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

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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. Elsevier. 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 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.

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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]

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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 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.

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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 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.

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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 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 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.

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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. 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: 31st International Symposium on Rarefied Gas Dynamics. 31st International Symposium on Rarefied Gas Dynamics 2018, 23.-27. Jul. 2018, Glasgow, Scotland. Volltext nicht 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. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.J056312 ISSN 0001-1452 Volltext nicht online.

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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 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. 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). Forschungszentrum Jülich GmbH. DOI: 10.17815/jlsrf-4-168 ISSN 2364-091X

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 (2018) Non-equilibrium parameter for a hybrid Fokker-Planck/ DSMC scheme. In: 31st International Symposium on Rarefied Gas Dynamics. 31st International Symposium on Rarefied Gas Dynamics 2018, 23.-27. Juli 2018, Glasgow, Scotland. Volltext nicht online.

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.

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) 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.

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.

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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 Pressure Driven Rarefied Gas Flow Through A Thin Slit. In: 31st International Symposium on Rarefied Gas Dynamics 2018. 31st International Symposium on Rarefied Gas Dynamics 2018, 23.-27. Jul. 2018, Glasgow, Scotland. 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.

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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 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.

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.

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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. 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.

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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 (2018) Time Response Calibration of Ultra-Fast Temperature Sensitive Paints for the Application in High Temperature Hypersonic Flows. In: 21th STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics. 21. STAB/DGLR Symposium 2018, 6.-7. Nov. 2018, Darmstadt. Volltext nicht online.

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 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.

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 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.

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Neumann, Andreas (2017) Update on Diagnostics for DLR's Electric Propulsion Test Facility. Procedia Engineering, 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. 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 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 (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.

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.

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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.

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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.

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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. 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

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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. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.B36611 ISSN 0748-4658 Volltext nicht online.

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 Hannemann, Volker and Hannemann, Klaus (2018) 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. 7th Symposium on Hybrid RANS-LES Methods, 17.-19. Sep. 2018, Berlin, Deutschland.

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 Porous Surfaces. Journal of Spacecraft and Rockets, 210059. 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.

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.

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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.

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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 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 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 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 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, 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 (3). Springer. DOI: 10.1007/s12567-019-00249-9 ISSN 1868-2502 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. AIAA SciTech, 8–12 January 2018, Kissimmee, USA. 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. 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.

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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.