Items where Subject is "Institute for Aerodynamics and Flow Technology > Spacecraft, GO"

Institutes and Facilities (115060)
- Institute for Aerodynamics and Flow Technology (1730)
  - Spacecraft, GO (195)

Jump to: B | C | D | E | F | G | H | J | K | L | M | N | O | P | R | S | T | V | W | Z

Number of items at this level: 195.

B

Banuti, Daniel and Grabe, Martin and Hannemann, Klaus (2019) Flow characteristics of monopropellant micro-scale planar nozzles. Aerospace Science and Technology, 86, pp. 341-350. Elsevier. doi: 10.1016/j.ast.2018.11.057. ISSN 1270-9638. Volltext nicht online.

Banuti, Daniel and Hannemann, Volker and Hannemann, Klaus and Weigand, B. (2016) An efficient multi-fluid-mixing model for real gas reacting flows in liquid propellant rocket engines. Combustion and Flame, 168, pp. 98-112. Elsevier. doi: 10.1016/j.combustflame.2016.03.029. ISSN 0010-2180. Volltext nicht frei.

Beinke, Scott and Banuti, Daniel and Hardi, Justin and Karl, Sebastian and Oschwald, Michael and Dally, Bassam (2017) Modelling of a Coaxial LOx/GH2 Injection Element Under High Frequency Transverse Acoustic Velocity Forcing. 16th International Conference on Numerical Combustion, 3. - 5. Apr. 2017, Orlando, USA. Volltext nicht online.

Beinke, Scott and Banuti, Daniel and Hardi, Justin and Oschwald, Michael and Dally, Bassam (2019) Modeling of a Coaxial Liquid Oxygen/Gaseous Hydrogen Injection Element Under High-Frequency Acoustic Disturbances. In: Progress in Propulsion Physics Torus Press. pp. 273-294. doi: 10.1051/eucass/201911225. ISBN 978-5-94588-228-7. ISSN 2493-3503.

Beinke, Scott and Hardi, Justin and Banuti, Daniel and Karl, Sebastian and Dally, Bassam and Oschwald, Michael (2020) Experimental and numerical study of transcritical oxygen-hydrogen rocket flame response to transverse acoustic excitation. Proceedings of the Combustion Institute. Elsevier. doi: 10.1016/j.proci.2020.05.027. ISSN 1540-7489.

Beinke, Scott and Hardi, Justin and Oschwald, Michael and Banuti, Daniel T. and Karl, Sebastian and Dally, Bassam D. (2018) Experimental and numerical study of Oxygen-hydrogen rocket flame Response to transverse acoustic excitation. In: Proceedings 2018 Joint Propulsion Conference. AIAA/SAE/ASEE Joint Propulsion Conference 2018, 9. - 11. Jul. 2018, Cincinnati (OH), USA. doi: 10.2514/6.2018-4467. Volltext nicht online.

C

Christopher, N. and Hickey, Jean-Pierre and De Graaf, S. and Bellan, J. and Bushe, W. K: and Devaud, C. and Hannemann, Volker (2017) Probability Density Function Characterization for Conditional Source-term Estimation in High-Pressure Combustion. [Other]

D

De Graaf, S. and Taylor, S. R. and Hendra, G. R. and Christopher, N. and Bushe, W. K. and Devaud, C. and Hannemann, Volker and Hickey, Jean-Pierre (2017) Numerical Simulation of High-Pressure Combustion using Conditional Source-term Estimation. [Other]

Dittert, Christian and Kütemeyer, Marius and Kuhn, Markus and Wagner, Alexander (2018) Process Optimization of Ceramic Matrix Composites for Ultrasonically Absorptive TPS Material. In: 2018 Joint Thermophysics and Heat Transfer Conference. AIAA. 2018 Joint Thermophysics and Heat Transfer Conference, 25.-29.Jun.2018, Atlanta, Georgia. Volltext nicht online.

Dumont, Etienne and Ecker, Tobias and Chavagnac, Christophe and Witte, Lars and Windelberg, Jens and Klevanski, Josef and Giagkozoglou, Sofia (2018) CALLISTO - Reusable VTVL launcher first stage demonstrator. Space Spropulsion Conference 2018, 14.-18. Mai 2018, Sevilla, Spanien.

Dumont, Etienne and Ishimoto, Shinji and Tatiossian, Pascal and Klevanski, Josef and Reimann, Bodo and Ecker, Tobias and Witte, Lars and Riehmer, Johannes and Sagliano, Marco and Giagkozoglou, Sofia and Petkov, Ivaylo and Rotärmel, Waldemar and Schwarz, René and Seelbinder, David and Markgraf, Markus and Sommer, Jan and Pfau, Dennis and Martens, Hauke (2019) CALLISTO: a Demonstrator for Reusable Launcher Key Technologies. 32nd ISTS, 17.21. Jun. 2019, 32nd ISTS.

Dumont, Etienne and Ishimoto, Shinji and Tatiossian, Pascal and Klevanski, Josef and Reimann, Bodo and Ecker, Tobias and Witte, Lars and Riehmer, Johannes and Sagliano, Marco and Giagkozoglou, Sofia and Petkov, Ivaylo and Rotärmel, Waldemar and Schwarz, René and Seelbinder, David and Markgraf, Markus and Sommer, Jan and Pfau, Dennis and Martens, Hauke (2021) CALLISTO: A Demonstrator for Reusable Launcher Key Technologies. Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan, 19 (1), pp. 106-115. JSASS. doi: 10.2322/tastj.19.106. ISSN 1884-0485. Volltext nicht online.

Dumont, Etienne and Stappert, Sven and Ecker, Tobias and Wilken, Jascha and Karl, Sebastian and Krummen, Sven and Sippel, Martin (2017) Evaluation of Future Ariane Reusable VTOL Booster stages. In: Proceedings of the International Astronautical Congress, IAC. 68th International Astronautical Congress, 25-29 September 2017, Adelaide, Australia.

E

Ecker, Tobias and Karl, Sebastian and Dumont, Etienne and Stappert, Sven and Krause, Daniel (2017) A Numerical Study on the Thermal Loads During a Supersonic Rocket Retro-Propulsion Maneuver. In: 53nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016. 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 10.-12. Juni 2017, Atlanta, USA. doi: 10.2514/6.2017-4878. Volltext nicht frei.

Ecker, Tobias and Karl, Sebastian and Dumont, Etienne and Stappert, Sven and Krause, Daniel (2019) Numerical Study on the Thermal Loads During a Supersonic Rocket Retropropulsion Maneuver. Journal of Spacecraft and Rockets, 57 (1), pp. 131-146. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.A34486. ISSN 0022-4650. Volltext nicht online.

Ecker, Tobias and Karl, Sebastian and Hannemann, Klaus (2017) Modeling of Aluminum Particle Combustion in Solid Rocket Combustion Chambers. 53rd AIAA/SAE/ASEE Joint Propulsion Conference, 10.-12. Juni 2017, Atlanta, USA. Volltext nicht frei.

Ecker, Tobias and Karl, Sebastian and Hannemann, Klaus (2019) Combustion Modeling in Solid Rocket Motor Plumes. In: 17th International Conference on Numerical Combustion. 17th International Conference on Numerical Combustion, 6.-8. Mai 2019, Aachen. Volltext nicht online.

Ecker, Tobias and Karl, Sebastian and Hannemann, Klaus (2019) Combustion modeling in solid rocket motor plumes. In: 8th European Conference for Aeronautics and Space Sciences 2019. 8th European Conference for Aeronautics and Space Sciences 2019, 1 - 4 Juli, 2019, Madrid, Spanien. Volltext nicht frei.

Ecker, Tobias and Zilker, Franziska and Dumont, Etienne and Karl, Sebastian and Hannemann, Klaus (2018) Aerothermal Analysis of Reusable Launcher Systems during Retro-Propulsion Reentry and Landing. Space Propulsion Conference 2018, 14.-18. Mai 2018, Sevilla, Spanien.

F

Fechter, Stefan and Horchler, Tim and Karl, Sebastian and Hannemann, Klaus (2019) Numerical simulation of cryogenic flows under high-pressure conditions. In: 17th International Conference on Numerical Combustion 2019. 17th International Conference on Numerical Combustion 2019, 6.-8. Mai 2019, Aachen, Deutschland. Volltext nicht online.

Fechter, Stefan and Horchler, Tim and Karl, Sebastian and Hannemann, Klaus (2019) Investigation of RANS turbulence models for cryogenic rocket combustion chambers. In: 8th European Conference for Aeronautics and Space Sciences (EUCASS) 2019. 8th European Conference for Aeronautics and AeroSpace Sciences (EUCASS), 01.-04. Juli 2019, Madrid, Spanien. Volltext nicht frei.

Fechter, Stefan and Horchler, Tim and Karl, Sebastian and Hannemann, Klaus (2020) Generic test case to understand cryogenic methane combustion dynamics. In: NICFD 2020, pp. 1-6. 3nd International Seminar on Non-Ideal Compressible-Fluid Dynamics for Propulsion & Power, 29.-30. Okt. 2020, Delft, Niederlande. Volltext nicht frei.

Fechter, Stefan and Horchler, Tim and Karl, Sebastian and Hannemann, Klaus and Suslov, Dmitry and Hardi, Justin and Oschwald, Michael (2018) Numerical simulation of cryogenic flows in rocket combustion chambers. 2ND INTERNATIONAL SEMINAR ON NON-IDEAL COMPRESSIBLE-FLUID DYNAMICS FOR PROPULSION & POWER, 04.-05.10.2018, Bochum, Deutschland. Volltext nicht online.

Fechter, Stefan and Horchler, Tim and Karl, Sebastian and Hannemann, Klaus and Suslov, Dmitry and Hardi, Justin and Oschwald, Michael (2020) Efficient handling of cryogenic equation of state for the simulation of rocket combustion chambers. In: Non-Ideal Compressible Fluid Dynamics for Propulsion and Power Lecture Notes in Mechanical Engineering. Springer, Cham. pp. 19-30. doi: 10.1007/978-3-030-49626-5_2. ISBN 978-3-030-49626-5. ISSN 2195-4364. Volltext nicht online.

Fechter, Stefan and Karl, Sebastian and Hannemann, Klaus (2018) Influence of non-linear mixing effects onto flow and heat transfer in rocket combustion chambers. Space Propulsion Conference 2018, 14.-18. Mai 2018, Sevilla, Spanien. Volltext nicht online.

Fechter, Stefan and Karl, Sebastian and Hannemann, Volker and Hannemann, Klaus (2017) Simulation of LOx/GH2 single coaxial injector at high pressure conditions. AIAA/SAE/ASEE Joint Propulsion Conference, AIAA Propulsion and Energy Forum, 10.-12. Juli 2017, Atlanta, GA, USA. doi: 10.2514/6.2017-4765. Volltext nicht frei.

G

Grabe, Martin (2017) DLR vacuum test facilities for thruster plume investigation. [Other] Volltext nicht online.

Grabe, Martin (2017) Modellierung der Treibstrahl-Wechselwirkung von Kleintriebwerken unter Hochvakuumbedingungen. Dissertation. DLR-Forschungsbericht. DLR-FB-2017-42. Volltext nicht online.

Grabe, Martin (2016) STG-CT: High-vacuum plume test facility for chemical thrusters. Journal of Large-Scale Research Facilities JLSRF, 2 (A86), pp. 1-5. Forschungszentrum Jülich GmbH. doi: 10.17815/jlsrf-2-139. ISSN 2364-091X.

Grabe, Martin (2017) Plume Flow and Impingement Research at DLR Göttingen. European Contamination modelling workshop, 08. Feb. 2017, Bremen, Deutschland. Volltext nicht online.

Grabe, Martin and Dettleff, Georg and Hepp, Christian and Hannemann, Klaus (2018) Effect of Source Geometry on Fully Expanding Free Jets. In: AIP Conference Proceedings, 2132 (030001). American Institute of Physics Inc.. 31st International Symposium on Rarefied Gas Dynamics 2018, 23.-27. Jul. 2018, Glasgow, Scotland. doi: 10.1063/1.5119526. ISBN 978-073541874-5. ISSN 0094243X. Volltext nicht online.

Grabe, Martin and Soares, Carlos E. (2019) Status and Future of Research on Plume Induced Contamination. In: Proceedings of the International Astronautical Congress, IAC. IAF. 70th International Astronautical Congress, 21.–25. Okt. 2019, Washington, USA.

Guédron, Sylvain and Ishimoto, Shinji and Dumont, Etienne and Tatiossian, Pascal and Chavagnac, Christophe and Desmariaux, Jean and Monchaux, David and Frenoy, Olivier and Cliquet Moreno, Elisa and Deremaux, Carole and Lidon, Norbert and Cesco, Nathalie and Witte, Lars and Sagliano, Marco and Seelbinder, David and Klevanski, Josef and Ecker, Tobias and Reimann, Bodo and Riehmer, Johannes and Ertl, Moritz and Krummen, Sven (2020) CALLISTO DEMONSTRATOR: Focus on system aspects. In: 71st International Astronautical Congress. 71th International Astronautical Congress, 12.-14. October 2020, online.

Génin, Chloé and Stark, Ralf and Karl, Sebastian (2017) Shock System Deformation in High Mach Number Rocket Nozzles, No. 425. In: Proceedings of the 31st International Symposium on Shock Waves (ISSW31). 31st International Symposium on Shock Waves (ISSW31), 10. - 14. Jul. 2017, Nagoya, Japan. Volltext nicht online.

Gülhan, Ali and Esser, Burkard and Koch, Uwe and Fischer, Michael and Magens, Eggert and Hannemann, Volker (2017) Characterization of High-Enthalpy-Flow Environment for Ablation Material Tests Using Advanced Diagnostics. AIAA Journal, 56 (3), pp. 1072-1084. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J056312. ISSN 0001-1452. Volltext nicht online.

Gülhan, Ali and Kallenbach, Alexander and Bussler, Leonid and Petkov, Ivaylo and Zuber, Christian and Klopsch, Linda and Steffens, Lars and Liebisch, Martin and Poppe, Georg and Kobald, Mario and Ecker, Tobias and May, Stefan and Rüttgers, Alexander and Klingenberg, Florian (2019) ATEK (Antriebstechnologien und Komponenten für Trägersysteme). Project Report. Volltext nicht frei.

H

Hannemann, Klaus (2017) Hypersonic Research in the High Enthalpy Shock Tunnel Göttingen. Seminar, 03. Jun. 2017, Hong Kong, China. Volltext nicht online.

Hannemann, Klaus (2017) Launch Vehicle Propulsion and High Enthalpy Hypersonic Aerothermodynamics – Selected Research Activities at the DLR Spacecraft Department. Seminar, Department of Mechanical and Aerospace Engineering, 05. Jun. 2017, Hong Kong, China. Volltext nicht online.

Hannemann, Klaus (2017) Space Propulsion. Invited Lecture, 03. März 2017, China. Volltext nicht online.

Hannemann, Klaus (2017) Re-entry Aerothermodynamics. Invited Lecture, 03. März 2017, China. Volltext nicht online.

Hannemann, Klaus (2017) Numerische Modellierung von Raketenschubkammern. 5. DLR_Summer_School "Raumfahrtantriebe", 13. Sep. 2017, Lampoldshausen, Deutschland. Volltext nicht online.

Hannemann, Klaus (2018) High Enthalpy Hypersonic Aerothermodynamics and Space Propulsion Research at the DLR Spacecraft Department Göttingen. Seminar, Tokyo Metropolitan University, Japan, 9. April 2018, Tokyo. Volltext nicht online.

Hannemann, Klaus (2018) High Enthalpy Hypersonic Aerothermodynamics and Space Propulsion Research at the DLR Spacecraft Department Göttingen. Seminar, Japan Aerospace Exploration Agency (JAXA) 2018, 9. April 2018, Tokyo, Japan. Volltext nicht online.

Hannemann, Klaus (2018) Hypersonic and Space Propulsion Research at the DLR Spacecraft Department Göttingen. Seminar, China Aerodynamics Research & Development Center (CARDC), 21. Juli 2018, Mianyang. Volltext nicht online.

Hannemann, Klaus (2018) Free Flight Force Measurement Technique. In: Summer School on Advanced Experimental Diagnostic Technology 2018. Summer School on Advanced Experimental Diagnostic Technology 2018, 23.-27. Juli 2018, Xiamen, China. Volltext nicht online.

Hannemann, Klaus (2018) High Enthalpy Short Duration Testing - Free Piston Driven Shock Tunnels. In: Summer School on Advanced Experimental Diagnostic Technology 2018. Summer School on Advanced Experimental Diagnostic Technology 2018, 23.-27. Juli 2018, Xiamen, China. Volltext nicht online.

Hannemann, Klaus (2018) Aerothermodynamic Ground Base Testing - Fundamentals. In: Summer School on Advanced Experimental Diagnostic Technology 2018. Summer School on Advanced Experimental Diagnostic Technology 2018, 23.-27. Juli 2018, Xiamen, China. Volltext nicht online.

Hannemann, Klaus (2018) Numerische Modellierung von Raketenschubkammern. 6. DLR_Summer_School Raumfahrtantriebe, 27. August - 7. September 2018, Lampoldshausen, Deutschland. Volltext nicht online.

Hannemann, Klaus (2018) Advance of Scramjet Operating Mode Comprehension based on Shock Tunnel Experiments and Numerical Modelling. In: 69th International Astronautical Congress (IAC). 69th International Astronautical Congress (IAC), 1.-5. Oktober 2018, Bremen, Deutschland. Volltext nicht online.

Hannemann, Klaus (2019) DLR Spacecraft Department Göttingen - Research Fields, Infrastructure and selected Research Activities. Lunchtime Seminar, Centre for Hypersonics, School of Mechanical and Mining Engineering, 17. Januar 2019, Brisbane, Australia. Volltext nicht online.

Hannemann, Klaus (2019) High Enthalpy Hypersonic Aerothermodynamics and Space Propulsion Research at the DLR Spacecraft Department Göttingen. USQ Toowoomba, Seminar 2019, 13. Februar 2019, Toowoomba, Australien. Volltext nicht online.

Hannemann, Klaus (2019) Aerothermodynamics and Space Propulsion Research at the DLR Spacecraft Department Göttingen. UNSW Canberra, Seminar 2019, 21. März 2019, Canberra, Australia. Volltext nicht online.

Hannemann, Klaus (2019) High Enthalpy Shock Tunnel Testing and Numerical Analysis of Hypersonic Airbreathing Propulsion Configurations. 1st Brazilian School on Hypersonic Airbreathing Propulsion (scramjet technology), 13.-17.5.2019, Natal, Brasilien. Volltext nicht online.

Hannemann, Klaus (2019) Hypersonic Airbreathing Propulsion Testing in Shock Tunnels Including Numerical Analysis. Summer School on Numerical Simulation and Measurement of Hypersonic Gas Dynamics and Combustion, 22.-26. Juli 2019, Xiamen, China. Volltext nicht online.

Hannemann, Klaus (2019) Numerische Modellierung von Raketenschubkammern. 7. DLR_Summer_School „Raumfahrtantriebe“, 02. September – 13. September 2019, Lampoldshausen, Deutschland. Volltext nicht online.

Hannemann, Klaus (2019) Research in Space Transportation at the German Aerospace Center: Selected Topics. 4th REST Modelling Workshop 2019, 20.-21. November 2019, Lampoldshausen, Deutschland. Volltext nicht online.

Hannemann, Klaus (2019) Analyse heißer Hyperschallströmungen in Hochenthalpie-Stoßkanälen. Seminar Plasmaphysik, 17.12.2019, Darmstadt, Deutschland. Volltext nicht online.

Hannemann, Klaus (2020) Study of Hot Hypersonic Flows in High-Enthalpy Shock Tunnels. 6th National Symposium on Shock Waves (NSSW2020), 26 - 28 February 2020, Chennai, India. Volltext nicht online.

Hannemann, Klaus (2020) DLR Spacecraft Department Göttingen: High Enthalpy Hypersonic Aerothermodynamics and Space Propulsion Research. Seminar Department of Aerospace Engineering Indian Institute of Technology - Kanpur (IITK), 24. Februar 2020, Kanpur, India. Volltext nicht online.

Hannemann, Klaus (2020) Shock Tunnel Ground Based Testing and Numerical Modelling of Scramjet Flow Paths. International Workshop on Energy, Environment, and Multiphase Flows, IWEEM-2020, February 24-26, 2020, Kanpur, India. Volltext nicht online.

Hannemann, Klaus and Hepp, Christian and Grabe, Martin and Hannemann, Volker (2019) Numerical Analysis of Re-entry Configuration Aerodynamics in the Near Continuum Rarefied Flow Regimes. In: Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019), pp. 1591-1601. Research Publishing Singapore. 32nd International Symposium on Shock Waves, 14.-19. Juli 2019, Singapore. doi: 10.3850/978-981-11-2730-4_0306-cd. ISBN 978-981-11-2730-4. Volltext nicht online.

Hannemann, Klaus and Hepp, Christian and Winkler, Violetta and Hannemann, Volker and Schlegat, Thomas and Grabe, Martin (2018) Numerical and Experimental Analysis of Rarefaction Effects on Aerodynamic Coefficients of a Slender Re-entry Vehicle. In: International Conference on High-Speed Vehicle Science and Technology (HiSST). International Conference on High-Speed Vehicle Science and Technology (HiSST), 26.–29. November 2018, Moskau, Russland. Volltext nicht online.

Hannemann, Klaus and Itoh, Katsuhiro and Mee, D. J. and Hornung, Hans G. (2016) Free Piston Shock Tunnels HEG, HIEST, T4 and T5. In: Experimental Methods of Shock Wave Research Shock Wave Science and Technology Reference Library, 9. Springer Verlag, Cham. pp. 181-264. doi: 10.1007/978-3-319-23745-9_7. ISBN 978-3-319-23744-2. Volltext nicht online.

Hannemann, Klaus and Martinez Schramm, Jan and Karl, Sebastian and Laurence, Stuart Jon (2017) Enhancement of Free Flight Force Measurement Technique for Scramjet Engine Shock Tunnel Testing. 21st AIAA International Space Planes and Hypersonic Systems and Technologie Conference, 06.-09. März 2017, Xiamen, China. Volltext nicht online.

Hannemann, Klaus and Martinez Schramm, Jan and Riedl, Philipp and Hannemann, Volker and Oblapenko, Georgii (2018) Thermal Non-equilibrium Effects on Spherically Blunted Cone Flows. 12th International Workshop on Shock Tunnel Technology, 12. - 13.April 2018, Kakuda, Japan. Volltext nicht online.

Hannemann, Klaus and Martinez Schramm, Jan and Wagner, Alexander and Ponchio Camillo, Giannino (2018) The High Enthalpy Shock Tunnel Göttingen of the German Aerospace Center (DLR). Journal of Large-Scale Research Facilities JLSRF, 4 (A133), pp. 1-14. Forschungszentrum Jülich GmbH. doi: 10.17815/jlsrf-4-168. ISSN 2364-091X.

Hannemann, Volker (2019) TAU extensions for spacecraft applications. TAU Anwenderschulung, 3.-4. Sept. 2019, Filton, UK. Volltext nicht online.

Hepp, Christian and Grabe, Martin and Hannemann, Klaus (2017) Aerodynamic coefficients computed for a generic sharp-edged re-entry configuration. Clean Space Industrial Days & AeroThermoDynamics Design for Demise Workshop, 26. Okt. 2017, Noordwijk, Niederlande. Volltext nicht online.

Hepp, Christian and Grabe, Martin and Hannemann, Klaus (2019) Non-equilibrium parameter for a hybrid Fokker-Planck/ DSMC scheme. In: AIP Conference Proceedings, 2132 (070002). AIP Publishing. 31st International Symposium on Rarefied Gas Dynamics 2018, 23.-27. Juli 2018, Glasgow, Scotland. doi: 10.1063/1.5119556. ISBN 978-073541874-5. ISSN 0094243X.

Hepp, Christian and Grabe, Martin and Hannemann, Klaus (2019) Modeling of rarefied gas flows with particle methods. Seminar / University of New Mexico - Mechanical Engineering Department, 27. Sept 2019, Albuquerque. Volltext nicht frei.

Hepp, Christian and Grabe, Martin and Hannemann, Klaus (2020) A kinetic Fokker–Planck approach for modeling variable hard-sphere gas mixtures. AIP Advances, 10 (8), 085219-1. American Institute of Physics (AIP). doi: 10.1063/5.0017289. ISSN 2158-3226.

Hepp, Christian and Grabe, Martin and Hannemann, Klaus (2020) Master equation approach for modeling diatomic gas flows with a kinetic Fokker-Planck algorithm. Journal of Computational Physics, 418 (109638). Elsevier. doi: 10.1016/j.jcp.2020.109638. ISBN 0021-9991. ISSN 0021-9991. Volltext nicht online.

Hepp, Christian and Grabe, Martin and Hannemann, Klaus (2020) A kinetic Fokker-Planck approach to model hard-sphere gas mixtures. Physics of Fluids, 32 (2), pp. 1-18. American Institute of Physics (AIP). doi: 10.1063/1.5141909. ISSN 1070-6631.

Hepp, Christian and Grabe, Martin and Klaus, Hannemann (2019) Modeling of internal energy modes within a kinetic Fokker-Planck algorithm. DSMC 2019 Conference, 22.-25. Sep. 2019, Santa Fe. Volltext nicht frei.

Hepp, Christian and Grabe, Martin and Schlegat, Thomas and Hannemann, Klaus (2017) DSMC-Simulation einer Wiedereintrittskonfiguration in verdünnter Hyperschall-Strömung. 18. STAB-Workshop, 07.-08. Nov. 2017, Göttingen, Deutschland. Volltext nicht online.

Hilfer, Michael and Martinez Schramm, Jan and Isberner, Leonard (2019) Time Response Calibration of Ultra-Fast Temperature Sensitive Paints for the Application in High Temperature Hypersonic Flows. In: 7th Japanese-German Joint Seminar – Molecular Imaging Technology for Interdisciplinary Research – (O-12). 7th Japanese-German Joint Seminar – Molecular Imaging Technology for Interdisciplinary Research –, 17. - 19. Sept. 2019, Hokkaido University, Sapporo, Hokkaido 060-8628, Japan. Volltext nicht online.

Hoppe, Theresa and Hepp, Christian and Hannemann, Volker and Hannemann, Klaus (2019) Comparison of Slip-flow Boundary Conditions for Perfect Gas Hypersonic Flow Simulations. In: 19. STAB Workshop. 19. STAB Workshop, 5.-6. Nov. 2019, Göttingen, Deutschland. Volltext nicht online.

Horchler, Tim and Armbruster, Wolfgang and Hardi, Justin and Karl, Sebastian and Hannemann, Klaus and Gernoth, Andreas and De Rosa, Marco (2018) Modeling combustion chamber acoustics using the DLR TAU code. In: Space Propulsion Conference 2018. Space Propulsion Conference 2018, 14.-18. Mai 2018, Sevilla, Spanien. Volltext nicht frei.

Horchler, Tim and Fechter, Stefan and Hannemann, Klaus (2018) Validation of the DLR TAU Code for Scale-Resolving Combustion Simulations. Space Propulsion 2018, 14.-18. Mai 2018, Sevilla, Spanien. Volltext nicht online.

Horchler, Tim and Fechter, Stefan and Karl, Sebastian and Hannemann, Klaus (2019) Comparison of Detailed Chemistry and Flamelet Combustion Modeling in a H2/LOx Subscale Combustion Chamber. In: 17th International Conference on Numerical Combustion 2019. 17th International Conference on Numerical Combustion 2018, 6.-8. Mai 2019, Aachen, Deutschland. Volltext nicht online.

Horchler, Tim and Fechter, Stefan and Karl, Sebastian and Hannemann, Klaus (2019) Recent Developments in the DLR TAU Code for Combustion Chamber Modeling. 15th REST Scientific Workshop, 22. Januar 2019, Rouen, Frankreich. Volltext nicht online.

Horchler, Tim and Fechter, Stefan and Karl, Sebastian and Hannemann, Klaus (2019) A Timescale-Augmented Spalart-Allmaras Turbulence Model for Flamelet Combustion Applications. In: 8th European Conference for Aeronauticas and Aerospace Sciences (EUCASS). 8th European Conference for Aeronauticas and Aerospace Sciences (EUCASS), 1. - 4. Juli 2019, Madrid, Spanien. Volltext nicht frei.

Horchler, Tim and Karl, Sebastian and Hannemann, Klaus and Gernoth, Andreas and De Rosa, M. (2018) Modeling Combustion Chamber Acoustics Using the DLR TAU Code. In: Space Propulsion 2018. Space Propulsion 2018, 14.-18. Mai 2018, Sevilla, Spanien. Volltext nicht online.

Horchler, Tim and Oßwald, Kai and Hannemann, Volker and Hannemann, Klaus (2018) Hybrid RANS-LES Study of Transonic Flow in the Wake of a Generic Space Launch Vehicle. In: Progress in Hybrid RANS-LES Modelling, 137, pp. 291-300. Springer, Cham. Progress in Hybrid RANS-LES Modelling. HRLM 2016., 26.-28. Sep. 2016, Straßburg, Frankreich. doi: 10.1007/978-3-319-70031-1_24. ISBN 978-3-319-70030-4. ISSN 1612-2909. Volltext nicht frei.

Horchler, Tim and van Schyndel, Jan and Fechter, Stefan and Zhukov, Victor / V. P. and Hannemann, Klaus and Oschwald, Michael (2019) Simulation of the HF-10 Test Case using the DLR TAU Code. 4th REST Workshop on Combustion Instability Modeling 2019, 20.-21. Nov. 2019, Lampoldshausen, Deutschland. Volltext nicht online.

Hornung, Hans G. and Martinez Schramm, Jan and Hannemann, Klaus (2019) Hypersonic flow over spherically blunted cone capsules for atmospheric entry, Part I: The sharp cone and the sphere. Journal of Fluid Mechanics, 871, pp. 1097-1116. Cambidge University Press. doi: 10.1017/jfm.2019.342. ISSN 0022-1120. Volltext nicht online.

Hoste, Jimmy-John and Fechter, Stefan and Karl, Sebastian and Hannemann, Klaus (2020) Study of a supersonic reacting wall jet with a variable turbulent Prandtl and Schmidt number approach. Aerospace Science and Technology, 106 (106070). Elsevier. doi: 10.1016/j.ast.2020.106070. ISSN 1270-9638. Volltext nicht online.

Huismann, Immo and Fechter, Stefan and Leicht, Tobias (2020) HyperCODA -- Extension of Flow Solver CODA to Hypersonic Flows. In: HyperCODA -- Extension of Flow Solver CODA Towards Hypersonic Flows, XIII. Springer International Publishing. STAB-Symposium 2020, Germany. Volltext nicht frei.

J

Jun, Eunji (2019) Cubic Fokker-Planck-DSMC hybrid method for diatomic rarefied gas flow through a slit and an orifice. Vacuum, 159, pp. 125-133. Elsevier. doi: 10.1016/j.vacuum.2018.10.028. ISSN 0042-207X. Volltext nicht online.

Jun, Eunji and Gorji, M. Hossein and Grabe, Martin and Hannemann, Klaus (2018) Assessment of the cubic Fokker-Planck-DSMC hybrid method for hypersonic rarefied flows past a cylinder. Computers & Fluids, 168, pp. 1-13. Elsevier. doi: 10.1016/j.compfluid.2018.03.059. ISSN 0045-7930. Volltext nicht online.

Jun, Eunji and Grabe, Martin and Hannemann, Klaus (2018) Cubic Fokker-Planck-DSMC hybrid method for diatomic gas flow through a slit. In: AIP Conference Proceedings, 2132 (070001). American Institute of Physics Inc.. 31st International Symposium on Rarefied Gas Dynamics 2018, 23.-27. Jul. 2018, Glasgow, Scotland. doi: 10.1063/1.5119555. ISBN 978-073541874-5. ISSN 0094243X. Volltext nicht online.

Jun, Eunji and Grabe, Martin and Hannemann, Klaus (2018) Cubic Fokker-Planck Method for Rarefied Monatomic Gas Flow through a Slit and an Orifice. Computers & Fluids, 175, pp. 199-213. Elsevier. doi: 10.1016/j.compflui.2018.08.028. ISSN 0045-7930. Volltext nicht online.

K

Karl, Sebastian and Hickey, Jean Pierre and Lacombe, Francis (2017) Reynolds Stress Models for Shock - Turbulence lnteraction. 31 st International Symposium on Shock Waves, 09.-14.Juli 2017, Nagoya, Japan. Volltext nicht online.

Karl, Sebastian and Martinez Schramm, Jan and Hannemann, Klaus (2019) Post-Test Analysis of the LAPCAT-II Subscale Scramjet. In: Proceedings of the 1st International Conference on High-Speed Vehicle Science and Technology. 1st International Conference on High-Speed Vehicle Science Technology, 26.-29. Nov. 2018, Moskau, Russland. Volltext nicht online.

Karl, Sebastian and Martinez Schramm, Jan and Hannemann, Klaus (2020) Post-test analysis of the LAPCAT-II subscale scramjet. CEAS Space Journal, 12 (3), pp. 385-395. Springer. doi: 10.1007/s12567-020-00307-7. ISSN 1868-2502.

Karl, Sebastian and Steelant, Johan (2017) Cross-Flow Phenomena in Streamline Traced Hypersonic Intakes. Journal of Propulsion and Power, 34 (2), pp. 449-459. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514. ISSN 0748-4658. Volltext nicht online.

Keiderling, David (2017) THE DLR TAU-CODE FOR CRYOGENIC FLUID BEHAVIOUR. ArianeGroup R&T PHD DAYS ’17 GERMANY, 12. Okt. 2017, Bremen, Deutschland. Volltext nicht frei.

Kirchheck, Daniel and Marwege, Ansgar and Klevanski, Josef and Riehmer, Johannes and Gülhan, Ali and Karl, Sebastian and Gloth, Oliver (2019) Validation of Wind Tunnel Test and CFD Techniques for Retro-propulsion (RETPRO): Overview on a Project within the Future Launchers Preparatory Programme (FLPP). International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions & Engineering (FAR), 30. Sep. - 3. Okt. 2019, Monopoli, Italien.

Klevanski, Josef and Ecker, Tobias and Riehmer, Johannes and Reimann, Bodo and Dumont, Etienne and Chavagnac, Christophe (2018) Aerodynamic Studies in Preparation for CALLISTO - Reusable VTVL Launcher First Stage Demonstrator. 69th International Astronautical Congress (IAC), 1-5 October 2018, Bremen, Germany.

L

Lacombe, Francis and Roy, Subhajit and Sinha, Krishnendu and Karl, Sebastian and Hickey, Jean-Pierre (2020) Characteristic Scales in Shock–Turbulence Interaction. AIAA Journal, pp. 1-7. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J059499. ISSN 0001-1452. Volltext nicht online.

Laurence, Stuart Jon and Butler, C. S. and Hannemann, Klaus and Martinez Schramm, Jan (2017) Force and Moment Measurements on a Free-Flying Capsule in a Shock Tunnel. Journal of Spacecraft and Rockets, 55 (2), pp. 403-414. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.A33820. ISSN 0022-4650. Volltext nicht online.

Laurence, Stuart Jon and Ozawa, Hiroshi and Martinez Schramm, Jan and Hannemann, Klaus (2018) Time-resolved Temperature Sensitive Paint Measurements on a Hypersonic Intake Ramp. In: 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 2018. 22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference, 17.-19. Sep. 2018, Orlando, Florida, USA. doi: 10.2514/6.2018-5383. ISBN 978-162410577-7. Volltext nicht online.

Leroy, Benjamin (2017) Investigation of instability growth in a hypersonic boundary layer using Schlieren visualization. Master's. Volltext nicht online.

M

Marineau, Eric C. and Grossir, Guillaume and Wagner, Alexander and Leinemann, Madlen and Radespiel, Rolf and Tanno, Hideyuki and Wadhams, Tim P. and Chynoweth, B. C. and Schneider, S. P. and Wagnild, Ross M. and Casper, Katya M. (2018) Compilation and Analysis of Second-Mode Amplitudes on Sharp Cones in Hypersonic Wind Tunnels. In: AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting (210059). AIAA. AIAA Science and Technology Forum and Exposition (SciTech 2018), 08. -11. Jan. 2018, Kissimee, Florida USA. doi: 10.2514/6.2018-0349. ISBN ISBN: 978-162410524-1. Volltext nicht online.

Martinez Schramm, Jan (2018) Ultra-fast Temperature Sensitive Paints in the High Enthalpy Shock Tunnel Göttingen, HEG. In: 12th International Workshop on Shock Tube Technology, IWSTT. 12th International Workshop on Shock Tube Technology, IWSTT, 12.-13. Apr. 2018, Kakuda Space Center, Japan. Volltext nicht frei.

Martinez Schramm, Jan and Hannemann, Klaus (2017) Study of MHD Effects in the High-Enthalpy Shock Tunnel Göttingen (HEG) using a 30T Pulsed Magnet System. 31st International Symposium on Shock Waves, 09.-14. Juli 2017, Nagoya, Japan.

Martinez Schramm, Jan and Hannemann, Klaus (2019) SCRAMJET THRUST MEASUREMENTS IN A SHOCK TUNNEL USING A COMPLETELY FREE-FLIGHT AND A RESTRAINED FORCE MEASUREMENT SET-UP. International Society for Air Breathing Engines Congference, 22.-27.Sep.2019, Canberra, Australien. Volltext nicht online.

Martinez Schramm, Jan and Hannemann, Klaus and Hornung, Hans G. (2017) Shock Shape Transition on Spherically Blunted Conesin Hypersonic Flows. 31st International Symposium on Shock Waves (ISSW31), 09.-14. Juli 2017, Nagoya, Japan. Volltext nicht online.

Martinez Schramm, Jan and Hannemann, Klaus and Hornung, Hans G. (2019) Hypersonic non-equilibrium flow over spherically blunted cone capsules. In: Proceedings of the 32nd International Symposium on Shock Waves (ISSW32 2019), pp. 2503-2516. Research Publishing Singapore. 32nd International Symposium on Shock Waves, 14.-19. July 2019, Singapur. doi: 10.3850/978-981-11-2730-4_0455-cd. ISBN 978-981-11-2730-4. Volltext nicht online.

Martinez Schramm, Jan and Hilfer, Michael (2020) Time Response Calibration of Ultra-Fast Temperature Sensitive Paints for the Application in High Temperature Hypersonic Flows. In: 21st STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics, 142, pp. 143-152. Springer Nature. 21. STAB/DGLR Symposium 2018, 6.-7. Nov. 2018, Darmstadt. doi: 10.1007/978-3-030-25253-3_14. ISBN 978-3-030-25252-6. ISSN 1612-2909. Volltext nicht online.

Martinez Schramm, Jan and Luis, Diana (2020) Absorption Spectroscopy of NO in Hydrogen Combustion based on Heterodyne Techniques using Quantum Cascade Lasers. In: 22nd STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics XIII - Jahresbericht 2020, pp. 44-45. Springer Nature. 22. STAB/DGLR Symposium 2020, 15. Juli 2020, Göttingen. Volltext nicht online.

Martinez Schramm, Jan and Schmidt, Leni (2020) Application of Ultra-Fast Internal Temperature Sensitive Paints to a Hydrogen Combustion Flow. In: 22nd STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics XIII - Jahresbericht 2020, pp. 46-47. Springer Nature. 22. STAB/DGLR Symposium 2020, 15. Juli 2020, Göttingen. Volltext nicht online.

Marwege, Ansgar and Klevanski, Josef and Riehmer, Johannes and Kirchheck, Daniel and Karl, Sebastian and Bonetti, Davide and Vos, J. and Jevons, Matthew and Krammer, Anett and Carvalho, João (2019) Retro Propulsion Assisted Landing Technologies (RETALT): Current Status and Outlook of the EU Funded Project on Reusable Launch Vehicles. Paper presented at the 70th International Astronautical Congress, 21-25 October 2019, Washington D.C., United States, 21-25 October 2019, Washington D.C., United States.

Marwege, Ansgar and Riehmer, Johannes and Klevanski, Josef and Gülhan, Ali and Ecker, Tobias and Reimann, Bodo and Dumont, Etienne (2019) First Wind Tunnel Data of CALLISTO - Reusable VTVL Launcher First Stage Demonstrator. EUCASS 2019, 1. - 4. Juli, Madrid, Spanien.

May, Stefan and Karl, Sebastian and Bozic, Ognjan (2017) Development of an Eddy Dissipation Model for the use in Numerical Hybrid Rocket Engine Combustion Simulation. EUCASS 2017, 03.-06. Jul. 2017, Mailand, Italien. doi: 10.13009/EUCASS2017-157. Volltext nicht online.

Meyer, Lisa (2018) The DLR TAU-Code for Cryogenic Fluid Behavior: Modeling of a Free Surface. 6th German PHD Day, 05. Dez. 2018, Bremen. Volltext nicht online.

Meyer, Lisa (2019) Asymptotic Single and Multiple Scale Expansions in the Low Mach Number Limit for Real Fluids. 7th German PhD Day, 11. Dez. 2019, Bremen. Volltext nicht online.

Meyer, Lisa (2020) Low Mach Preconditioning Scheme for a Van der Waals-Gas. 8th German PhD Day Ariane Group, 09. Dez. 2020, Bremen. Volltext nicht online.

Meyer, Lisa and Keiderling, David and Hannemann, Klaus (2017) Numerical investigation of the wall contactangle influence on the movement of freesurfaces in launch vehicle upper stage tanks. 18. STAB-Workshop, 07.-08. Nov. 2017, Göttingen. Volltext nicht online.

N

Nagel, Aaron (2020) Modellierung von Teilchenwechselwirkung mit kryogenen Oberflächen im kinetischen DSMC Verfahren. Bachelor's, DLR Institut für Aerodynamik und Strömungstechnik Göttingen. Volltext nicht online.

Neumann, Andreas (2017) Update on Diagnostics for DLR's Electric Propulsion Test Facility. Procedia Engineering, 185, pp. 47-52. Elsevier. doi: 10.1016/j.proeng.2017.03.289. ISSN 1877-7058.

Neumann, Andreas (2017) STG-ET: DLR electric propulsion test facility. Journal of Large-Scale Research Facilities JLSRF, 3 (A108), pp. 1-6. Forschungszentrum Jülich GmbH. doi: 10.17815/jlsrf-3-156. ISSN 2364-091X.

Neumann, Andreas (2017) Das EU-Projekt LEOSWEEP: Weltraummüll-Entsorgung mit Ionenstrahlen. XXIV. Erfahrungsaustausch Oberflächentechnologie mit Plasma- und lonenstrahlprozessen, 07.-09. März 2017, Mühlleithen, Deutschland. Volltext nicht online.

Neumann, Andreas (2017) Update on Diagnostics for DLR's Electric Propulsion Test Facility. In: Procedia Engineering, 185, pp. 47-52. 6th Russian-German Conference on Electric Propulsion and Their Application, 28. Aug. - 02. Sep. 2016, Samara, Russland. doi: 10.1016/j.proeng.2017.03.289.

Neumann, Andreas (2018) STG-ET: DLR Electric Propulsion Test Facility. Journal of Large-Scale Research Facilities JLSRF. Forschungszentrum Jülich GmbH. doi: 10.17815/jlsrf-3-156-1. ISSN 2364-091X.

Neumann, Andreas (2019) Eine neue Schubwaage für die DLR EP-Testanlage. 26. Erfahrungsaustausch Oberflächentechnologie mit Plasma- und Ionenstrahlprozessen, Mühlleithen. Volltext nicht online.

Neumann, Andreas and Volkmar, Chris and Geile, Christopher and Hannemann, Klaus (2017) Mitigation of Detrimental Electric Thruster Force Measurement Effects. 35th International Electric Propulsion Conference, Georgia Institute of Technology, 08.-12. Okt. 2017, Atlanta, Georgia, USA. Volltext nicht online.

Neumann, Andreas and Volkmar, Chris and Geile, Christopher and Hannemann, Klaus (2018) Cryopumping of Different Noble Gases in DLRs Electric Propulsion Test Facility. In: 7th German-Russian Conference on Electric Propulsion and Their Application (RGCEP 2018). 7th German-Russian Conference on Electric Propulsion and Their Application (RGCEP 2018), 21.-26.10.2018, Rauischholzhausen, Deutschland. Volltext nicht online.

Neumann, Andreas and Volkmar, Chris and Hannemann, Klaus (2019) Challenges of Cryopumping EP-Propellants in DLR’s Electric Propulsion Test Facility. In: 36th International Electric Propulsion Conference 2019. 36th International Electric Propulsion Conference, 15-20 September 2019, Wien, Austria. Volltext nicht online.

Neumann, Horst and Harmann, Hans-Peter and Neumann, Andreas and Leiter, Hans (2016) German EP community – an overview on its activities inside the German Society for Aeronautics and Astronautics (DGLR) and presentation of the latest position paper. In: 6th Russian-German Conference on Electric Propulsion and Their Application. 6th Russian-German Conference on Electric Propulsion and Their Application, 28. Aug. - 02. Sept. 2016, Samara, Russland. Volltext nicht online.

Nöding, Peter and Meyer, Lisa and Keiderling, David (2018) Recent Developments of the DLR Tau Code regarding CFD Simulation of Tank Sloshing Phenomena. 4th Airbus/Ariane Propellant Sloshing Symposium, 07.-08. Nov. 2018, Immenstaad. Volltext nicht online.

O

Oblapenko, G.P. and Kustova, E.V. and Hannemann, Klaus and Hannemann, Volker (2018) Assessment of Recent Thermo-chemical Relaxation Models Using the DLR-TAU Code. In: 31st International Symposium on Rarefied Gas Dynamics (RGD31). 31st International Symposium on Rarefied Gas Dynamics (RGD31), 23.-27. Juli 2018, Glasgow, UK. Volltext nicht online.

Ozawa, Hiroshi and Wagner, Alexander and Martinez Schramm, Jan and Hannemann, Klaus (2019) Aerothermodynamic experiments using TSP in high-speed and complex flows. In: 7th Japanese-German Joint Seminar – Molecular Imaging Technology for Interdisciplinary Research –. 7th Japanese-German Joint Seminar, Molecular Imaging Technology for Interdisciplinary Research, 17.-19.Sep. 2019, Hokkaido, Japan.

P

Pearson, Joe and Horchler, Tim and Hannemann, Volker and Karl, Sebastian and Hannemann, Klaus (2017) Vorhersage von Flammenlängen in Raketenbrennkammern. 18. STAB-Workshop, 07.-08. Nov. 2017, Göttingen, Deutschland. Volltext nicht frei.

Ponchio Camillo, Giannino and Wagner, Alexander and Dittert, Christian and Benjamin, Leroy and Wartemann, Viola and Neumann, Jens and Hink, Rüdiger (2020) Experimental investigation of the effect of transpiration cooling on second mode instabilities in a hypersonic boundary layer. Experiments in Fluids, 61 (162), pp. 1-19. Springer. doi: 10.1007/s00348-020-02994-8. ISSN 0723-4864.

Ponchio Camillo, Giannino and Wagner, Alexander and Hannemann, Klaus (2019) Focused Laser Differential Interferometer for Shock Tunnel Applications. Diagnostik in Verbrennung und Aerodynamik, 26.-27.11.2019, Göttingen, Deutschland. Volltext nicht online.

R

Riedmann, Hendrik and Banuti, Daniel and Ivancic, Blazenko and Knab, Oliver and Hannemann, Klaus (2019) Modeling of H2/O2 single-element rocket thrust chamber combustion at sub- and supercritical pressures with different computational fluid dynamics tools. In: EUCASS Book Series - Advances in Aerospace Sciences: Progress in Propulsion Physics EUCASS book series - Advances in AeroSpace Sciences, 11. EDP Sciences. pp. 247-272. doi: 10.1051/eucass/201911247. ISBN 978-5-94588-228-7. ISSN 2493-3503.

Risius, Steffen and Beck, Walter H. and Klein, Christian and Henne, Ulrich and Wagner, Alexander (2017) Determination of heat transfer into a wedge model in a hypersonic flow using temperature-sensitive paint. Experiments in Fluids, 58 (9), pp. 1-13. Springer. doi: 10.1007/s00348-017-2393-z. ISSN 0723-4864.

S

Scalo, Carlo and Sousa, Victor C. B. and Wartemann, Viola and Wagner, Alexander (2018) Numerical Investigation of Hypersonic Turbulence Transition Delay via Porous Walls. 71st Annual Meeting of the APS Division of Fluid Dynamics, 18.–20. Nov. 2018, Atlanta, Georgia. Volltext nicht online.

Schlegat, Thomas and Hannemann, Klaus (2018) Experimental Investigation of Rarefaction Effects on Aerodynamic Coefficients of Slender and Blunt Re-entry Vehicles. In: International Conference on High-Speed Vehicle Science and Technology 2018 (HiSST). International Conference on High-Speed Vehicle Science and Technology (HiSST), 26.–29. November 2018, Moskau, Russland. Volltext nicht online.

Schneider, Dirk and Génin, Chloé and Stark, Ralf and Oschwald, Michael and Karl, Sebastian and Hannemann, Volker (2017) Numerical Model for Nozzle Flow Application under LOX/Methane Hot Flow Conditions. Journal of Propulsion and Power, 34 (1), pp. 221-233. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.B36611. ISSN 0748-4658. Volltext nicht online.

Schneider, Dirk and Hardi, Justin and Martin, Jan and Stark, Ralf and Suslov, Dmitry and Tonti, Federica and Van Schyndel, Jan and Zhukov, Victor / V. P. and Oschwald, Michael and Costa Ruiz, Eugeni and Fechter, Stefan and Horchler, Tim and Karl, Sebastian and Hannemann, Klaus and Adler, Marko and Jack, Sebastian and Eggers, Thino and Lechtenberg, Ansgar and Gerlinger, Peter (2019) DLR Project TAUROS: TAU for Rocket Thrust Chamber Simulation. In: Proceedings of the 8th European Conference for Aeronautics and Space Sciences. 8th European Conference for Aeronautics and Space Sciences EUCASS, 1. - 4. Jul. 2019, Madrid, Spain. doi: 10.13009/EUCASS2019-515.

Schrijer, Ferry and van Gent, P. L. and Hannemann, Klaus and Horchler, Tim and Fertig, M. and Deck, S. (2017) Comparison of high speed PIV experiments, unsteady pressure measurements and DES computations of a transonic Ariane 5 base-flow using POD. In: 7th European Conference for Aeronautics and Space Sciences (EUCASS) 2017. Proceedings 7th European Conference for Aeronautics and Space Sciences (EUCASS), 03.-06. Juli 2017, Mailand, Italien. doi: 10.13009/EUCASS2017-42.

Schumann, Jan-Erik and Fertig, Markus and Hannemann, Volker and Eggers, Thino and Hannemann, Klaus (2021) Numerical Investigation of Space Launch Vehicle Base Flows with Hot Plumes. In: Future Space-Transport-System Components under High Thermal and Mechanical Loads Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 146. Springer, Cham. pp. 179-191. doi: 10.1007/978-3-030-53847-7_11. ISBN 978-3-030-53846-0. ISSN 1612-2909.

Schumann, Jan-Erik and Hannemann, Volker and Hannemann, Klaus (2019) Investigation of structured and unstructured grid topology and resolution dependence for scale-resolving simulations of axisymmetric detaching-reattaching shear layers. In: Progress in Hybrid RANS-LES Modelling, 143, pp. 169-179. Springer International Publishing. 7th Symposium on Hybrid RANS-LES Methods, 17.-19. Sep. 2018, Berlin, Deutschland. doi: 10.1007/978-3-030-27607-2_13. ISBN 978-3-030-27606-5. ISSN 1612-2909.

Schumann, Jan-Erik and Toosi, Siavash and Larsson, Johan (2020) Assessment of grid anisotropy effects on LES models with different length scales. AIAA Journal, 58 (10), pp. 1-12. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J059576. ISSN 0001-1452.

Sousa, Victor C. B. and Patel, Danish and Chapelier, J.-B. and Wagner, Alexander and Scalo, Carlo (2018) Numerical Investigation of Second Mode Attenuation over Carbon/Carbon Surfaces on a Sharp Slender Cone. AIAA Science and Technology Forum and Exposition (SciTech 2018), 08. -11. Jan. 2018, Kissimee, Florida USA. Volltext nicht online.

Sousa, Victor C. B. and Patel, Danish and Chapelier, J.-B. and Wagner, Alexander and Scalo, Carlo (2018) Numerical Investigation of Second Mode Attenuation over Carbon/Carbon Surfaces on a Sharp Slender Cone. Journal of Spacecraft and Rockets, 210059, pp. 1-11. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/6.2018-0350. ISBN ISBN: 978-162410524-1. ISSN 0022-4650. Volltext nicht online.

Sousa, Victor C. B. and Wartemann, Viola and Wagner, Alexander and Scalo, Carlo (2019) Towards Direct Numerical Simulation of Hypersonic Transition Delay Via Distributed Wall Porosity. AIAA Science and Technology Forum and Exposition (AIAA SciTech 2019), 07.-11. Jan. 2019, San Diego, California, USA. Volltext nicht online.

Stappert, Sven and Wilken, Jascha and Bussler, Leonid and Sippel, Martin and Karl, Sebastian and Klevanski, Josef and Hantz, Christian and Briese, Lale Evrim and Schnepper, Klaus (2019) European Next Reusable Ariane (ENTRAIN): A Multidisciplinary Study on a VTVL and a VTHL Booster Stage. In: Proceedings of the International Astronautical Congress, IAC. 70th International Astronautical Congress, 21.10-25.10.2019, Washington DC.

Stark, Ralf and Génin, Chloé (2017) Experimental Study of TICTOP Nozzles. In: Proceedings of the 31st International Symposium on Shock Waves (ISSW31). 31st International Symposium on Shock Waves (ISSW31), 10. - 14. Jul. 2017, Nagoya, Japan. Volltext nicht online.

Steelant, Johan and Villace, Victor F. and Kallenbach, Alexander and Wagner, Alexander and Andro, Jean-Yves and di Benedetto, Sara and Saracoglu, 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 Grigoriev, N.V. and Neely, A.J, and Verstraete, D. and Buttsworth, D. (2018) Flight Testing Designs in HEXAFLY-INT for High-Speed Transportation. In: International Conference on High-Speed Vehicle Science and Technology 2018 (HiSST). International Conference on High-Speed Vehicle Science and Technology 2018 (HiSST), 26.-29. November 2018, Moskau, Russland. Volltext nicht frei.

Surujhlal, Divek and Ponchio Camillo, Giannino and Wagner, Alexander (2019) Distributed Roughness-Induced Transition in a Hypersonic Boundary-Layer on a Cone. 19. STAB-Workshop, 5.-6.11.2019, Göttingen, Germany. Volltext nicht online.

Surujhlal, Divek and Wagner, Alexander and Ponchio Camillo, Giannino (2019) High-speed TSP applications to transitional hypersonic boundary-layers. Diagnostik in Verbrennung und Aerodynamik, 26.-27.11.2019, Göttingen, Deutschland. Volltext nicht online.

T

Tanno, Hideyuki and Noguchi, Y and Ito, Katsuhiro and Friedl, Damian and Martinez Schramm, Jan and Hannemann, Klaus (2019) FORCE MEASUREMENT COMPARISON OF BLUNT CONES IN HIGH-ENTHALPY SHOCK TUNNEL HEG AND HIEST. International Conference on Flight vehicles, Aerothermodynamics and Re-entry Missions and Engineering (FAR), 30.9-3.10.2019, Monopoli, Italien. Volltext nicht online.

Tonti, Federica and Hardi, Justin and Horchler, Tim and Fechter, Stefan and Oschwald, Michael (2019) Influence of numerical model setup on the response of acoustically forced LOx/H2 flames. In: Proceedings of the 8th European Conference for Aeronautics and Space Sciences. 8th European Conference for Aeronautics and Space Sciences EUCASS, 1. - 4. Jul. 2019, Madrid, Spain. doi: 10.13009/EUCASS2019-559.

V

Volkmar, Chris (2017) Elektrische Antriebe – Eine Kerntechnologie der Raumfahrt: Electric Propulsion Made in Gießen. Absolventenfeier Technische Hochschule Mittelhessen, 10. Nov. 2017, Gießen, Deutschland. Volltext nicht online.

Volkmar, Chris and Geile, C. and Hannemann, K. (2018) Radio-Frequency Ion Thrusters—Power Measurement and Power Distribution Modeling. Journal of Propulsion and Power, 34 (4), pp. 1061-1069. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.B36868. ISSN 0748-4658.

Volkmar, Chris and Geile, Christopher and Neumann, Andreas and Hannemann, Klaus (2018) Fluxgate Magnetometer-Based Determination of Ion Beam Current. Space Propulsion 2018, 14.-18. Mai 2018, Sevilla, Spanien. Volltext nicht online.

Volkmar, Chris and Geile, Christopher and Neumann, Andreas and Hannemann, Klaus (2019) Direct-current current transformer for the measurement of an electric propulsion ion beam. Review of Scientific Instruments, 90 (3), 033303. American Institute of Physics (AIP). doi: 10.1063/1.5087804. ISSN 0034-6748.

Volkmar, Chris and Neumann, Andreas and Geile, Christopher and Hannemann, Klaus (2017) Real-time in-situ measurement of inductively coupled power and numerical prediction of power distribution in RF ion thrusters. 35th International Electric Propulsion Conference, 08.-12. Okt. 2017, Atlanta, GA, USA. Volltext nicht frei.

Volkmar, Chris and Neumann, Andreas and Geile, Christopher and Hannemann, Klaus (2018) Fluxgate Magnetometer Based Determination of Ion Beam Current – Work in Progress. XXV. Erfahrungsaustausch Oberflächentechnologie mit Plasma- und Ionenstrahlprozessen, 20.-23. März 2018, Mühlleithen, Deutschland. Volltext nicht online.

Volkmar, Chris and Neumann, Andreas and Geile, Christopher and Hannemann, Klaus (2017) Real-time in situ determination of inductively coupled power and axi-symmetric model based prediction of heuristic plasma parameters in RF ion thrusters. XXIV. Erfahrungsaustausch Oberflächentechnologie mit Plasma- und Ionenstrahlprozessen, 07.-09. März 2017, Mühlleithen, Deutschland. Volltext nicht online.

Volkmar, Chris and Neumann, Andreas and Geile, Christopher and Hannemann, Klaus (2018) Direct-current current transformer for accurate ion beam measurement. In: 7th Russian German Conference on Electric Propulsion and Their Application (RGCEP 2018). 7th Russian German Conference on Electric Propulsion and Their Application(RGCEP 2018), 21.-26. Okt. 2018, Rauischholzhausen, Deutschland. Volltext nicht online.

Volpiani, Pedro S. and Larsson, Johan and Bernardini, Matteo and Wagner, Alexander (2019) Using large-eddy simulations to design a new hypersonic shock/boundary-layer interaction experiment. In: AIAA Scitech Forum, 2019. AIAA Science and Technology Forum AIAA SciTech 2019, 7.-11. Jan. 2019, San Diego, California, USA. doi: 10.2514/6.2019-0098. ISBN 978-162410578-4. Volltext nicht online.

W

Wagner, Alexander (2018) High Frequency Pressure Measurements in Shock Tunnels using Piezoelectric Transducers. 12th International Workshop on Shock Tube Technology, IWSTT, 12.-13.04.2018, Kakuda, Japan. Volltext nicht online.

Wagner, Alexander (2018) High Frequency Pressure Measurements by means of Piezoelectric Transducers. AIAA Aviation Transition Open Forum, 29.06.2018, Atlanta, USA. Volltext nicht online.

Wagner, Alexander (2019) Prediction, Modeling and Measurement of Hypersonic Turbulence. STO AVT-ET-200 Kick-Off Meeting, 15.-16.04.2019, Purdue, USA. Volltext nicht online.

Wagner, Alexander (2019) Influence of Leading Edge Imperfection on Boundary Layer State - Testing at HEG (DLR) - Progress Report. Project Report. Volltext nicht online.

Wagner, Alexander (2019) Influence of Leading Edge Imperfection on Boundary Layer State - Testing at HEG (DLR) - FINAL REPORT. Project Report. Volltext nicht online.

Wagner, Alexander and Dittert, Christian and Kütemeyer, Marius (2017) Hypersonic Transition in High Enthalpy Facilities. Lecture Series: Multiphysics phenomena analysis on boundary layer stability in hypersonic regime - STO-AVT-289, 20. Sep. 2017, Sint-Genesius-Rode, Belgium. Volltext nicht online.

Wagner, Alexander and Dittert, Christian and Kütemeyer, Marius and Wartemann, Viola (2017) Ultrasonically Absorptive Thermal Protection Materials for Passive Hypersonic Transition Control. Passive Hypersonic Transition Control by Means of Ultrasonically Absorptive Thermal Protection Materials, 24. Juli 2017, Purdue University, USA. Volltext nicht online.

Wagner, Alexander and Hannemann, Klaus (2019) Selected Research Activities and Future Fields of Interest at DLR Göttingen AS-RFZ. 1st German Hypersonic Forum, 23.-24.09.2019, München, Deutschland. Volltext nicht online.

Wagner, Alexander and Martinez Schramm, Jan and Dittert, Christian and C. B. Sousa, Victor and Patel, Danish and Scalo, Carlo (2018) Experimental and numerical acoustic characterization of ultrasonically absorptive porous materials. AIAA Aviation and Aeronautics Forum and Exposition 2018, 25.-29. Juni 2018, Atlanta, USA.

Wagner, Alexander and Martinez Schramm, Jan and Dittert, Christian and Sousa, Victor C. B. and Patel, Danish and Scalo, Carlo (2018) Experimental and numerical acoustic characterization of ultrasonically absorptive porous materials. 2018 AIAA AVIATION Forum, 25.-29. Juni 2018, Atlanta, USA.

Wagner, Alexander and Martinez Schramm, Jan and Hannemann, Klaus (2018) Flow characterization and numerical modeling of the DLR High-Enthalpy Shock Tunnel Göttingen (HEG). In: STO-AVT-325 - Flow Characterization and Modeling of Hypersonic Wind Tunnels. NATO STO. STO-AVT-325 - Flow Characterization and Modeling of Hypersonic Wind Tunnels, 3.-5. Dez. 2018, Brüssel, Belgien. Volltext nicht frei.

Wagner, Alexander and Martinez Schramm, Jan and Wartemann, Viola and Ponchio Camillo, Giannino and Ozawa, Hiroshi and Steelant, Johan (2019) Boundary Layer Transition Studies on the HEXAFLY-INT Hypersonic Glide Vehicle. FAR 2019 - International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions & Engineering, 30.09.-03.10.2019, Monopoli, Italien. Volltext nicht frei.

Wagner, Alexander and Scalo, Carlo (2019) RTG proposal on Measurement, Modeling and Prediction of Hypersonic Turbulence. AVT 44th Panel Business Meeting Week, 7.-11.10.2019, Trondheim. Volltext nicht online.

Wagner, Alexander and Scalo, Carlo (2019) ET-200 closure: Measurement, Modeling and Prediction of Hypersonic Turbulence. AVT 44th Panel Business Meeting Week, 7.-11.10.2019, Trondheim, Norwegen. Volltext nicht online.

Wagner, Alexander and Schülein, Erich and Petervari, René and Hannemann, Klaus and Syed Raza, Christopher Ali and Cerminara, Adriano and Sandham, N.D. (2018) Combined free-stream disturbance measurements and receptivity studies in hypersonic wind tunnels by means of a slender wedge probe and direct numerical simulation. Journal of Fluid Mechanics, 842, pp. 495-531. Cambidge University Press. doi: https://doi.org/10.1017/jfm.2018.132. ISSN 0022-1120. Volltext nicht online.

Wagner, Alexander and Surujhlal, Divek (2019) Hypersonic Flat Plate Shock Wave Boundary-Layer Interactions Heated. 2019 AFOSR/ONR/HVSI Hypersonic Aerothermodynamics Portfolios Review, 8.-12.07.2019, Boulder, USA. Volltext nicht online.

Wagner, Alexander and Wartemann, Viola and Dittert, Christian and Kütemeyer, Marius (2017) Passive Hypersonic Transition Control by Means of Ultrasonically Absorptive Thermal Protection Materials (UAT). 2017 Annual Review for the AFOSR High Speed Aerodynamics Portfolio and the ONR Hypersonics Portfolio, 24. Juli 2017, NASA Langley, Hampton, VA, USA. Volltext nicht online.

Wagner, Alexander and Wartemann, Viola and Dittert, Christian and Kütemeyer, Marius (2019) Design and Test of an Ultrasonically Absorptive Thermal Protection Material for Passive Hypersonic Transition Control. In: Ninth IUTAM Symposium on Laminar-Turbulent Transition. IUTAM Symposium on Laminar-Turbulent Transition, 02.-06.09.2019, London, GB.

Wagner, Alexander and Wartemann, Viola and Dittert, Christian and Kütemeyer, Marius (2019) UAT - Passive Hypersonic Transition Control by Means of Ultrasonically Absorptive Thermal Protection Materials. 2019 AFOSR/ONR/HVSI Hypersonic Aerothermodynamics Portfolios Review, Boulder, USA. Volltext nicht online.

Wagner, Alexander and Wartemann, Viola and Dittert, Christian and Kütemeyer, Marius (2019) Passive Hypersonic Transition Control by Means of Ultrasonically Absorptive Thermal Protection Materials (UAT) - FINAL REPORT. Project Report. Volltext nicht frei.

Wagner, Bernd and Schneider, Dirk and Beinke, Scott and Suslov, Dmitry and Génin, C. and Hardi, Justin and Oschwald, Michael and Costa Ruiz, Eugeni and Karl, S. and Fechter, Stefan and Banuti, Daniel and Hannemann, Klaus and Jack, Sebastian and Alder, Marko and Rudolph, Martin and Eggers, Thino and Gerlinger, P. and Lempke, M. (2017) Rocket propulsion in TAU: an overview of the DLR ProTAU project. In: 7th European Conference for Aeronautics and Space Sciences (EUCASS) 2017. 7th European Conference for Aeronautics and Space Sciences (EUCASS), 03. - 06. Jul. 2017, Mailand, Italien. doi: 10.13009/EUCASS2017-42.

Wartemann, Viola and Ponchio Camillo, Giannino and Reiter, Philipp and Neumann, Jens and Wagner, Alexander (2018) Influence of active cooling on second mode instabilities investigated on hypersonic, conical flows. HiSST: International Conference on High-Speed Vehicle Science Technology, 26. - 29. Nov. 2018, Moskau. Volltext nicht online.

Wartemann, Viola and Ponchio Camillo, Giannino and Reiter, Philipp and Neumann, Jens and Wagner, Alexander (2019) Influence of transpiration cooling on second mode instabilities investigated on hypersonic, conical flows. CEAS Space Journal, 11, pp. 341-350. Springer. doi: 10.1007/s12567-019-00249-9. ISSN 1868-2502. Volltext nicht online.

Wartemann, Viola and Ponchio Camillo, Giannino and Wagner, Alexander and Neumann, Jens and Weber, Alexander (2019) Stability analyses of hypersonic, conical flows with transpiration cooling. IUTAM Symposium on Laminar Turbulent Transition, 2. - 6.9.2019, London, Großbritanien. Volltext nicht online.

Wartemann, Viola and Wagner, Alexander and Wagnild, Ross and Pinna, Fabio and Miro Miro, Fernando and Tanno, Hideyuki (2018) Code to code comparison on hypersonic high enthalpy transitional boundary layers. In: AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting, 210059. AIAA. AIAA SciTech, 8–12 January 2018, Kissimmee, USA. doi: 10.2514/6.2018-0351. ISBN 978-162410524-1. Volltext nicht online.

Wartemann, Viola and Wagner, Alexander and Wagnild, Ross and Pinna, Fabio and Miro Miro, Fernando and Tanno, Hideyuki and Johnson, Heath (2018) High-Enthalpy Effects on Hypersonic Boundary-Layer Transition. Journal of Spacecraft and Rockets, 56 (2), pp. 347-356. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.A34281. ISBN ISSN 0022-4650 (print) and 1533-6794 (online). ISSN 0022-4650. Volltext nicht online.

Z

Zilker, Franziska (2018) Aerothermal Analysis of Re-usable First Stage during Rocket Retro-propulsion. Master's.

Zilker, Franziska and Ecker, Tobias and Dumont, Etienne and Hannemann, Klaus (2017) Aerothermal Analysis of Reusable First Stage Launcher during Re-Entry Retro-Propulsion. 18. STAB-Workshop 2017, 07.-08. Nov. 2017, Göttingen, Deutschland. Volltext nicht online.

This list was generated on Fri Apr 9 20:36:19 2021 CEST.