Source: https://elib.dlr.de/view/subjects/as-rf.html
Timestamp: 2019-04-25 10:57:20+00:00

Document:
electronic library - Items where Subject is "Institute of Aerodynamics and Flow Technology > Spacecraft"
Items where Subject is "Institute of Aerodynamics and Flow Technology > Spacecraft"
Alder, Marko (2015) Development and Validation of a Fluid–Structure Solver for Transonic Panel Flutter. AIAA Journal, 53 (12), pp. 3509-3521. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.J054013 ISSN 0001-1452 Volltext nicht frei.
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 (Unpublished) Volltext nicht online.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, 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 (2015) Crossing the Widom-line - supercritical pseudo-boiling. The Journal of Supercritical Fluids, 98 (03), pp. 12-16. Elsevier. DOI: 10.1016/j.supflu.2014.12.019 ISSN 0896-8446 Volltext nicht online.
Banuti, Daniel (2015) Thermodynamic Analysis and Numerical Modeling of Supercritical Injection. Dissertation, University of Stuttgart, Institute of Aerospace Thermodynamics. Volltext nicht online.
Banuti, Daniel and Grabe, Martin and Hannemann, Klaus (2014) Planar Micro Nozzles - CFD Model Demands for Thrust Optimization. Space Propulsion 2014, 19. - 22. May 2014, Cologne, Germany. Volltext nicht online.
Banuti, Daniel and Grabe, Martin and Hannemann, Klaus (2014) Flow Characteristics of Micro-Scale Planar Nozzles. American Institute of Aeronautics and Astronautics. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 28. - 30. July 2014, Cleveland, Ohio, USA. Volltext nicht online.
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.
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.
Banuti, Daniel and Hannemann, Klaus (2014) Efficient multiphase rocket propellant injection model with high quality equation of state. Space Propulsion 2014, 19. - 22. May 2014, Cologne, Germany. Volltext nicht online.
Banuti, Daniel and Hannemann, Klaus (2014) Supercritical Pseudo-Boiling and its Relevance for Transcritical Injection. American Institute of Aeronautics and Astronautics. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 28. - 30. July 2014, Cleveland, Ohio, USA. Volltext nicht online.
Banuti, Daniel and Hannemann, Klaus (2014) Application of a Real-Gas-Library Multi-Fluid-Mixing Model to Supercritical Single Injector Flow. American Institute of Aeronautics and Astronautics. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 28. - 30. July 2014, Cleveland, Ohio, USA. Volltext nicht online.
Banuti, Daniel and Hannemann, Klaus (2015) The absence of a dense potential core in transcritical injection. 15th International Conference on Numerical Combustion, 19. - 22. April 2015, Avignon, France. Volltext nicht online.
Banuti, Daniel and Hannemann, Klaus (2016) The absence of a dense potential core in supercritical Injection: A thermal break-up mechanism. Physics of Fluids, 28 (035103). American Institute of Physics (AIP). DOI: 10.1063/1.4943038 ISSN 1070-6631 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 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.
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: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 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.
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: New Results in Numerical and Experimental Fluid Mechanics VII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 112. Springer Verlag, Berlin Heidelberg. pp. 355-363. ISBN 978-3-642-14242-0. ISSN 1612-2909 Volltext nicht frei.
Barth, Tarik and Longo, Jose (2010) Advanced Flight Analysis of SHEFEX-I. In: New Results in Numerical and Experimental Fluid Mechanics VII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 112. Springer Verlag, Berlin Heidelberg. pp. 431-439. ISBN 978-3-642-14242-0. ISSN 1612-2909 Volltext nicht frei.
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.
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.
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. 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.
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.
Bartolome Calvo, Javier and Hannemann, Klaus (2010) Analysis of the Heat Transfer in Liquid Rocket Engine Cooling Channels. In: New Results in Numerical and Experimental Fluid Mechanics VII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 112. Springer-Verlag, Berlin Heidelberg. pp. 441-448. ISBN 978-3-642-14242-0. ISSN 1612-2909 Volltext nicht online.
Bartolome Calvo, Javier and Wolko, Stephan and Eggers, Thino (2010) Application of a Coupling of Aerodynamics and Flight Dynamics to Predict the SHEFEX I Ascent Phase. 17. DGLR / STAB Fachsymposium, 9.-10. Nov. 2010, Berlin, Deutschland. Volltext nicht online.
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).
Bengsch, Philipp (2015) Berechnung der Dämpfungsderivate eines Wiedereintrittskörpers durch Lösen zeitlinearisierter Strömungsgleichungen im Frequenzbereich. Master's, TU Hamburg-Harburg. Volltext nicht online.
Birkenkampf, Peter (2011) Systemtest der Implementierung einer domänenspezifischen Sprache zur Messdatenauswertung. Bachelor's, Duale Hochschule Baden-Württemberg. Volltext nicht frei.
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: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 121. Springer Verlag. pp. 101-108. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht frei.
Bode, Christoph and Eggers, Thino (2010) Numerical generation of a Flush Air Data System for the Hypersonic Flight Experimental HIFiRE 7. 17. DGLR / STAB Fachsymposium, 9.-10. Nov. 2010, Berlin, Deutschland. 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.
Boyer, Christian (2014) Entwicklung einer Aufnahmevorrichtung für eine Mikroschubwaage in Kryovakuumumgebung. Other. Studienarbeit R 1419 S, 76 S. 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.
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.
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.
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. Springer Verlag. (In Press) Volltext nicht online.
Bozic, Ognjan (2015) Stand der Technik und Perspektiven bei der Entwicklung von Feststoff und Hybridraketentriebwerken. DGLR Workshop „Feststoff- und Hybridraketentriebwerke – Aktueller Entwicklungsstand und Perspektiven“, 18. - 19. Juni 2015, Braunschweig, Deutschland. Volltext nicht frei.
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.
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). Iniplu 2000.
Bozic, Ognjan and Behrens, Jörg (2005) Per Schienenkanone ins All (Teil 2): Blitzschnell und günstig in den Orbit. Raumfahrt Concret, 2 (37). Iniplu 2000.
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.
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.
Bozic, Ognjan and Mokhtari Molk Abadi, Noushin and Poppe, Georg and May, Stefan (2015) Modeling of the Transformation Kinetics of Small Metal Particles during Combustion inside the Chamber of Hybrid Rocket Engines. 6th EUCASS 2015, 29. June – 2. July 2015, Krakow, Poland. Volltext nicht frei.
Bozic, Ognjan and Poppe, Georg and Porrmann, Dennis (2014) An Advanced Hybrid Rocket Engine for an Alternative Upper Stage of the Brasilian VLM 1 LEO Launcher. In: 65th International Astronautical Congress (ISSN: xxxx ). International Astronautical Fedration. 65th International Astronautical Congress, 29 Sept. – 3 Oct. 2014, Toronto, Canada. ISSN xxxx Volltext nicht frei.
Bozic, Ognjan and Porrmann, Dennis (2010) Estimation of Flow Field Properties and Thrust Performances of Axisymmetric Plug - Nozzles using CFD Simulations. In: Turbulence, Heat and Mass Transfer Begell House, Inc., New York, Wallingford (UK). pp. 599-602. ISBN 978-1-56700-262-1. Volltext nicht online.
Bozic, Ognjan and Porrmann, Dennis and Lancelle, Daniel and May, Stefan (2014) THE LAST ACHIEVEMENTS IN THE DEVELOPMENT OF A ROCKET GRADE HYDROGEN PEROXIDE CATALYST CHAMBER WITH FLOW CAPACITY OF 1 KG/S. In: 3AF - Paris, DVDROM, ST-RCS. SPACE PROPULSION 2014 Conference, 19th to 22nd May 2014, Cologne, Germany. Volltext nicht frei.
Bozic, Ognjan and Porrmann, Dennis and Lancelle, Daniel and May, Stefan (2016) ENHANCED DEVELOPMENT OF A CATALYST CHAMBER FOR THE DECOMPOSITION OF UP TO 1.0 KG/S HYDROGEN PEROXIDE. CEAS Space Journal, 8 (2), pp. 77-88. Springer. DOI: 10.1007/s12567-015-0109-x ISBN x ISSN 1868-2502 Volltext nicht online.
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.
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.
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, pp. 1-13. 6th International Symposium on Turbulence, Heat and Mass Transfer (THMT´09), 14-18 Sept. 2009, Rom, Italy. DOI: 10.1615/ICHMT.2009.TurbulHeatMassTransf.700 Volltext nicht frei.
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.
Brandes, Julia (2010) Herleitung und Analyse eines Finite-Volumen-Verfahrens für reibungsfreie Strömungen. Bachelor's, Universität Kassel. Volltext nicht online.
Breul, Philipp (2015) Bewertung von Opacity-Binning-Methoden zur Vorhersage der Strahlungswärmelasten beim atmosphärischen Eintritt von Raumfahrzeugen. Bachelor's, Georg-August-Universität Göttingen. Volltext nicht online.
Buanga, Björn and Hannemann, Volker and Lüdeke, Heinrich and You, Yancheng and Mack, A. (2009) Modeling of the interaction between a space vehicle’s external ﬂow and it’s plume. In: Annual Report 2009 of SFB/TR 40, Lehrstuhl für Aerodynamik, TU München, 2009 Sonderforschungsbereich/Transregio 40 - Annual Report 2009, --. TU-Braunschweig. pp. 137-148.
Buffetti, Barbara (2014) Title confidential. Project Report. DLR-IB 124-2014/901, 19 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.
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.
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.
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.
Böttcher, Carmen and Longo, Jose Maria (2009) Simulation magnetohydrodynamischer Strömungen in Argon unter Verwendung des DLR TAU-Codes. Other.
Carstensen, Leif (2016) Modellierung von Partikelejektionen in Feststoffraketen. Bachelor's. Volltext nicht frei.
Castaneda Fuentes, Gustavo (2016) Flugmechanische Analyse erzwungener Canardbewegungen anhand der SHEFEX II Experimentalphase. Other. Other. Volltext nicht online.
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.
Dahm, Patrick (2016) Entwurf einer Schubwaage für den Einsatz im Ultrahochvakuum. Bachelor's. Volltext nicht online.
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 Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 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: RTO Educational Notes Models and Computational Methods for Rarefied Flows. 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.
Dittrich, R. (2010) D2.4.2 Report on the Application of MDO Approaches for a Mach 6 SST. Project Report.
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. 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.
Donn, Philipp (2017) Auswertung von Wetterballondaten zur aerodynamischen Einflussanalyse der SHEFEX II Startphase. Bachelor's. Volltext nicht online.
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.
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.
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.
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.
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: New Results in Numerical and Experimental Fluid Mechanics VIII Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 121. Springer Verlag. pp. 67-74. ISBN 978-3-642-35679-7. ISSN 1612-2909 Volltext nicht online.
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.
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.
Fabra Pérez, Miguel (2015) CFD Investigation of the Drag for the VLM-1. Master's. Volltext nicht online.
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, Markus (2015) Investigation of Heatflux Modification by Magnetohydrodynamic Interaction Employing the DLR CFD Code TAU. 8th European Symposium on Aerothermodynamics for Space Vehicles, 02. - 06. Mar. 2015, Lisbon, Portugal. Volltext nicht frei.
Fertig, Markus (2015) Finite Rate Surface Catalysis Modelling of PM1000 and SiC Employing the DLR CFD Solver TAU. 8th European Symposium on Aerothermodynamics for Space Vehicles, 02. - 06. Mar. 2015, Lisbon, Portugal. Volltext nicht frei.
Fertig, Markus (2014) EXOMARS 2018 - DLR-CFD Activities Synthesis Report. Project Report. EXM-D2-TNO-DLR-0001, 60 S. Volltext nicht frei.
Fertig, Markus and Eggers, Thino (2011) DLR-CFD Activities Synthesis Report :EXM-DM-TNO-DLR-0002. DLR-Interner Bericht. DLR-IB 124-2011/915, 40 S. Volltext nicht frei.
Fertig, Markus and Eggers, Thino (2015) Planetary Probe — Numerical Rebuilding Report. Project Report. PP-RCH-DLR-0002, 41 S. Volltext nicht frei.
Fertig, Markus and Eggers, Thino (2015) Development of an Innovative Validation Strategy of Gas-Surface Interaction Modelling for Re-Entry Applications — TN4210 - Development and validation of numerical models in TAU. Project Report. GSI-MODA-DLR-4210. Volltext nicht frei.
Fertig, Markus and Eggers, Thino (2015) Characterisation of the radio transmission black-out — CFD Evaluation of Black-Out. Project Report. ATV-BUC-TN-4007. Volltext nicht frei.
Franze, Marius (2013) Bestimmung der dynamischen Derivative scharfkantiger Raumfahrzeuge. Diploma, Technische Universität Dresden. Volltext nicht online.
Franze, Marius (2016) SHEFEX II - A First Aerodynamic and Atmospheric Post-Flight Analysis. In: ATMOSPHERIC FLIGHT MECHANICS CONF. AIAA Atmospheric Flight Mechanics Conference, 04.-08. Januar 2016, San Diego, California, USA. Volltext nicht frei.
Franze, Marius (2016) SHEFEX II - An Aerodynamic and Structural Post-Flight Analysis. In: ATMOSPHERIC FLIGHT MECHANICS CONF. AIAA Atmospheric Flight Mechanics Conference, 13.-17. Juni 2016, Washington D.C., USA. Volltext nicht frei.
Friedl, Damian and Martinez Schramm, Jan and Hannemann, Klaus (2015) Measurements by Means of Optical Tracking in the High Enthalpy Shock Tunnel Göttingen, HEG. 8th European Symposium on Aerothermodynamics for Space Vehicles, 02. - 06. March 2015, Lissabon, Portugal. Volltext nicht online.
Friedl, Damian and Martinez Schramm, Jan and Hannemann, Klaus (2015) Aerodynamic Testcases: DLR TAU Code. 1st Spacecraft Demise Workshop, 06. March 2015, Lissabon, Portugal. Volltext nicht online.
Friedl, Damian and Martinez Schramm, Jan and Hannemann, Klaus (2015) Freiflugkraftmesstechnik am Hochenthalpiekanal Göttingen (HEG). DIVA - 11 Workshop, Diagnostik in Verbrennung und Aerodynamik, 17. - 18. Nov. 2015, Göttingen, Germany. Volltext nicht online.
Friedl, Damian and Martinez Schramm, Jan and Hannemann, Klaus (2016) Measurement of Aerodynamic Coefficients of Blunt Cones at the High Enthalpy Shock Tunnel Göttingen. 11th International Workshop on Shock Tube Technology, 30.06.2016, Göttingen, Deutschland. 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.
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 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. American Institute of Aeronautics and Astronautics (AIAA). 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, 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.
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.
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).
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.
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.
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.
Grabe, Martin (2008) Numerical Simulation of Nitrogen Nozzle Expansion Using Kinetic and Continuum Approaches. 59th International Astronautical Conference, 2008-09-28, Glasgow.
Grabe, Martin (2012) Response of the Patterson probe in the transition flow regime. AIP| Conference Proceedings|1501 (1188). American Institute of Physics. ISBN 978-0-7354-1115-9. ISSN 0094-243X Volltext nicht online.
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.
Grabe, Martin and Dettleff, Georg and Hannemann, Klaus (2014) Comparison of Computed Free Thruster Plume Expansion to Experiments. Space Propulsion Conference 2014, 19. - 22. May 2014, Cologne, Germany. Volltext nicht online.
Grabe, Martin and Dettleff, Georg and Hannemann, Klaus (2016) Impact of Nozzle Separation on the Plumes of Two Parallel Thrusters. 30th International Symposium on Rarefied Gas Dynamics, 10.-15. Juli 2016, Victoria, Kanada. DOI: 10.1063/1.4967669 Volltext nicht online.
Grabe, Martin and Holz, Andre and Dettleff, Georg and Ziegenhagen, Stefan and Hannemann, Klaus (2014) Numerical Investigation of Two Interacting Parallel Thruster-Plumes and Comparison to Experiment. 29th International Symposium on Rarefied Gas Dynamics, 13. - 18. Juli 2014, Xi´an, China. Volltext nicht online.
Grabe, Martin and Holz, André and Ziegenhagen, Stefan and Hannemann, Klaus (2014) Numerical Investigation of Two Interacting Parallel Thruster-Plumes and Comparison to Experiment. AIP Conference Proceedings, 1628 (581). Americen Institut of Physics (AIP). ISBN 978-0-7354-1265-1. ISSN 0094-243X Volltext nicht online.
Grabe, Martin and Schlegat, Thomas and Hannemann, Klaus (2016) Experimental determination of aerodynamic coefficients in rarefied environment based on the DLR-VxG lowdensity wind tunnels. STO-AVT-262 lecture series and VKI workshop Space debris reentry and mitigation, 15. Sept. 2016, Rhode-Saint-Genèse, Belgium. Volltext nicht online.
Haidn, Oskar and Ciezki, Helmut and Hannemann, Klaus and Karl, S. (2007) Selected Supersonic Combustion Activities at DLR within the European LAPCAT Project. 2nd European Conference for Aerospace Sciences (EUCASS2007), 2007-07-01 - 2007-07-06, Brussels (Belgium). Volltext nicht online.
Hanne, Jennifer (2016) Entwicklung eines vakuumtauglichen Schutzgehäuses für eine Infrarotkamera. Bachelor's. 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, 1, p. 4. Curran Associates, Inc.. 27th International Symposium on Shock Waves, 19. - 24. July 2009, St. Petersburg, Russia. ISBN 978-1-61782-781-5 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. 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 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-Verlag, Berlin Heidelberg. 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, Klaus (2014) Vorlesung: Grundlagen der Raumfahrt. Grundlagen der Raumfahrt (Phy-MP22), Wintersemester 2014/2015, Giessen, Deutschland. Volltext nicht online.
Hannemann, Klaus (2015) Hypersonic Research in the High Enthalpy Shock Tunnel Göttingen. Symposium on Shock Waves - ISSW 30, 19. - 24. July 2015, Tel-Aviv, Israel. Volltext nicht online.
Hannemann, Klaus (2015) CFD von Raketenbrennkammern. DLR_Summer_School Raumfahrtantriebe 2015, 21. Sept. - 02. Okt. 2015, München, Germany. Volltext nicht online.
Hannemann, Klaus (2016) "Numerische Modellierung von Raketenschubkammern". DLR_Summer_School Raumfahrtantriebe 2016, 09. Sep. 2016, DLR_Campus_Lampoldshausen, Deutschland. Volltext nicht online.
Hannemann, Klaus (2016) "Einmal Weltraum und zurück - ein Bestandteil unserer Mobilität im 21. Jahrhundert ?". PSE 2016 - Sth International Conference on Plasma Surface Engineering, 12. Sep. 2016, Garmisch-Patenkirchen, Deutschland. Volltext nicht online.
Hannemann, Klaus and Lüdeke, 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 and Karl, Sebastian and Laurence, Stuart (2015) Free Flight Testing of a Scramjet Engine in a Large Scale Shock Tunnel. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 06. - 09. July 2015, Glasgow, Scotland, United Kingdom. DOI: 10.2514/6.2015-3608 Volltext nicht online.
Hannemann, Klaus and Martinez Schramm, Jan and Laurence, Stuart and Karl, Sebastian (2015) Shock tunnel free flight force measurements using a complex model configuration. 8th European Symposium on Aerothermodynamics for Space Vehicles, 02. - 06 March 2015, Lisbon, Protugal. Volltext nicht online.
Hannemann, Klaus and Martinez Schramm, Jan and Laurence, Stuart and Karl, Sebastian and Langener, Tobias and Steelant, Johan (2014) Experimental and Numerical Analysis of the small Scale LAPCAT II Scramjet Flow Path in High Enthalpy Shock Tunnel Conditions. Space Propulsion 2014, 19. - 22. May 2014, Cologne, Germany. Volltext nicht online.
Hannemann, Klaus and Martinez Schramm, Jan and Viguier, Paul and Defoort, Sebastien and Steelant, Johan (2015) Experimental Comparative Synthesis on the Scramjet Powered Waverider Vehicle in HEG and F4 within the LAPCAT II project. 8th European Symposium on Aerothermodynamics for Space Vehicles, 02. - 06. March 2015, Lisbon, Portugal. Volltext nicht online.
Hannemann, Klaus and Seiler, Friedrich (2009) 26th International Symposium on Shock Waves. Springer-Verlag, Berlin Heidelberg. 800 S. ISBN 978-3-540-85167-7. Volltext nicht online.
Hannemann, Volker (2016) Report on Simulations with Thermal Fluid-Structure Interaction. Project Report. Volltext nicht frei.
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.
Harmann, H. P. and Dartsch, H. and Werner, Ellen (2016) Low Drift Thrust Balance with High Resolution. 34rd International Electric Propulsion Conference, 04. -10. Juli 2015, Kobe, Japan. Volltext nicht online.
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-Verlag, Berlin Heidelberg. pp. 421-426. ISBN 978-3-540-85167-7. Volltext nicht online.
Herdrich, G. and Fertig, Markus and Fasoulas, S. and Löhle, S. and Lein, S. and Steinbeck, A. (2011) Review of Non-Equilibrium Atmospheric Entry In-Flight Instrumentations. 7th European Symposium on Aerothermodynamics for Space Vehicles, 09. - 12. Mai 2011, Brügge, Belgien. Volltext nicht online.
Herdrich, Georg and Fertig, Markus and Lein, Sebastian and Löhle, S. and Preci, Arianit and Steinbeck, A. and Wernitz, R. and Auweter-Kurtz, M. and Röser, Hans-Peter (2010) Current Status of Instrumentation Developments at IRS: In-Situ Investigations and Airborne Measurement Campaigns. Acta Astronautica, 66 (7-8), pp. 1087-1098. Elsevier. DOI: 10.1016/j.actaastro.2009.09.028 ISSN 0094-5765 Volltext nicht online.
Herdrich, Georg and Fertig, Markus and Petkow, D. and Steinbeck, A. and Fasoulas, S. (2012) Experimental and Numerical Techniques to Assess Catalysis. Progress in Aerospace Sciences, 48-49, pp. 27-41. Elsevier. DOI: 10.1016/j.paerosci.2011.06.007 ISSN 0376-0421 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.
Hink, Rüdiger (2015) Validation of the k – ω turbulence model for the thermal boundary layer profile of effusive cooled walls. CEAS Space Journal, 7 (3), pp. 389-398. Springer. DOI: 10.1007/s12567-015-0089-x ISSN 1868-2502 Volltext nicht online.
Hink, Rüdiger (2015) HYDRA III Hybrid Rocket Engine - Flight Version Test Results. In: Deutscher Luft- und Raumfahrtkongress 2015. DGLR. Deutscher Luft- und Raumfahrtkongress 2015, 22.-24. Sept. 2015, Rostock, Deutschland. Volltext nicht frei.
Hink, Rüdiger and Eggers, Thino (2014) Valdiation of the k-ω Turbulence Model for the Thermal Turbulent Boundary Layer Profile of Effusive Cooled Walls. Deutscher Luft- und Raumfahrt Kongress 2014, 16.-18. Sept. 2014, Augsburg. Volltext nicht frei.
Hink, Rüdiger and Hannemann, Volker and Eggers, Thino (2014) Extension of the Spalart-Allmaras One-Equation Turbulence Model for Effusive Cooled Rocket Chambers. In: 4th International Space Propulsion Conference. Space Propulsion 2014, 19.-22. Mai 2014, Köln, Germany.
Hock, Stephan (2013) Heat Flux Determination in the High-Enthalpy Shock Tunnel Göttingen 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 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.
Horchler, Tim (2011) Numerische Analyse des Wärmetransports durch Gasstrahlung beim atmosphärischen Wiedereintritt. Diploma, Geor-August Universität Göttingen. Volltext nicht online.
Horchler, Tim and Mani, Karthik V. and Hannemann, Klaus (2015) Dynamic Mode Decomposition of Backward Facing Step Flow Simulation Data. AIAA Aviation - 22nd AIAA Computational Fluid Dynamics Conference, 22. - 26. June 2015, Dallas, Texas, USA. DOI: 10.2514/6.2015-3411 Volltext nicht online.
Horchler, Tim and Oßwald, Kai and Hannemann, Volker and Hannemann, Klaus (2016) Hybrid RANS-LES Study of Transonic Flow in the Wake of a Generic Space Launch Vehicle. 6th Symposium on Hybrid RANS-LES Methods, Straßburg, Frankreich. Volltext nicht online.
Horchler, Tim and Serhan, Chadi and Hannemann, Klaus and Blinde, Paul and Schrijer, Ferdinand (2015) Comparative Analysis of CFD and PIV Base Buffeting Data Considering Decomposition Techniques and Filtering Effects in the Measurement Chain. 3rd TRR 40 Summer Research Program 2015, 20. July - 14. Aug. 2015, Garching, Germany. Volltext nicht online.
Hundertmark, Stephan and Lancelle, Daniel (2014) A Scenario for a Future European Shipboard Railgun. 17th Electromagnetic Launch Symposium, 07.07.2014 - 11.07.2014, San Diego, USA.
Hundertmark, Stephan and Lancelle, Daniel (2015) A Scenario for a Future European Shipboard Railgun. In: IEEE Transactions on Plasma Science pp. 1194-1197. ISSN 0093-3813 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.
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.
Ivancic, Blazenko and Riedmann, Hendrik and Frey, M. and Knab, O. and Karl, Sebastian and Hannemann, Klaus (2016) Investigation of different modeling approaches for computational fluid dynamics simulation of high-pressure rocket combustors. In: EUCASS Book Series Advances in Aerospace Sciences: Progress in Propulsion Physics pp. 95-116. Volltext nicht online.
Ivanov, Dmitrij (2015) MDO-Tool extension and application to the ATLLAS-II reference configuration. DLR-Interner Bericht. DLR-IB 124-2015/912, 57 S. Volltext nicht online.
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.
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 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 (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 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: High Temperature Phenomena in Shock Waves Springer Verlag, Berlin Heidelberg. 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.
Karl, Sebastian (2015) Design, testing and assessment of a subscale scramjet vehicle. Symposium of VKI PhD Research 2015, 11. March - 13. March 2015, Sint-Genesius-Rode (Brussels), Belgium. Volltext nicht online.
Karl, Sebastian and Hannemann, Klaus and Hornung, Hans G. (2012) Bluntness Effects in Hypersonic Flow over Slender Cones and Wedges. In: 28th International Symposium on Shock Waves Shock Waves, 2. Springer Verlag, Berlin Heidelberg. pp. 691-696. ISBN 978-3-642-25684-4. Volltext nicht online.
Karl, Sebastian and Potter, Daniel and Lambert, Markus and Hannemann, Klaus (2015) CFD Analysis of radiative heat loading on hypervelocity re-entry vehicles. Journal of Spacecraft and Rockets, 52 (1), pp. 63-74. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.A32791 ISSN 0022-4650 Volltext nicht online.
Karl, Sebastian and Steelant, Johan (2015) Cross-Flow Phenomena in Streamline Traced Hypersonic Intakes. American Institute of Aeronautics and Astronautics (AIAA). 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 06. - 09. July 2015, Glasgow, Scotland. DOI: 10.2514/6.2015-3594 Volltext nicht online.
Keiderling, David (2015) Advancement of the DLR TAU Code to Simulate Two-phase Flow including Phase-change at the Interface. PhD Network Days 2015 Space Systems Germany, 09. Sept. 2015, Bremen, Deutschland. Volltext nicht online.
Keiderling, David (2015) Advancement of the DLR TAU code Method to Simulate Two-phase Flow with Phase-change at the Interface with Applications in Upper Stages of Space Launch Systems. Project Report. Volltext nicht online.
Keiderling, David (2016) Development of the DLR TAU-Code for the Simulation of Propellant Motion and Phase Change Processes. Seminar Justus Liebig University Gießen, 15. Nov. 2016, Gießen, Deutschland. 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.
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.
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, 21 (3), pp. 233-241. Springer. DOI: 10.1007/s00193-011-0314-2 ISSN 0938-1287 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.
Klar, Peter J. and Hannemann, Klaus and Ricklefs, Ubbo and Leiter, Hans (2015) Overview of the research activities of the RITSAT-project. 34th International Electric Propulsion Conference, 06. - 10. July 2015, Kobe-Hyogo, Japan. Volltext nicht online.
Klaus, Johannes Tobias (2015) Einfluss der Verwirbelung vergaster Treibstoffkomponenten auf den Prozess in der Brennkammer eines Hybridraketentriebwerks. Bachelor's, Technische Universität Braunchweig. Volltext nicht online.
Klaus, Johannes Tobias (2016) Entwurf und innerballistische Analyse der Brennkammer eines HRT-Demonstrators in der Schubklasse bis 13000 N. Other. Volltext nicht online.
Klaus, Johannes Tobias and Bozic, Ognjan and May, Stefan and Poppe, Georg (2016) ERHÖHUNG DES SCHUBS VON HYBRIDRAKETENTRIEBWERKEN DURCH OPTIMIERUNG DER BRENNSTOFFTREIBSATZFORM MIT VERWUNDENER FINOZYLGEOMETRIE. 65. DLRK, 13.-15. Sep. 2016, Braunschweig, Deutschland. 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.
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).
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.
Kuhn, Tobias (2014) Strömungscharakterisierung der Hypersonischen Versuchsanlage V2G. Other. Studienarbeit, 67 S. Volltext nicht online.
Lancelle, Daniel (2015) Zur Optimierung eines elektromagnetisch gestarteten Satellitenträgers. Dissertation. DLR-Forschungsbericht. DLR/FB 2015/07, 157 S. Volltext nicht online.
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.
Lancelle, Daniel and Bozic, Ognjan (2015) Thermal Protection, Aerodynamics, and Control Simulation of an Electromagnetically Launched Projectile. IEEE Transactions on Plasma Science, 43 (5), pp. 1156-1161. IEEE - Institute of Electrical and Electronics Engineers. ISBN ISSN: 0093-3813 ISSN 0093-3813 Volltext nicht online.
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.
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 - Institute of Electrical and Electronics Engineers. ISBN 978-1-4673-0306-4 ISSN 0093-3813 Volltext nicht frei.
Lancelle, Daniel and Božić, Dr. Ognjan (2014) Thermal Protection-, Aerodynamics- and Control Simulation of an Electromagnetically Launched Projectile. 17th Electromagnetic Launch Symposium, 07.07.2014-11.07.2014, San Diego, USA.
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.
Langener, Tobias and Steelant, Johan and Karl, Sebastian and Hannemann, Klaus (2014) Numerical Validation of a Free-Flying Scramjet Powered Vehicle at Realistic Wind Tunnel Conditions. Space Propulsion 2014, 19. - 22. Mai 2014, Cologne, Germany. Volltext nicht online.
Larsson, Johan and Laurence, Stuart Jon and Bermejo-Moreno, Ivan and Bodart, Julien and Karl, Sebastian and Vicquelin, Ronan (2015) Incipient thermal choking and stable shock-train formation in the heat-release region of a scramjet combustor: Part II: Large eddy simulations. Combustion and Flame, 162 (4), pp. 907-920. Elsevier. DOI: 10.1016/j.combustflame.2014.09.017 ISSN 0010-2180 Volltext nicht online.
Lau, Matthias and Grabe, Martin and Herdrich, Georg (2014) Experimental Characterization of a Scalable Pulsed Magnetoplasmadynamic Propulsion System. Space Propulsion 2014, 19. - 22. May 2014, Cologne, Germany. 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 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.
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.
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.
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. DOI: 10.1007/s00348-009-0780-9 ISSN 0723-4864 (Print), 1432-1114 (Online) Volltext nicht online.
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 Karl, Sebastian and Hannemann, Klaus (2015) Experimental and Numerical Investigation of the HyShot II Flight Experiment. Springer International Publishing. ISBN 978-3-319-16834-0. Volltext nicht online.
Laurence, Stuart and Wagner, Alexander and Hannemann, Klaus (2014) Schlieren-based techniques for investigating instability development and transition in a hypersonic boundary layer. Experiments in Fluids, 55 (8), pp. 1-17. Springer. DOI: 10.1007/s00348-014-1782-9 ISSN 0723-4864 Volltext nicht online.
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 (2015) Investigation of Hypersonic Boundary-Layer Transition Using High-Speed Visualization Techniquesment. Springer International Publishing. ISBN 978-3-319-16834-0. Volltext nicht online.
Laurence, Stuart and Wagner, Alexander and Hannemann, Klaus (2016) Experimental study of second-mode instability growth and breakdown in a hypersonic boundary layer using high-speed schlieren visualization. Journal of Fluid Mechanics. Cambidge University Press. DOI: 10.1017/jfm.2016.280 ISSN 0022-1120 Volltext nicht online.
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.
Laurence, Stuart Jon and Lieber, Damien and Martinez Schramm, Jan and Hannemann, Klaus and Larsson, Johan (2015) Incipient thermal choking and stable shock-train formation in the heat-release region of a scramjet combustor: Part I: Shock-tunnel experiments. Combustion and Flame, 162 (4), pp. 921-931. Elsevier. DOI: 10.1016/j.combustflame2014.09016 ISSN 0010-2180 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.
Lein, S. and Steinbeck, A. and Preci, A. and Fertig, Markus and Herdrich, G. and Röser, H.-P. and Auweter-Kurtz, M. (2010) Final Design and Performance Parameters of the Payloads PYREX, PHLUX and RESPECT on EXPERT. Transactions of the Japan Society for Aeronautical and Space Sciences, Space Technology Japan, 8 (ists27), Tm_41-Tm_47. DOI: 10.2322/tastj.8.Tm_41 ISSN 1347-3840 Volltext nicht online.
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.
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 (2015) Hot Stage Seperation of Rockets Using Coupled CFD and Flight Mechanics Method. Dissertation. DLR-Forschungsbericht. DLR-FB 2015-19, 141 S. 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. ISSN 0094-5765 Volltext nicht frei.
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.
Li, Yi and Reimann, Bodo and Eggers, Thino (2016) Coupled simulation of CFD-flight-mechanics with a two-species-gas-model for the hot rocket staging. Acta Astronautica (128), pp. 44-61. Elsevier. ISBN ISSN 0094-5765 ISSN 0094-5765 Volltext nicht frei.
Liebhart, H. and Fertig, Markus and Herdrich, Georg and Fasoulas, Stefanos and Röser, Hans-Peter (2011) Contribution of Vacuum-Ultraviolet Transitions of Molecular Nitrogen to Radiative Heat Flux During Aatmospheric Reentry. 4th International Workshop Radiation of High Temperature Gases in Atmospheric Entry, 12.-15. Okt. 2010, Lausanne, Schweiz. ISBN 978-92-9092-253-7 Volltext nicht frei.
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).
Longo, J.M.A. and Hannemann, K. and Hannemann, V. (2007) The Challenge of Modeling High Speed Flows. ISBN 978-3-901608-32-2.
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).
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).
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).
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).
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.
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.
Löhle, S. and Wernitz, R. and Herdrich, G. and Fertig, M. and Röser, H.-P. and Ritter, H (2011) Airborne re-entry observation experiment SLIT: UV spectroscopy during STARDUST and ATV1 re-entry. CEAS Space Journal, 1 (1-4), pp. 59-69. Springer. DOI: 10.1007/s12567-011-0018-6 ISSN 1868-2502 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, 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.
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.
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.
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.
Lüdeke, Heinrich and Bartolome Calvo, Javier (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. Springer. DOI: 10.1007/s12567-010-0002-6 ISSN 1868-2502 Volltext nicht online.
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. Springer. DOI: 10.1007/s12567-010-0002-6 Volltext nicht frei.
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.
Lüdeke, Heinrich and Mulot, Jean Daniel and Hannemann, Klaus (2015) Launch Vehicle Base Flow Analysis Using Improved Delayed Detached Eddy Simulation. AIAA Journal, 53 (9), pp. 2454-2471. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.J053297 ISSN 0001-1452 Volltext nicht online.
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.
Lüdeke, Heinrich and Seitz, Arne and Wartemann, Viola (2010) Direkte numerische Simulation von Tollmien Schlichting Wellen zur Unterstützung linearer Stabilitätsanalysen. 17. DGLR / STAB Fachsymposium, 9.-10. Nov. 2010, Berlin, Deutschland. Volltext nicht online.
Lüdeke, Heinrich and Wartemann, Viola (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.
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.
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-Verlag, Berlin Heidelberg. pp. 619-624. ISBN 978-3-540-85182-0. Volltext nicht online.
Majid, A. and Bauder, U. and Fertig, Markus and Herdrich, G. and Röser, H.-P. (2010) Particle Wall Interactions in Dusty Hypersonic Entry Flows. Frontier of applied plasma technology, 3 (1). ISSN 1883-5589 Volltext nicht online.
Majid, A. and Bauder, U. and Herdrich, G. and Fertig, Markus (2012) Effect of Dust Particles on Space Vehicles Entering Mars at Hypersonic Speeds. 63rd International Astronautical Congress 2012 (IAC 2012), 01.-05. Okt. 2012, Neapel, Italien. Volltext nicht online.
Majid, A. and Bauder, U. and Herdrich, G. and Fertig, Markus (2016) Two-Phase Flow Solver for Hypersonic Entry Flows in a Dusty Martian Atmosphere. Journal of Thermophysics and Heat Transfer, pp. 418-428. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.T4542 ISSN 0887-8722 Volltext nicht online.
Mani, Karthik V. and Cervone, Angelo and Hickey, Jean-Pierre (2016) Turbulence Modeling of Cavitating Flows in Liquid Rocket Turbopumps. Journal of Fluids Engineering - Transactions of the ASME. American Society of Mechanical Engineers (ASME). DOI: 10.1115/1.4034096 ISSN 0098-2202 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 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 Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 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 Edzards, Frank and Hannemann, Klaus (2016) Development of Ultra-fast Temperature Sensitive Paints for Hypersonic High Enthalpy Flows. 20. DGLR Fachsymposium der STAB, 08.-09. Nov. 2016, Braunschweig, Deutschland. Volltext nicht online.
Martinez Schramm, Jan and Hannemann, Klaus and Karl, Sebastian and Defoort, Sebastien and Viguier, Paul and Steelant, Johan (2015) Ground Testing Synthesis of the LAPCAT II Small Scale Flight Experiment Configuration Scramjet Flow Path. American Institute of Aeronautics and Astronautics. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 06. - 09. July 2015, Glasgow, Scotland, United Kingdom. DOI: 10.2514/6.2015-3627 Volltext nicht online.
Martinez Schramm, Jan and Hannemann, Klaus and Ozawa, Hiroshi and Beck, Walter and Klein, Christian (2015) Development of Temperature Sensitive Paints in the High Enthalpy Shock Tunnel Göttingen, HEG. 8th European Symposium on Aerothermodynamics for Space Vehicles, 02. - 06 March 2015, Lisbon, Portugal. Volltext nicht online.
Martinez Schramm, Jan and Wagner, Alexander and Reimann, Bodo and Fertig, M. 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 (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 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.
Massuti-Ballester, B. and Pidan, Sergej and Herdrich, G. and Fertig, Markus (2015) Recent Catalysis Measurements at IRS. Advances in Space Research, pp. 1-55. Elsevier. DOI: 10.1016/j.asr.2015.04.028 ISSN 0273-1177 Volltext nicht online.
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.
May, Stefan (2013) Bestimmung der Wärmelasten am Düsenausgang eines Hybridraketentriebwerks. Other, Technische Universität Braunschweig. Volltext nicht online.
May, Stefan (2015) Numerische Verbrennungssimulation in HTPB/H2O2 Hybridraketentriebwerken. DGLR Workshop „Feststoff- und Hybridraketentriebwerke – Aktueller Entwicklungsstand und Perspektiven“, 18.-19. Jun., Braunschweig, Deutschland. Volltext nicht online.
May, Stefan and Bozic, Ognjan (2014) Numerical Simulation of the Flow and Combustion inside the Reaction Chamber of the AHRES Hybrid Rocket Engine. In: Jahresbericht der STAB 2014, 2014, pp. 58-59. 19. DGLR-Fachsymposium der STAB, 04.-05. Nov. 2014, München, Deutschland. Volltext nicht online.
May, Stefan and Bozic, Ognjan (2013) Bestimmung der Wärmelasten am Düsenausgang eines Hybridraketentriebwerks. In: Jahresbericht der STAB 2013, 2013, pp. 58-59. 16. STAB-Workshop, 12.-13. Nov. 2013, Göttingen, Deutschland. Volltext nicht online.
May, Stefan and Bozic, Ognjan (2016) Numerical Simulation of the Flow and Combustion inside the Reaction Chamber of the AHRES Hybrid Rocket Engine. In: New Results in Numerical and Experimental Fluid Mechanics X Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 132. Springer Verlag. pp. 801-810. ISBN 978-3-319-27278-8. ISSN 1612-2909 Volltext nicht online.
May, Stefan and Bozic, Ognjan (2015) CFD Simulation of Chemical Non‐Equilibrium Reacting Flow within the AHRES Hybrid Rocket Engine. 6th EUCASS, 29. Jun. - 2. Jul., Krakau, Polen. Volltext nicht online.
Merrem, Clemens Hans-Joachim (2014) Auswahl eines geeigneten Regressionsmodells für Hybridraketenantriebe aufgrund von experimentellen Ultraschall Messdaten. Other, TU Braunschweig. Volltext nicht online.
Merrem, Clemens Hans-Joachim (2015) Statische und dynamische Eigenschaften eines geregelten pneumatisch-hydraulischen Druckgas-Fördersystems zur Anwendung in einem Hybridraketentriebwerk. Master's, Technische Universität Braunschweig. 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.
Mokhtari Molk Abadi, Noushin (2014) Kinetik der Umwandlung und Verbrennung von metallhaltigen Kleinpartikeln innerhalb eines Hybridraketentriebwerks. Master's. 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.
Munk, Johannes (2016) Numerical Investigations of Rotating Liquids with the DLR THETA code. Master's. Volltext nicht frei.
müller, Lukas (2016) Application and enhancement of a Fortran-Software to compute Panel flutter phenomenia in potential flows. Bachelor's, Hochschule für Angewandte Wissenschaften Hamburg. 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.
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.
Neumann, Andreas (2014) Electric Propulsion Test Facility at DLR. Electric Propulsion Innovation & Competitiveness (EPIC), 25. - 28. Nov. 2014, Brussel, Belgium. Volltext nicht online.
Neumann, Andreas (2015) Messung von Schubkräften im mN-Bereich an Raumfahrtantrieben. DIVA - 11 Workshop, Diagnostik in Verbrennung und Aerodynamik, 17. - 18. Nov. 2015, Göttingen, Germany. Volltext nicht online.
Neumann, Andreas (2015) DLR’s Electric Propulsion Test Facility – Status and Perspective. International Science and Applied Research Conference devoted to the 60-th anniversary of EDB Fakel, 05. - 07. Oct. 2015, Kaliningrad, Russia. Volltext nicht online.
Neumann, Andreas (2015) Neue Entwicklungen an der Göttinger Testanlage für elektrische Raumantriebe. XXII. Erfahrungsaustausch „Oberflächentechnologien mit Plasma- und Ionenstrahlprozessen“, 10. bis 12. März 2015, Mühlleiten, Deutschland. Volltext nicht online.
Neumann, Andreas (2016) Update on Diagnostics for DLR's Electric Propulsion Test Facility. 6th Russian-German Conference on Electric Propulsion and Their Application, 28. Aug. - 02. Sept. 2016, Samara, Russland. Volltext nicht online.
Neumann, Andreas and Geile, Christopher and Stämm, Stefan and Hannemann, Klaus (2015) DLR’s Electric Propulsion Test Facility – the First Three Years of Thruster Operation. 34th International Electric Propulsion Conference, 04. - 10. July 2015, Kobe-Hyogo, Japan. Volltext nicht online.
Neumann, Andreas and Hannemann, Klaus (2014) Electric Propulsion Testing at the DLR Göttingen: Facility and Diagnostics. Space Propulsion 2014, 19. - 22. May 2014, Cologne, Germany. Volltext nicht online.
Neumann, Andreas and Mühlich, Nina and Hannemann, Klaus (2016) Magnetic Fields and Ion Thruster Beam Effects in DLR’s EP Test Facility. Space Propulsion 2016, 02.- 06. Mai 2016, Rom, Italien. Volltext nicht online.
Neumann, Andreas and Nigmatzyanov, Vladislav V. and Stämm, Stefan (2014) Measurement system for plasma beam profiling at long distance inside the DLR electric propulsion test facility. 5th Russian-German Conference “Electric Propulsions - New Challenges”, 07. - 12. Sept. 2014, Dresden, Germany. Volltext nicht online.
Neumann, Andreas and V. Nigmatzyanov, Vladislav (2016) Far-Field Beam Diagnostics at DLR’s EP Test Facility. Space Propulsion 2016, 02. - 06. Mai 2016, Rom, Italien. Volltext nicht online.
Nigmatzyanov, Vladislav V. and Neumann, Andreas and Hannemann, Klaus and Klar, Peter J. (2015) New 2d Far Field Beam Scanning Device at DLR's Electric Propulsion Test Facility. 34th International Electric Propulsion Conference, 04. - 10. July 2015, Kobe-Hyogo, Japan. Volltext nicht online.
Nizenkov, P. and Noeding, P. and Konopka, M. and Reimann, Bodo and Fasoulas, Stefanos (2016) Numerical Investigation of the Aerodynamics of the REX-Free Flyer in the Rarefied Gas Regime. In: AIP Conference Proceedings. 30th International Symposium on Rarefied Gas Dynamics, 10.-15. Juli 2016, Victoria, Kanada. DOI: 10.1063/1.4967683 Volltext nicht online.
Noeding, 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.
Nordin-Bates, K. and Fureby, Christer and Karl, Sebastian and Hannemann, Klaus (2016) Understanding scramjet combustion using LES of the HyShot II combustor. Proceedings of the Combustion Institute, pp. 1-8. Elsevier. DOI: 10.1016/j.proci.2016.07.118 ISSN 1540-7489 Volltext nicht online.
Odam, Judith and Paull, Allan (2006) Radical Farming in Scramjets. In: Notes Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 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.
Ozawa, Hiroshi and Laurence, Stuart Jon and Martinez Schramm, Jan and Wagner, Alexander and Hannemann, Klaus (2015) Fast‑response temperature‑sensitive‑paint measurements on a hypersonic transition cone. Experiments in Fluids, 56 (1), pp. 1-13. Springer. DOI: 10.1007/s00348-014-1853-y ISSN 0723-4864 Volltext nicht online.
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.
Oßwald, Kai and Hannemann, Volker (2015) An implicit-explicit time stepping scheme for hybrid RANS/LES methods. 6th European Conference for Aeronautics and Space Sciences (EUCASS), 29. June - 03. July, Kraków, Poland. Volltext nicht online.
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.
Oßwald, Kai and Siegmund, Alexander and Birken, Philipp and Hannemann, Volker and Meister, Andreas (2015) L²Roe: A low-dissipation version of Roe's approximate Riemann solver for low Mach numbers. International Journal for Numerical Methods in Fluids, pp. 1-16. Wiley. DOI: 10.1002/fld.4175 ISSN 0271-2091 Volltext nicht online.
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.
Petervari, René (2016) Die Messung von Anströmungsstörungen in hypersonischen Windkanälen mit intrusiven und nicht-intrusiven Messtechniken. Master's. Volltext nicht online.
Petervari, René and Wagner, Alexander and Hannemann, Klaus (2015) Messung von Anströmungsstörungen in Hypersonischen Windkanälen. 17. STAB-Workshop, 10.-11. November 2015, Göttingen, Deutschland. Volltext nicht online.
Petervari, René and Wagner, Alexander and Hannemann, Klaus (2015) Messung von Anströmungsstörungen in Hypersonischen Windkanälen - Motiviert durch Transitionsuntersuchungen am HEG. DIVA - 11 Workshop, Diagnostik in Verbrennung und Aerodynamik, 17. - 18. Nov. 2015, Göttingen, Germany. Volltext nicht online.
Petervari, René and Wagner, Alexander and Laurence, Stuart and Wartemann, Viola and Hannemann, Klaus (2014) Quantitative Auswertung von Hochgeschwindigkeitsschlierenaufnahmen der hypersonischen Grenzschichtinstabilität am Hochenthalpiekanal Göttingen. 19. DGLR-Fachsymposium der STAB, 04. - 05. Nov. 2014, München, Deutschland. Volltext nicht online.
Pezzella, Giuseppe and Marini, Marco and Reimann, Bodo and Steelant, Johan (2015) Aerodynamic Design Analysis of the HEXAFLY-INT Hypersonic Glider. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference (Hypersonics 2015), 6 - 9 July 2015, Glasgow, Scotland. 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.
Piechotka, Markus and Nigmatzyanov, Vladislav V. and Holste, Kristof and Henning, Thorsten and Neumann, Andreas and Hannemann, Klaus and Klar, Peter J. (2015) Test Procedure for locally assessing potential risks of sputter damage due to thruster plumes. 34th International Electric Propulsion Conference, 04. - 10. July 2015, Kobe-Hyogo, Japan. Volltext nicht online.
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.
Poppe, Georg (2014) Hydraulisch-pneumatische und innenballistische Eigenschaften des AHREUS-Triebwerks für die Oberstufe der VLM-Trägerrakete. Master's, Technische Universität Braunschweig. Volltext nicht online.
Poppe, Georg (2013) Charakterisierung der Innenballistik und der Wärmeübertragung in der Brennkammer von Feststoff- und Hybridraketentriebwerken. Other, Technische Universität Braunschweig. Volltext nicht online.
Poppe, Georg and Koch, Patrick and Bozic, Ognjan (2015) Optimierung der Finozylen Treibstoffgeometrie in Feststoffboostern. DGLR Workshop „Feststoff- und Hybridraketentriebwerke – Aktueller Entwicklungsstand und Perspektiven“, 18. - 19. Juni 2015, Braunschweig, Deutschland. Volltext nicht frei.
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.
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.
Rana, Usman and Hink, Rüdiger (2014) Design of a Valve Segment for a Hybrid Rocket Engine. Deutscher Luft- und Raumfahrtkongress 2014, 16.-18. September, Augsburg. Volltext nicht frei.
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.
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 Johnston, Ian and Hannemann, Volker (2003) DLR τ-Code for High Enthalpy Flows. New Results in Numerical and Experimental Fluid Mechanics IV, 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.
Reimann, Bodo (2015) Numerical Simulation of the Free Pitch Oscillation for a Re-entry Vehicle in Transonic Wind Tunnel Flow. 8th European Symposium on Aerothermodynamics for Space Vehicles, 2-6 March 2015, Lissabon, Portugal. Volltext nicht online.
Reimann, Bodo (2016) Numerical Prediction of LongitudinalDynamic Stability for a Lifting Body in Transonic Flow. AIAA AVIATION 2016, 13.-17. Juni 2016, Washington, USA. Volltext nicht online.
Reimann, Bodo (2009) Numerische Untersuchung der Stoßrohrströmung im Hochenthalpiekanal Göttingen. Dissertation, Universität Duisburg-Essen. Volltext nicht online.
Reimann, Bodo and Hannemann, Volker and Hannemann, Klaus (2009) Computations of shock wave propagation with local mesh adaptation. In: 26th International Symposium on Shock Waves Shock Waves, 2. Springer Verlag. pp. 1383-1388. ISBN 978-3-540-85182-0. Volltext nicht online.
Reinke, Nico (2009) Numerische Analyse kompressibler turbulenter Strömungsfelder. Diploma, Georg August Universität Göttingen. Volltext nicht online.
Reiter, Philipp (2016) Transition Prediction for Hypersonic Conical Flows with Active Cooling. Other, Technische Universität Branuschweig/ DLR Institut für Aerodynamik und Strömungstechnik. Volltext nicht frei.
Riedmann, Hendrik and Banuti, Daniel and Ivancic, Blazenko and Knab, Oliver and Hannemann, Klaus (2015) Modeling of H_2/O_2 Single-Element Rocket Thrust Chamber Combustion at Sub- and Supercritical Pressures with Different CFD Tools. 6th European Conference for Aeronautics and Space Sciences - EUCASS 2015, 29. June - 03 July 2015, Kraków, Poland. Volltext nicht online.
Risius, Steffen and Beck, Walter and Klein, Christian and Henne, Ulrich and Wagner, Alexander (2016) Heat Transfer Measurements on a Ramp Model in the High Enthalpy Shock Tunnel (HEG) using Temperature Sensitive Paint. 51’st 3AF International Conference on Applied Aerodynamics: Thermal effects and aerodynamics, 04. – 06. April 2016, Strasbourg, France. 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 Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 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, 1 (1), pp. 45-57. Springer. 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.
Rolfes, Steffen (2016) Inbetriebnahme einer Hybridraketentriebwerkslaborbrennkammer zur Messung der Abbrandrate des festen Brennstoffs und der Charakterisierung des Verbrennungsprozesses. [Other] 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.
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.
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.
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.
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.
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 (9), pp. 2243-2252. American Institute of Aeronautics and Astronautics (AIAA). Volltext nicht frei.
Sarma, G. S. R. (2005) Electric Thruster Plume Characterization. DLR-Interner Bericht. DLR-IB 224-2004 A09, 88 S. Volltext nicht online.
Schlegat, Thomas (2015) Re-design of the Strain Gauge Force Balances for the Hypersonic Vacuum Wind Tunnel Göttingen. DLR-Forschungsbericht. DLR-FB--2013-18, 118 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.
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 - Institute of Electrical and Electronics Engineers. 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.
Schäfer, Stefan (2015) Numerische Untersuchung von reagierenden Hyperschallströmungen um sphärisch abgestumpfte Kegel. Master's, Karlsruher Institut für Technologie (Universität in Karlsruhe, Baden-Württemberg), Fakultät für Maschinenbau. 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. Volltext nicht frei.
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).
Steelant, J. and Villace, V. and Marini, M. and Pezzella, G. and Reimann, B. and Chernyshev, S. L. and Gubanov, A. A. and Talyzin, V. A. and Voevodenko, N. V. and Kukshinov, N. V. and Prokhorov, A. N. and Neely, A. J . and Kennel, C. and Verstraete, D. and Buttsworth, D. (2016) Numerical ans Experimental Research on Aerodynamics of a High-speed Passenger Vehicle within the HEXAFLY-INT Project. ICAS 2016, Daejeon. Korea. Volltext nicht online.
Steelant, Johan and Varvill, Richard and Defoort, Sebastien and Hannemann, Klaus and Marini, Marco (2015) Achievements Obtained for Sustained Hypersonic Flight within the LAPCAT-II Project. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 06. - 09. July 2015, Glasgow, Scotland, United Kingdom. DOI: 10.2514/6.2015-3677 Volltext nicht online.
Stollmeier, Frank (2009) Rechengitter zur Teilchenverfolgung in DSMC-Strömungssimulationen. Bachelor's, Georg-August-Universität Göttingen.
Stollmeier, Frank and Grabe, Martin (2011) A Voronoi Grid and a Particle Tracking Algorithm for DSMC. AIP| Conference Proceedings|1333 (331). 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.
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.
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.
Stämm, Stefan and Neumann, Andreas (2016) Diagnostik und Entwicklungsstand an der STG-ET. XXIII. Erfahrungsaustausch Oberflächentechnologie mit Plasma- und Ionenstrahlprozessen, 17.03.2016, Mühlleithen, Deutschland. Volltext nicht online.
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.
Tanno, H. and Komuro, T. and Sato, K. and Fujita, K. and Laurence, Stuart (2014) Free-flight measurement technique in the free-piston high-enthalpy shock tunnel. Review of Scientific Instruments, 85 (4), pp. 1-8. American Institute of Physics (AIP). DOI: 10.1063/1.4870920 ISSN 0034-6748 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 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.
Traphan, Dominik (2011) Experimentelle Untersuchung von Freistrahlen aus geometrisch ähnlichen Düsen. Diploma, DLR. Volltext nicht online.
Vogt, Daniel (2015) Vorauslegungsverfahren zur Massenabschätzung von Raketenstufen. Bachelor's, Technische Universität Braunschweig. Volltext nicht online.
Volkmar, Robin (2014) Umgestaltung einer Software zur Messdatenerfassung zur Vereinfachung künftiger Erweiterungen. Bachelor's, Dualen Hochschule Baden-Württemberg Mannheim. Volltext nicht online.
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.
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.
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.
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.
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 (2014) Passive Hypersonic Boundary Layer Transition Control Using Ultrasonically Absorptive Carbon-Carbon Ceramic with Random Microstructure / Passive Kontrolle des Laminar-Turbulenten Grenzschichtumschlages durch Verwendung von ultraschallabsorbierendem, kohlenstofffaserverstärktem Kohlenstoff mit zufälliger Mikrostruktur. Dissertation. DLR-Forschungsbericht. DLR-FB 2014-31, 146 S. Katholieke Universiteit Leuven – Faculty of Engineering, Celestijnenlaan 300C box 2402, 3001 Leuven, Belgium (Belgium). Volltext nicht frei.
Wagner, Alexander (2015) Freestream disturbance measurements in HEG. NATO STO AVT-240 & RTG-082: Hypersonic Boundary-Layer Transition Prediction, 27. March 2015, Tucson, USA. Volltext nicht online.
Wagner, Alexander (2015) Title confidential. DLR-Interner Bericht. DLR-IB 224-2015 C 175, 41 S. Volltext nicht online.
Wagner, Alexander (2015) The role of carbon/carbon composites in the delay of hypersonic laminar to turbulent boundary layer transition. Porous media interactions with high temperature and high speed flows - NATO STO AVT-261, 07. - 09. Sept. 2015, Brussels, Belgium. Volltext nicht online.
Wagner, Alexander and Benjamin, Leroy (2016) Investigation of the 1st and 2nd Mode Instability by Means of Schlieren Visualization. NATO STO AVT-240 & RTG-082: Hypersonic Boundary Layer Transition Prediction, 30. Sept. 2016, Avila, Spanien. Volltext nicht online.
Wagner, Alexander and Hannemann, Klaus (2016) Proposals on Boundary Layer Transition by DLR AS-GÖ – Experimental Studies at HEG. AFRL/DLR Project Agreement Workshop Hypersonic Technologies, 09. - 10. Juni 2016, Göttingen, Deutschland. Volltext nicht online.
Wagner, Alexander and Martinez Schramm, Jan (2016) Stoß-Grenzschicht-Wechselwirkungen an einer beheizten ebenen Platte im HEG. Institutskolloquium, 29. April 2016, Göttingen, Deutschland. Volltext nicht online.
Wagner, Alexander and Schramm, M. and Hickey, Jean Pierre and Hannemann, Klaus (2016) Hypersonic Shock Wave Boundary Layer Interaction Studies on a Flat Plate at Elevated Surface Temperature. 22nd International Shock Interaction Symposium, 04.-08. Juli 2016, Glasgow, England. Volltext nicht online.
Wagner, Alexander and Wartemann, Viola (2014) Boundary Layer Transition Studies in HEG - OVERVIEW. NATO STO AVT-240 & RTG-082: Hypersonic Boundary-Layer Transition Prediction, Munich, Germany. Volltext nicht online.
Wagner, Alexander and Wartemann, Viola (2015) Hypersonic Boundary-Layer Transition in the DLR High Enthalpy Shock Tunnel Göttingen (HEG) – Part 2. Seminar Sandia National Laboratories, 23. March 2015, Albuquerque, NM, USA. Volltext nicht online.
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.
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 . American Institute of Aeronautics and Astronautics (AIAA). 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.
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.
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.
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.
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.
Wartemann, Viola and Lüdeke, Heinrich (2010) Numerical investigations of hypersonic boundary layer stabilization by means of porous surfaces. 17. DGLR / STAB Fachsymposium, 9.-10. Nov. 2010, Berlin, Deutschland. Volltext nicht online.
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.
Wartemann, Viola and Wagner, Alexander (2015) Hypersonic Boundary-Layer Transition in the DLR High Enthalpy Shock Tunnel Göttingen (HEG) – Part 1. Seminar of Sandia National Laboratories, 23. March 2015, Albuquerque, USA. Volltext nicht online.
Wartemann, Viola and Wagner, Alexander and Eggers, Thino (2016) Passive hypersonic boundary layer control: The Potential of an Ultrasonically Absorptive Ceramic for HEXAFLY-INT. AIAA Aviation – 8th AIAA Flow Control Conference, 13. - 17. Juni 2016, Washington, USA. DOI: 10.2514/6.2016-4250 Volltext nicht online.
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.
Wartemann, Viola and Wagner, Alexander and Eggers, Thino and Hannemann, Klaus (2014) Passive hypersonic boundary layer transition control using an ultrasonically absorptive coating with random microstructure - Part 2: Computational Analysis. IUTAM - ABCM Symposium on Laminar-Turbulent Transition, 08.-12. Sep. 2014, Rio de Janeiro, Brazil. Volltext nicht online.
Wartemann, Viola and Wagner, Alexander and Eggers, Thino and Hannemann, Klaus (2015) Passive hypersonic boundary layer control by means of ultrasonically absorptive carbon-carbon ceramics: Investigations of different boundary conditions. 20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 06. - 09. July 2015, Glasgow, United Kingdom. Volltext nicht online.
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: 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.
Weigmann, Pascal (2015) Die Genauigkeit optischer Bewegungsverfolgung eines Modell-Targets im HEG. Bachelor's, Georg-August-Universität. Volltext nicht online.
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.
Werner, Ellen and Dettleff, Georg and Grabe, Martin and Hannemann, Klaus (2014) Experimental study of plume flow emanating from rectangular orifices. Space Propulsion 2014, 19. - 22. May 2014, Cologne, Germany. Volltext nicht online.
Wilken, Jascha (2014) Analyse von Ultraschallsignalen für die Regressionsmessung eines Hybridraketentriebwerkes. Other, Technische Universität Braunschweig. Volltext nicht online.
Wolf, Christian and You, Yancheng and Hörnschemeyer, R. and Lüdeke, Heinrich and Hannemann, Volker (2013) Base-flow sensitivity of a generic rocket forbody towards small freestream angles. In: Progress in Flight Physics Eucass Book Series, 5 (6). Torus Press. pp. 169-190. ISBN 978-2-7598-0877-9. 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, 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.
Wolfram, Jeremy (2004) Implementierung einer modularen Auswertesoftware für die Versuchsauswertung am Hochenthalpiekanal Göttingen. Diploma, Berufsakademie Mannheim. Volltext nicht frei.
Wollenhaupt, Birk (2007) Turbulenzmodellierung mit dem DLR TAU Verfahren. Diploma, Universität Stuttgart. Volltext nicht online.
Wucherpfennig, Jens and Schröder, Andreas and Martinez-Schramm, Jan (2009) DLR-Forscher machen Hyperschall sichtbar. [Other] Volltext nicht online.
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. 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, 97 (2), pp. 1-7. EPLA. 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). pp. 1-12. 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.
You, Yancheng and Oßwald, Kai and Lüdeke, Heinrich and Hannemann, Volker (2011) Numerical Study of the Subsonic Base Flow with a Side Support. Fourth Symposium on Hybrid RANS-LES Methods, 28.-30. Sep. 2011, Peking, China. Volltext nicht online.
You, Yancheng and Oßwald, Kai and Lüdeke, Heinrich and Hannemann, Volker (2012) Numerical Study of the Subsonic Base Flow with a Side Support. In: Progress in Hybrid RANS-LES Modelling Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 117. Springer Verlag. pp. 427-437. ISBN 978-3-642-31817-7. ISSN 1612-2909 Volltext nicht online.

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