daejeon, Republic of Korea. (Unpublished) Volltext nicht frei. file

  Starke, J. and Belmont, J.-P. and Longo, J. and Novelli, Ph. and Kordulla, W. (2008) Some Considerations on Suborbital Flight in Europe. 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2008-04, Dayton (USA). file

  Steelant, Johan and Mack, Andreas and Hannemann, Klaus and Gardner, Anthony (2006) Comparison of Supersonic Combustion Tests with Shock Tunnels Flight and CFD. In: AIAA Conference Proceedings, Session 60-HYP-3 (AIAA 2006-4684), p. 14. American Institute of Aeronautics and Astronautics. 42th AIAA Joint Propulsion Conference, 2006-07-09 - 2006-07-12, Sacramento, CA (USA). Volltext nicht online.

  Steelant, Johan and Mack, Andreas and Hannemann, Klaus and Gardner, Anthony Donald (2006) Comparison of supersonic combustion tests with shock tunnels, flight and CFD. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 9-12, 2006, Sacramento, California. Volltext nicht online.

  Stollmeier, Frank (2009) Rechengitter zur Teilchenverfolgung in DSMC-Strömungssimulationen. Bachelor's, Georg-August-Universität Göttingen. file

  Stollmeier, Frank and Grabe, Martin (2011) A Voronoi Grid and a Particle Tracking Algorithm for DSMC. AIP| Conference Proceedings|1333 (PART ONE). American Institute of Physics. ISBN 978-0-7354-0889-0. ISSN 0094-243X Volltext nicht online.

  Stollmeier, Frank and Grabe, Martin (2009) Rechengitter zur Teilchenverfolgung in DSMC-Strömungssimulationen. In: STAB Mitteilungen. 14. STAB-Workshop, 11-13 Nov 2009, Göttingen. file

  Stollmeier, Frank and Grabe, Martin (2011) A Voronoi Grid and a Particle Tracking Algorithm for DSMC. Rarefied Gas Dynamics: 27th International Symposium, 10. - 15. Jul. 2010, Monterey, USA. file

  Storch, David-Maximiliam and Steinmacher, Bermann and Martinez Schramm, Jan (2011) Calibration of ultra-fast thermocouples for heat-flux determination in the High Enthalpy Shock Tunnel Göttingen (HEG). STAB Workshop 2011, 9.-10. Nov. 2011, Göttingen, Deutschland. Volltext nicht online.

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  Tanno, Hideyuki and Komuro, Tomoyuki and Sato, Kazuo and Itoh, Katsuhiro and Takahashi, Masahiro and Fujita, Kazuhisa and Laurence, Stuart and Hannemann, Klaus (2012) Free-flight force measurement technique in a shock tunnel. 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, 09. - 12. Jan. 2012, Nashville, TN, USA. DOI: 10.2514/6.2012-1241. ISBN eISBN: 978-1-60086-936-5. file

  Tanno, Hideyuki and Sato, Kazuo and Komuro, Tomoyuki and Takahashi, Masahiro and Itoh, Katsuhiro and Fujita, Kazuhisa and Laurence, Stuart and Hannemann, Klaus (2011) Force Measurement Using Non-Restrained Models in a Shock Tunnel. 7th European Symposium on Aerothermodynamics for Space vehicles, 9. Mai - 12. Mai 2011, Brugge, Belgien. Volltext nicht online.

  Thees, Carsten (2009) Development and Optimization of a Two Wavelength Holographic Interferometer to Determine Electron Gas Densities for the HEG. Diploma, Georg-August-Universität Göttingen. Volltext nicht online.

  Togiti, Vamshi and Breuer, Michael and Longo, Jose' (2008) Influence of Boundary Layer on Supersonic Cavity Flow Dynamics. In: CD-ROM Proc. of the Sixth European Symp. of Aerothermodynamics for Space Vehicles. Sixth European Symp. of Aerothermodynamics for Space Vehicles, 3-5 Nov 2008, Versailles, France. Volltext nicht online.

  Togiti, Vamshi and Gruhn, Patrick and Longo, Jose (2008) A CFD Study on Interaction of the Single Expansion Ramp Nozzle Flow and the External Flow. In: Proceeedings of the 59th International Aeronautical conference (IAC). 59th International Astronautical Conference, Glasgow, Schottland. Volltext nicht online.

  Togiti, Vamshi and Breuer, Michael and Lüdeke, Heinrich (2010) Detached-Eddy and Delayed Detached-Eddy Simulation of Supersonic Flow over a Three-Dimensional Cavity. ERCOFTAC Series, Vol. 1 (8). Springer Verlag. ISBN 978-90-481-3651-3. Volltext nicht frei. file

  Traphan, Dominik (2011) Experimentelle Untersuchung von Freistrahlen aus geometrisch ähnlichen Düsen. Diploma, DLR. Volltext nicht online.

V

  Votta, Raffaele and Marini, Marco and Ranuzzi, Giuliano and Schlegat, Thomas and Hannemann, Klaus and Schwanekamp, Tobias and Sippel, Martin (2013) Rarefied Aerothermodynamics Technology Development for Future High-Altitude High-Speed Transport (EU-FAST20XX). AIAA SPACE 2013 Conference and Exposition, 10. - 12. Sept. 2013, San Diego, CA, USA. Volltext nicht online.

  Votta, Raffaele and Ranuzzi, Giuliano and Marini, Marco and Morsa, Luigi and Fels, Giorgio and Schlegat, Thomas and Hannemann, Klaus (2012) Numerical and Experimental Analysis of Low-Density Effects in Suborbital Flight of FAST20XX. 43rd AIAA Thermophysics Conference, 25.-28. Jun. 2012, New Orleans, Louisiana, USA. DOI: 10.2514/6.2012-3107. ISBN eISBN: 978-1-62410-186-1. Volltext nicht online.

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  Wagner, Alexander (2012) Title confidential. Other. DLR-Interner Bericht. DLR-IB 224-2012 C 116, 91 S. Volltext nicht online.

  Wagner, Alexander (2013) Laminar to Turbulent Transition in Hypersonic Flows: TN6000 Summary Report. DLR-Interner Bericht, Project Report. DLR-IB 224-2013 A 74, 51 S. Volltext nicht online.

  Wagner, Alexander (2013) Laminar to Turbulent Transition in Hypersonic Flows - TN6100 Executive Summary Report -. DLR-Interner Bericht, Project Report. DLR-IB 224-2013 A 80, 16 S. Volltext nicht online.

  Wagner, Alexander and Hannemann, Klaus (2012) Stabilization of a hypersonic boundary layer on a cone by means of ultrasonically absorptive carbon-carbon material. Seminar CALTECH, 20. Apr. 2012, Pasadena, California, USA. Volltext nicht online.

  Wagner, Alexander and Hannemann, Klaus and Eggers, Thino (2012) Recent Aerothermodynamic Studies in the High Enthalpy Shock Tunnel Göttingen (HEG). International Symposium on Hypersonic Aerothermodynamics - Recent Advances, 09. - 13. Dec. 2012, Bangalore, Indien. Volltext nicht frei. file

  Wagner, Alexander and Hannemann, Klaus and Wartemann, Viola and Tanno, Hideyuki and Ito, Katsuhiro (2012) Free piston driven shock tunnel hypersonic boundary layer transition experiments on a cone configuration. RTO-MP-AVT-200: Hypersonic Laminar-Turbulent Transition , 16. - 19. April 2012, San Diego, California, USA. Volltext nicht frei. file

  Wagner, Alexander and Johnstone, Emma and Parnaby, Garvin (2012) Hypersonic transition literature survey. DLR-Interner Bericht. DLR-IB 224–2012 A 70, 89 S. Volltext nicht frei. file

  Wagner, Alexander and Kuhn, Markus and Martinez Schramm, Jan and Hannemann, Klaus (2013) Experiments on passive hypersonic boundary layer control using ultrasonically absorptive carbon–carbon material with random microstructure. Experiments in Fluids, Vol. 54 (1606). Springer Verlag Berlin Heidelberg. DOI: 10.1007/s00348-013-1606-3. ISSN 0723-4864. Volltext nicht online.

  Wagner, Alexander and Laurence, Stuart and Martinez Schramm, Jan and Hannemann, Klaus and Wartemann, Viola and Lüdeke, Heinrich and Tanno, Hideyuki and Ito, Katsuhiro (2011) Experimental investigation of hypersonic boundary-layer transition on a cone model in the High Enthalpy Shock Tunnel (HEG) at Mach 7.5. Seminar, 19.04.2011, California Institute of Technology (Caltech), Los Angeles, Kalifornien. Volltext nicht online.

  Wagner, Alexander and Wartemann, Viola and Hannemann, Klaus and Eggers, Thino (2013) Experimental Investigations of Hypersonic Boundary-Layer Stabilization by means of Porous Surfaces. Texas A&M University Seminar, 11.01.2013, College Station, Texas, USA. Volltext nicht online.

  Wagner, Bernd and Karl, Sebastian and Hannemann, Klaus (2006) Test Case 1a: Short Nozzle Under Separated Flow Condition – Numerical Investigation with the DLR Tau-Code. In: Proceedings, FSCD-ATAC Workshop, p. 4. FSCD-ATAC Workshop, 2006-11-15 - 2006-11-16, Noordwijk, The Netherlands. Volltext nicht online.

  Wagner, Alexander and Hannemann, Klaus and Kuhn, Markus (2012) Experimental investigation of hypersonic boundary-layer stabilization on a cone by means of ultrasonically absorptive carbon-carbon material. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, 24. Sept. - 28. Sept. 2012, Tours, Frankreich. DOI: 10.2514/6.2012-5865. Volltext nicht frei. file

  Wagner, Alexander and Hannemann, Klaus and Kuhn, Markus (2014) Ultrasonic absorption characteristics of porous carbon–carbon ceramics with random microstructure for passive hypersonic boundary layer transition control. Experiments in Fluids, 55 (6), pp. 1-9. Springer Verlag, Berlin Heidelberg. DOI: 10.1007/s00348-014-1750-4. ISSN 0723-4864. Volltext nicht online.

  Wagner, Alexander and Laurence, Stuart and Martinez Schramm, Jan and Hannemann, Klaus and Wartemann, Viola and Lüdeke, Heinrich and Tanno, Hideyuki and Ito, Katsuhiro (2011) Experimental investigation of hypersonic boundary-layer transition on a cone model in the High Enthalpy Shock Tunnel (HEG) at Mach 7.5. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 11. - 14. Apr. 2011, San Francisco, USA. DOI: 10.2514/6.2011-2374. file

  Wagner, Alexander and Wartemann, Viola and Hannemann, Klaus (2013) Contributions to the AVT-### / RTG on HYPERSONIC BOUNDARY-LAYER TRANSITION PREDICTION. NATO AVT-ET-136 Hypersonic Boundary-Layer Transition Prediction, 09. - 10. Oct. 2013, Riga, Lettland. Volltext nicht online.

  Wagner, Alexander and Wartemann, Viola and Hannemann, Klaus and Giese, Tobias (2013) Hypersonic boundary-layer stabilization by means of ultrasonically absorptive carbon-carbon material, Part 1: Experimental Results. 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 07. - 10. Jan. 2013, Grapevine, Texas, USA. DOI: 10.2514/6.2013-270. Volltext nicht frei. file

  Wagner, Alexander and Wartemann, Viola and Kuhn, Markus and Martinez Schramm, Jan and Hannemann, Klaus (2013) Experimental investigation of hypersonic boundary layer transition delay by means of ultrasonically absorptive carbon-carbon material in the High Enthalpy Shock Tunnel G�öttingen (HEG). Lecture Series on high-speed laminar-turbulent transition, 30.-31.05.2013, Brüssel, Belgien. file

  Wartemann, Viola and Eggers, Thino and Wagner, Alexander and Hannemann, Klaus (2013) Numerical Investigations of Hypersonic Boundary-Layer Stabilization by means of Porous Surfaces. Seminar Texas A&M University, 11.01.2013, College Station, Texas. Volltext nicht online.

  Wartemann, Viola and Lüdeke , Heinrich and Sandham, Neil D. (2012) Numerical Investigation of Hypersonic Boundary-Layer Stabilization by Porous Surfaces. AIAA Journal, Vol. 50 (6), 1281-1290 . DOI: 10.2514/1.J051355. ISSN 0001-1452. Volltext nicht online.

  Wartemann, Viola and Willems, Sebastian and Gülhan, Ali (2012) Mack mode damping by micropores on a cone in hypersonic flow. RTO. Volltext nicht frei. file

  Wartemann, Viola (2014) Mack-Moden-Dämpfung mittels mikroporöser Oberflächen im Hyperschall. Dissertation. DLR-Forschungsbericht. DLR-FB 2014-19. Volltext nicht online.

  Wartemann, Viola and Eggers, Thino and Giese, Tobias and Wagner, Alexander and Hannemann, Klaus (2013) Hypersonic boundary-layer stabilization by means of ultrasonically absorptive carbon-carbon material - Part 2: Computational Analysis. 51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, 07. - 10. Jan. 2013, Grapevine, Texas. Volltext nicht frei. file

  Wartemann, Viola and Eggers, Thino and Wagner, Alexander and Giese, Tobias and Hannemann, Klaus (2013) Numerical investigations of hypersonic boundary layer stabilization by porous surfaces. VKI Lecture: High Speed Laminar - Turbulent Transition, 30 - 31 Mai, Brüssel, Belgien. Volltext nicht frei. file

  Wartemann, Viola and Heinrich, Lüdeke (2010) Numerical investigations of hypersonic boundary layer stabilisation by means of porous surfaces. STAB 2010. Geschäftsstelel der STAB, c/o Dr. H.-P. Kreplin, Bunsenstr. 10, 37073 Göttingen. (Unpublished) Volltext nicht frei. file

  Wartemann, Viola and Lüdeke, Heinrich (2010) Investigation of slip boundary conditions of hypersonic flow over microporous surfaces. V European Conference on Computational Fluid Dynamics - ECCOMAS CFD 2010, 14 - 17 June 2010, Lisbon, Portugal. Volltext nicht frei. file

  Wartemann, Viola and Lüdeke, Heinrich and Sandham, Neil D. (2009) Stability analysis of hypersonic boundary layer flow over microporous surfaces. 16th AIAA/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, 19 - 22 Dec 2009, Bremen, Germany. file

  Wartemann, Viola and Wagner, Alexander and Eggers, Thino and Hannemann, Klaus (2013) Experimental (HEG) and numerical investigations of hypersonic boundary-layer stabilization by means of porous surfaces, second-mode instability & transition, characterization of tunnel noise. STO Meeting: AVT - ET 136, College Station, Texas. Volltext nicht frei. file

  Wartemann, Viola and Wagner, Alexander and Giese, Tobias and Eggers, Thino and Hannemann, Klaus (2014) Boundary-layer stabilization by an ultrasonically absorptive material on a cone in hypersonic flow: numerical investigations. CEAS Space Journal, 6 (1), pp. 13-22. Springer. DOI: DOI 10.1007/s12567-013-0053-6. ISSN 1868-2502. Volltext nicht online.

  Wartemann, Viola and Lüdeke, Heinrich and Willems, Sebastian and Gülhan, Ali (2011) Stability analyses and validation of a porous surface boundary condition by hypersonic experiments on a cone model. 7th Aerothermodynamics Symposium, 9. - 12. Mai 2011, Brugge, Belgien. ISBN 978-92-9221-256-8. ISSN 1609-042X Volltext nicht frei. file

  Weking, Hendrik (2006) Aerodynamische und Thermodynamische Analyse der Hecksteuerklappe eines Wiedereintrittskörpers. Diploma, Universität Stuttgart. Volltext nicht online.

  Wennrich, Michèl (2011) Numerische Simulation generischer Körper in verdünnten Gasströmungen mit OpenFOAM. Other. Volltext nicht online.

  Wilken, Jascha (2014) Analyse von Ultraschallsignalen für die Regressionsmessung eines Hybridraketentriebwerkes. Other, Technische Universität Braunschweig. Volltext nicht online.

  Wolfram, Jeremy and Martinez Schramm, Jan (2008) Pattern Recognition in High Speed Schlieren Visualization at the High Enthalpy Shock Tunnel Göttingen (HEG). 16. DGLR/STAB Symposium, 2008-11-3 - 2008-11-04, Aachen. (Submitted) Volltext nicht online.

  Wolfram, Jeremy and Martinez Schramm, Jan (2010) Pattern Recognition in High Speed Schlieren Visualization at the High Enthalpy Shock Tunnel Göttingen (HEG). In: New Results in Numerical and Experimental Fluid Mechanics VII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, Vol. 112. Springer Verlag, Berlin Heidelberg. pp. 399-406. ISBN 978-3-642-14243-0. Volltext nicht online.

  Wolfram, Jeremy (2008) Bildanalyse zeitlich aufgelöster Sichtbarmachungen von Hochenthalpieströmungen in einer verteilten „Visual-Programming“-Umgebung. Master's, Universität Göttingen. Volltext nicht frei. file

  Wolfram, Jeremy (2004) Implementierung einer modularen Auswertesoftware für die Versuchsauswertung am Hochenthalpiekanal Göttingen. Diploma, Berufsakademie Mannheim. Volltext nicht frei. file

  Wollenhaupt, Birk (2007) Turbulenzmodellierung mit dem DLR TAU Verfahren. Diploma, Universität Stuttgart. Volltext nicht online.

  Wucherpfennig, Jens and Schröder, Andreas and Hannemann, Klaus and Martinez-Schramm, Jan (2009) Nie zuvor betrachtete Geschwindigkeiten. [Other] Volltext nicht online.

  Wucherpfennig, Jens and Schröder, Andreas and Hannemann, Klaus and Martinez-Schramm, Jan (2009) Sichtbarer Hyperschall. Mauritz&Grewe. [Other] Volltext nicht online.

  Wucherpfennig, Jens and Schröder, Andreas and Hannemann, Klaus and Martinez-Schramm, Jan (2009) Hyperschall sichtbar gemacht. [Other] Volltext nicht online.

  Wucherpfennig, Jens and Schröder, Andreas and Hannemann, Klaus and Martinez-Schramm, Jan (2009) Forscher machen Hyperschall sichtbar. Springer-Verlag Heidelberg. [Other] Volltext nicht online.

  Wucherpfennig, Jens and Schröder, Andreas and Hannemann, Klaus and Martinez-Schramm, Jan (2009) DLR-Forscher machen Hyperschall sichtbar. [Other] Volltext nicht online.

  Wucherpfennig, Jens and Schröder, Andreas and Martinez-Schramm, Jan (2009) DLR-Forscher machen Hyperschall sichtbar. [Other] Volltext nicht online.

  Wucherpfenning, Jens and Schröder, Andreas and Hannemann, Klaus and Martinez Schramm, Jan (2009) Hyperschallströmung mit der PIV-Methode sichtbar gemacht. [Other] Volltext nicht online.

Y

  You, Yancheng (2013) Laminar to Turbulent Transition in Hypersonic Flows: Extension of a RANS transition model for high speed flows (TN5200). DLR-Interner Bericht, Project Report. DLR-IB 224-2013 A 77, 51 S. Volltext nicht online.

  You, Yancheng and Buanga, Björn and Hannemann, Volker and Heinrich, Lüdeke (2012) Evaluation of Turbulence Models in Predicting Hypersonic and Subsonic Base Flows using Grid Adaptation Techniques. Chinese Journal of Aeronautics, Vol. 25 (3), pp. 325-334. Elsevier Limited. DOI: 10.1016/S1000-9361(11)60393-2. ISSN 1000-9361. Volltext nicht online.

  You, Yancheng and Luedeke, Heinrich and Hannemann, Klaus (2011) RANS and DES Mixing Layers Inverstigations with the DLR TAU code. Project Report. (Unpublished) Volltext nicht online.

  You, Yancheng and Luedeke, Heinrich and Hannemann, Klaus (2011) Numerical Study of Compressible Mixing Layers in Hyshot II Supersonic Combustor. SP-692. ESA Communications. ISBN 978-92-9221-256-8. ISSN 1609-042X Volltext nicht online.

  You, Yancheng and Lüdeke, Heinrich and Eggers, Thino and Hannemann, Klaus (2012) Application of the Re-theta Transition Model in High Speed Flows. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, 24. - 28. Sept. 2012, Tours, Frankreich. DOI: 10.2514/6.2012-5972. Volltext nicht online.

  You, Yancheng and Lüdeke, Heinrich and Hannemann, Klaus (2012) On the Flow Physics of a Low Momentum Flux Ratio Jet in a Supersonic Turbulence Crossflow. Europhysics Letters, Vol. 97 (2). IOPScience. DOI: 10.1209/0295-5075/97/24001. ISSN 0295-5075 . Volltext nicht online.

  You, Yancheng and Lüdeke, Heinrich and Hannemann, Klaus (2012) Injection and Mixing in a Scramjet Combustor: DES and RANS Studies. 34th International Symposium on Combustion, Warschau, Polen. Volltext nicht online.

  You, Yancheng and Oßwald, Kai and Lüdeke, Heinrich and Hannemann, Volker (2011) Numerical Investigation of a Generic Rocket Base Flows under Subsonic Conditions. In: Sonderforschungsbereich Transregio 40 - Jahresbericht 2010 Deutsche Forschungsgemeinschaft (DFG) Deutsche Forschungsgemeinschaft (DFG). Volltext nicht online.

  You, Yancheng and Oßwald, Kai and Lüdeke, Heinrich and Hannemann, Volker (2011) Numerical Study of the Subsonic Base Flow with a Side Support. Volltext nicht online.

  You, Yancheng and Oßwald, Kai and Hannemann, Volker (2012) Numerical Simulation of a Generic Rocket Base Flow with Plume in a Supersonic Environment. Project Report. Deutsche Forschungsgemeinschaft (DFG). Volltext nicht online.

  You, Yangcheng and Lüdeke, Heinrich and Hannemann, Klaus (2013) Injection and mixing in a scramjet combustor: DES and RANS studies. Proceedings of the Combustion Institute, Vol. 34 (2), pp. 2083-2092. Elsevier. DOI: 10.1016/j.proci.2012.10.001. ISSN 1540-7489. Volltext nicht online.

  You, Yancheng and Luedeke, Heinrich and Hannemann, Volker (2010) Detached Eddy Simulation of Base Flows under Subsonic Free Stream Conditions. Project Report. file

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