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Items where Subject is "Institute of Space Propulsion > Rocket Propulsion Technology"

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Number of items at this level: 82.

A

  Armbruster, Wolfgang (2022) Untersuchung injektorgekoppelter Verbrennungsinstabilitäten in einer kryogenen Raketenbrennkammer. DLR-Forschungsbericht. DLR-FB-2022-9. Dissertation. RWTH Aachen. 280 S. doi: 10.57676/4dth-bn38. file

  Armbruster, Wolfgang and Hardi, Justin and Martin, Jan and Oschwald, Michael (2021) Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine. Symposium on Thermoacoustics in Combustion: Industry meets Academia (SoTiC 2021), 6. - 10. Sept. 2021, Munich, Germany. Volltext nicht frei. file

  Armbruster, Wolfgang and Hardi, Justin and Oschwald, Michael (2022) REST HF-7 and HF-9 Test Case: Lessons learned for comparing simulation results with test data of a representative LOX/H2 thrust chamber with high-frequency combustion instabilities. 9th European Conference for Aeronautics and Space Sciences EUCASS, 27. Jun. - 01 Jul. 2022, Lille, France. doi: 10.13009/EUCASS2022-4739. file

  Armbruster, Wolfgang and Hardi, Justin and Oschwald, Michael (2022) Impact of shear-coaxial injector hydrodynamics on high-frequency combustion instabilities in a representative cryogenic rocket engine. International Journal of Spray and Combustion Dynamics, 14 (1-2). Sage Publications. doi: 10.1177/17568277221093848. ISSN 1756-8277. file

  Artzt, Katia Juliane and Barriobero Vila, Pere and Gussone, Joachim and Bauer, Peter-Philipp and Kasperovich, Galina and Löbbecke, Miriam and Requena, Guillermo and Riccius, Jörg and Suslov, Dmitry and Hümbert, Simon and Haubrich, Jan (2021) Additive Manufacturing of Components for Rocket Propulsion. IRAS Additive Manufacturing Workshop, 05 July 2021, Virtual. Volltext nicht online.

  Artzt, Katia Juliane and Bauer, Peter-Philipp and Gussone, Joachim and Kasperovich, Galina and Barriobero Vila, Pere and Requena, Guillermo and Haubrich, Jan and Kitsche, Wolfgang and Riccius, Jörg and Suslov, Dmitry and Kleinert, Jan and Rosauer, Philipp and Siggel, Martin and Hümbert, Simon (2022) Metal Additive Manufacturing of Space Components @ DLR. 1st international conference on advanced manufacturing for air, space and land transportation, 07.-11.März 2022, online event. Volltext nicht online.

B

  Bee, Alexander (2021) Design und experimenteller Vergleich von Swirl-Koaxialund Scher-Koaxial-Injektorelementen für Hauptbrennkammern von LOX/LNG-Triebwerken. Master's, Institut für Raumfahrtsysteme. file

  Bee, Alexander and Börner, Michael (2021) Laminar Burning Speeds and Flammability Limits of CH4/O2 Mixtures With Varying N2 Dilution at Sub-Atmospheric Conditions. Combustion Science and Technology. Taylor & Francis. doi: 10.1080/00102202.2021.2006191. ISSN 0010-2202. file

  Bonanni, Mathew and Mohaddes, Danyal and Nguyen, Ly and Perakis, Nikolaos and Hardi, Justin and Börner, Michael and Ihme, Matthias (2021) Toward Numerical Investigation of Ignition and Combustion Transition in a Subscale LOX/Methane Rocket Combustor. In: AIAA Scitech 2021 Forum. AIAA SciTech Forum, 19. - 21. Jan. 2021, Virtual event. doi: 10.2514/6.2021-1141. ISBN 978-162410609-5. Volltext nicht frei. file

  Boppana, Chaitanya Kumar (2021) A Spectroscopic Study of the OH* Radical and its Application in Thermometry. Master's, Delft University of Technology. Volltext nicht online.

  Börner, Michael (2022) Selected Topics of Space Propulsion. Vorlesungsreihe: Selected Topics of Space Propulsion, Nov. - Dez. 2022, Darmstadt, D. Volltext nicht online.

  Börner, Michael (2022) Space Propulsion and Space Transportation Systems. Vorlesungsreihe: Space Propulsion and Space Transportation Systems, Apr. - Jul. 2022, Darmstadt. Volltext nicht online.

  Börner, Michael (2022) Experimentelle Untersuchung der laserinduzierten Zündung von kryogenen Flüssigkeitsraketenbrennkammern. DLR-Forschungsbericht. DLR-FB-2022-29. Dissertation. RWTH Aachen. (In Press) Volltext nicht online.

  Börner, Michael (2022) Zündung von Flüssigraketentriebwerken. Vorlesungsreihe: Chemische Raumfahrtantriebe, 28. Nov. 2022, Stuttgart, D. Volltext nicht online.

  Börner, Michael (2022) Stand und Perspektive der Fusionsforschung: Welchen Beitrag kann die Fusionsforschung perspektivisch zur Energieversorgung leisten? Space Forum Vortragsreihe, 5. Mai 2022, DLR Lampoldshausen, D. Volltext nicht online.

  Börner, Michael and Klein, Sebastian and Rees, Andreas and Traudt, Tobias and Hardi, Justin (2022) Overview on the DLR M3 Test Infrastructure. 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions Engineering (FAR), 19. - 23. Juni 2022, Heilbronn. file

  Börner, Michael and Martin, Jan and Hardi, Justin and Suslov, Dmitry and Deeken, Jan C. and Oschwald, Michael (2021) Lumen thrust chamber - flame anchoring for shear coaxial injectors. Space Propulsion 2020 + 1, 17. - 19. Mrz. 2021, Virtual. Volltext nicht frei. file

  Börner, Michael and Martin, Jan and Hardi, Justin and Suslov, Dmitry and Deeken, Jan C. and Oschwald, Michael (2021) Flame anchoring for shear coaxial injectors in a LOX/LNG rocket engine demonstrator. ODAS MOTAR 2021, 14.06.2021, Virtual. Volltext nicht frei. file

  Börner, Michael and Traudt, Tobias and Klein, Sebastian and Hardi, Justin (2022) OVERVIEW OF THE DLR M3 TEST FIELD FOR COMPONENT TESTING FOR CRYOGENIC PROPULSION. In: 3rd Ground-based space facilities symposium 2022. 3rd Ground-Based Space Facilities Symposium, 6. - 8. Dez. 2022, Marseille, France. Volltext nicht online.

  Bürger, Chris (2021) Numerische Simulation des konjugierten Wärmeübergangs in einem mit überkritischem Stickstoff durchströmten Kühlkanal eines Flüssigraketentriebwerks. Master's, Universität Stuttgart. file

D

  Dresia, Kai and Kurudzija, Eldin and Waxenegger-Wilfing, Günther and Behler, Hendrik and Auer, Daniel and Fröhlke, Karsten and Neumann, Heike and Frank, Anja and Laurent, Jérôme and Fabreguettes, Luce (2022) AI-Assisted Control Systems for Rocket Engine Test Facilities within the ESA FLAME Program. In: 8th Space Propulsion Conference. 8th Space Propulsion Conference, 09.-13. Mai 2022, Estoril, Portugal. Volltext nicht online.

E

  Ehrt, Christian (2023) Data analysis and assessment of flame anchoring and combustion stability in a rocket combustion chamber with LOX/LNG depending on the operating conditions at supercritical and transcritical pressure conditions. Master's, Technische Universität Darmstadt. Volltext nicht frei. file

F

  Fombonne, A. and Leichtfuß, S. and Börner, Michael and Jakob, H. and Albert, J. and Schiffer, H.-P. (2022) DESIGN AND TESTING OF A PROPULSION SYSTEM FOR 3U-CUBESAT APPLICATION. In: 71. Deutscher Luft- und Raumfahrtkongress 2022. 71. Deutscher Luft- und Raumfahrtkongress 2022, 27. - 29. Sep. 2022, Dresden, D. Volltext nicht online.

  Fuchs, Hagen (2021) Analyse akustischer Eigenmoden in Raketenbrennkammern bei Umgebungsbedingungen. Bachelor's, Karlsruher Institut für Technologie (KIT). file

G

  Guda Vadla, Sai Kumar Reddy (2021) Cavitation Simulation using openFOAM. Master's, Universität Duisburg-Essen. Volltext nicht frei. file

  Gulczynski, Mateusz T. and Dos Santos Hahn, Robson Henrique and Riccius, Jörg and Zametaev, Evgeny and Waxenegger-Wilfing, Günther and Deeken, Jan C. and Oschwald, Michael (2022) Numerical Turbine Blade Fatigue Life Analysis for Reusable Liquid Rocket Engines (LREs) Applications. In: EUCASS-3AF 2022 9th European Conference for Aerospace Sciences. EUCASS-3AF. EUCASS-3AF 2022 9th European Conference for Aeronautics and Space Science, 27 June - 1 July 2022, Lille, France. doi: 10.13009/EUCASS2022-6150. file

  Gulczynski, Mateusz T. and Riccius, Jörg R. and Waxenegger-Wilfing, Günther and Deeken, Jan C. and Oschwald, Michael (2023) Combustion Chamber Fatigue Life Analysis for Reusable Liquid Rocket Engines (LREs). In: AIAA Scitech 2023. Aerospace Center. Published by the American Institute of Aeronautics and Astronautics, Inc.. AIAA SCITECH 2023 Forum, 23-27 January 2023, National Harbor, Washington DC, USA. doi: 10.2514/6.2023-1263. file

H

  Hardi, Justin (2022) Zündung und Verbrennung. Vorlesungsreihe: Luft- und Raumfahrttechnik 2, 09.06.2022, Aachen. Volltext nicht online.

  Hardi, Justin (2022) Treibstoffeinstpritzung und -aufbereitung. Vorlesungsreihe: Luft- und Raumfahrttechnik 2, 02.06.22, Aachen. Volltext nicht online.

  Hardi, Justin (2022) Treibstoffeinspritzung und -aufbereitung. Vorlesungsreihe: Chemische Raumfahrtantriebe, 21. Nov. 2022, Stuttgart, D. Volltext nicht online.

  Hardi, Justin (2022) DLR-RA Abteilung Raketenantriebstechnologie. DLR Summer School Space Propulsion 2022, 9. Sep. 2022, Lampoldshausen, D. Volltext nicht online.

  Hardi, Justin and Martin, Jan and Kaess, Roland and Horchler, Tim and Koegelmeier, Stefan and Tonti, Federica and Soller, Sebastian and Gernoth, Andreas (2022) Improving validation of predictive tools for injector-coupled combustion instabilities. 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions Engineering (FAR), 19. - 23. Juni 2022, Heilbronn. file

  Hermansson, Birgir (2022) Development and Analysis of a Gaseous Hydrogen-Oxygen Rotating Detonation Combustor. Institutsseminar, 11. Nov. 2022, Lampoldshausen, D. Volltext nicht online.

  Horchler, Tim and Fechter, Stefan and Hardi, Justin (2021) Numerical Investigation of Flame-Acoustic Interaction at Resonant and Non-Resonant Conditions in a Model Combustion Chamber. Symposium on Thermoacoustics in Combustion: Industry meets Academia, 06.-10. Sep. 2021, München, Deutschland. Volltext nicht online.

  Horchler, Tim and Fechter, Stefan and van Schyndel, Jan and Oschwald, Michael (2022) REST HF-10 Test Case: Numerical Simulation of a Single Coaxial LOX-CH4 Injector with Forced Mass Flow Oscillations Using the DLR TAU-Code. In: 9th European Conference for Aeronautics and Aerospace Sciences (EUCASS), pp. 1-14. 9th European Conference for Aeronautics and Aerospace Sciences (EUCASS), 27.06. - 01.07.2022, Lille, Frankreich. doi: 10.13009/EUCASS2022-4415. Volltext nicht frei. file

I

  Irtingkauf, John Luca (2021) Investigation of flame topology and dynamics in a research rocket combustor. Master's, Institut für Raumfahrtsysteme, Fakultät Luft- und Raumfahrttechnik und Geodäsie. file

J

  Jack, Sebastian and Stark, Ralf (2022) Design and Preliminary Numerical Analysis of a Flexible Structure for a Cold Gas Nozzle Experiment. 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions and Engineering, 19.-23. Juni 2022, Heilbronn, Deutschland. Volltext nicht online.

K

  Kaya, Dogan (2022) Modellierung der Blendenströmung im BKD LOX-Injektor mittels LES. Institutsseminar, 11. Nov. 2022, Lampoldshausen, D. Volltext nicht online.

  Kirchberger, Christoph and Deeken, Jan C. and Hardi, Justin and Frank, Anja and Lindner, Daniela and Schäfer, Klaus and Schlechtriem, Stefan (2022) Liquid Propulsion - Fundamentals and Highlights. 21st CVA Summer School, 14.07.2022, Bordeaux, France. Volltext nicht online.

  Klingenstein, Lars (2021) Plasmaspektroskopie an laserinduzierten Zündfunken in einer Raketenbrennkamer. Bachelor's, Justus-Liebig-Universität Gießen. file

  Kringe, Pascal and Bürger, Chris and Riccius, Joerg and Zametaev, Evgeny and Oschwald, Michael and Gernoth, Andreas and Soller, Sebastian and Lehmann, Marcus and Reese, Stefanie (2022) Dependency of Surface Temperature on Coolant Mass Flow and Heat Flux in Rocket Combustion Chambers. In: 2022 IEEE Aerospace Conference, AERO 2022. 2022 IEEE Aerospace Conference (AERO), 5. Mrz. - 12. Mrz. 2022, Big Sky, Montana, USA. doi: 10.1109/AERO53065.2022.9843694. ISBN 978-166543760-8. ISSN 1095-323X. Volltext nicht online.

  Kringe, Pascal and Riccius, Jörg and Zametaev, E. and Oschwald, Michael and Gernoth, Andreas and Soller, Sebastian and Lehmann, Marcus and Reese, Stefanie (2021) Dependency of Inner Liner Surface Temperature on Coolant Mass Flow Rate and Heat Flux in Rocket Combustion Chambers. Space Propulsion 2020 + 1, 17. - 19. Mrz. 2021, Online. file

M

  Martin, Jan and Armbruster, Wolfgang and Hardi, Justin (2021) Flame-acoustic interaction in a high-pressure, single-injector, LOX/H2 rocket combustor with optical access. Symposium on Thermoacoustics in Combustion: Industry meets Academia (SoTiC 2021), 6. - 10. Sept. 2021, Munich, Germany. Volltext nicht frei. file

  Martin, Jan and Armbruster, Wolfgang and Hardi, Justin and Suslov, Dmitry (2021) Experimental Investigation of Self-Excited Combustion Instabilities in a LOX/LNG Rocket Combustor. Journal of Propulsion and Power, 37 (6). American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.B38289. ISSN 0748-4658. file

  Martin, Jan and Armbruster, Wolfgang and Stützer, Robert and General, Stephan and Knapp, Bernhard and Suslov, Dmitry and Hardi, Justin (2021) Flame characteristics of a high-pressure LOX/H2 rocket combustor with large optical access. Case Studies in Thermal Engineering. Elsevier. doi: 10.1016/j.csite.2021.101546. ISSN 2214-157X. file

  Martin, Jan and Armbruster, Wolfgang and Stützer, Robert and Suslov, Dmitry and Hardi, Justin and Oschwald, Michael (2022) Flame dynamics of an injection element operated with LOX/H2 and LOX/CNG in a high-pressure rocket combustor with large optical access. In: 9ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS). 9th European Conference for Aeronautics and Space Sciences EUCASS, 27. Jun. - 01 Jul. 2022, Lille, France. doi: 10.13009/EUCASS2022-4688. file

  Martin, Jan and Armbruster, Wolfgang and Suslov, Dmitry and Stützer, Robert and Hardi, Justin and Oschwald, Michael (2022) Flame Characteristics of a High-Pressure LOX/CNG Rocket Combustor with Large Optical Access. In: 33rd International Symposium on Space Technology and Science. 33rd International Symposium on Space Technology and Science, 26. Feb. - 4. Mrz. 2022, Oita, Japan. Volltext nicht online.

  Martin, Jan and Armbruster, Wolfgang and Suslov, Dmitry and Stützer, Robert and Hardi, Justin and Oschwald, Michael (2022) Flame Characteristics and Response of a High-Pressure LOX/CNG Rocket Combustor with Large Optical Access. Aerospace. Multidisciplinary Digital Publishing Institute (MDPI). doi: 10.3390/aerospace9080410. ISSN 2226-4310. file

  McNutt, Benjamin (2022) RANS Modelling of a LOX/CH4 Single Injector Rocket Combustion Chamber. Institutsseminar, 13. Jul. 2022, Lampoldshausen, D. Volltext nicht online.

  McNutt, Benjamin Alexander (2022) RANS Modelling of a LOX/CH4 Single Injector Rocket Combustion Chamber. Master's, University of Sydney. file

  Morris, Clara Lydia (2022) RANS Modelling of Supercritical LOX/CH4 Combustion in DLR’s BKN Rocket Combustion Chamber. Institutsseminar, 17. Feb. 2022, Lampoldshausen, D. Volltext nicht online.

  Müller, Markus Carsten (2022) Untersuchung von Druckschwankungen in der Flüssigsauerstoffleitung des Mikrobrennkammerprüfstandes M3.1. Institutsseminar, 24. Mrz. 2022, Lampoldshausen, D. Volltext nicht online.

N

  Nakhare, Janhavi Anand (2021) Low-order acoustic stability model of a sub-scale research thrust chamber with LOX/LNG. Master's, Universität Bremen. Volltext nicht frei. file

R

  Riccius, Jörg and Zametaev, Evgeny and Gulczynski, Mateusz T. and Dos Santos Hahn, Robson Henrique (2022) Numerical LRE Turbine Blade Fatigue Life Analysis Taking Into Account Partial Admission Effects. European Space Agency. 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions Engineering (FAR), 19-23 June 2022, Heilbronn. Volltext nicht frei. file

  Riccius, Jörg R. (2022) Strukturmechanik. Vorlesungsreihe "Raumfahrtantriebe II", 11. Nov. 2022, online. Volltext nicht online.

  Riccius, Jörg R. and Zametaev, Evgeny B. (2023) HCF analysis of a prospective 3d-printed LRE turbine blade. AIAA SciTech 2023 Forum, 23.-27. Jan. 2023, National Harbor, MD, USA & Online. doi: 10.2514/6.2023-1086. Volltext nicht online.

  Riccius, Jörg R. and Zametaev, Evgeny B. (2023) HCF and LCF Analysis of a Generic Full Admission Turbine Blade. Aerospace, 10 (2), pp. 1-22. Multidisciplinary Digital Publishing Institute (MDPI). doi: 10.3390/aerospace10020154. ISSN 2226-4310. file

  Riccius, Jörg R. and Zametaev, Evgeny B. and Souverein, Louis J. (2022) HCF, LCF and creep life analysis of a generic LRE turbine blade. In: AIAA SciTech 2022 Forum, pp. 1-10. Aerospace Research Central (ARC). AIAA SciTech 2022 Forum, 3.-7. Jan. 2022, San Diego, CA, USA. doi: 10.2514/6.2022-0796. ISBN 978-162410631-6. Volltext nicht frei. file

S

  Schmitt, Thomas and Kaess, Roland and Behr, Roland and Koeglmeier, Stefan and Knab, Oliver and Horchler, Tim and Van Schyndel, Jan and Hardi, Justin and Marchal, David and Ducruix, Sébastien and Nicole, Aurélie and Dorey, Luc-Henry (2022) REST HF-10 test case: Synthesis of the Contributions for the Simulation of Excited Methane Flames under Real Gas Conditions. In: 9th European Conference for Aeronautics and Aerospace Sciences (EUCASS), pp. 1-15. 9th European Conference for Aeronautics and Aerospace Sciences (EUCASS), 27.06. - 01.07.2022, Lille, Frankreich. doi: 10.13009/EUCASS2022-4433. Volltext nicht frei. file

  Son, Min and Armbruster, Wolfgang and Hardi, Justin and Oschwald, Michael (2021) Measuring the velocity field of a shear-coaxial, cryogenic flame in a high-pressure rocket thrust chamber. Proceedings of the Combustion Institute, 38 (2), 3389 - 3397. Elsevier. doi: 10.1016/j.proci.2020.07.076. ISSN 1540-7489. file

  Son, Min and Armbruster, Wolfgang and Martin, Jan (2021) Velocimetry of a LOX jet in a high-pressure combustion field from high-speed flame images. ODAS MOTAR 2021, 14.06.2021, Virtual. Volltext nicht frei. file

  Son, Min and Armbruster, Wolfgang and Tonti, Federica and Hardi, Justin (2021) Numerical study of acoustic resonance in a LOX injector induced by orifice flow. In: AIAA Propulsion and Energy Forum, 2021. AIAA Propulsion and Energy 2021 Forum, 9. - 11. Aug. 2021, Virtual. doi: 10.2514/6.2021-3568. Volltext nicht frei. file

  Son, Min and Börner, Michael and Hardi, Justin (2021) Experimental study of intra-injector flow fluctuations induced by a LOX injector orifice driving combustion instability. Symposium on Thermoacoustics in Combustion: Industry meets Academia (SoTiC 2020), 14. - 17. Sept. 2021, Virtual. Volltext nicht frei. file

  Stark, Ralf (2021) Düsenexpansion. Vorlesungsreihe Raumfahrtantriebe I, 14. Mai 2021, Aachen, D. Volltext nicht online.

  Stark, Ralf (2022) Düsenexpansion. Vorlesungsreihe "Raumfahrtantriebe I", 20. Mai 2022, Aachen, D. Volltext nicht online.

  Stark, Ralf (2022) Düsenauslegung. DLR Summer School Space Propulsion 2022, 8. Sep. 2022, Lampoldshausen, D. Volltext nicht online.

  Steinn Hermannsson, Birgir (2022) Development and Analysis of a Gaseous Hydrogen-Oxygen Rotating Detonation Combustor. Master's, KTH, Stockholm, Schweden. Volltext nicht online.

  Strokach, Evgeny and Zhukov, Victor / V. P. and Borovik, Igor and Sternin, Andrej and Haidn, Oskar J. (2021) Simulation of a GOx-GCH4 Rocket Combustor and the Effect of the GEKO Turbulence Model Coefficients. Aerospace, 8 (11). Multidisciplinary Digital Publishing Institute (MDPI). doi: 10.3390/aerospace8110341. ISSN 2226-4310. file

  Stützer, Robert and Balkenhohl, Jakob and Lauck, Felix and Oschwald, Michael (2021) Optical Properties of the Hypergolic Reaction Between Green Ionic Liquids and Highly Concentrated Hydrogen Peroxide. 7. Space Propulsion Conference, 17.-19. März 2021, Internet. Volltext nicht online.

  Stützer, Robert and Balkenhohl, Jakob and Lauck, Felix and Oschwald, Michael and Schlechtriem, Stefan (2022) The Hypergolic Reaction Between the Green Ionic Liquid EMIM SCN and Hydrogen Peroxide in a Lab-Scale Drop Test Chamber. International Journal of Energetic Materials and Chemical Propulsion, 1, pp. 87-100. Begell House. doi: 10.1615/IntJEnergeticMaterialsChemProp.2021038219. ISSN 2150-766X. file

  Stützer, Robert and Balkenhohl, Jakob and Lauck, Felix and Oschwald, Michael and Schlechtriem, Stefan (2021) The Hypergolic Reaction Between Green Ionic Liquids and Hydrogen Peroxide in a Lab-Scale Drop Test Chamber. The 12th International Symposium on Special Topics in Chemical Propulsion & Energetic Materials (ISICP), 22.-25. März 2021, Internet. Volltext nicht online.

  Suslov, Dmitry (2021) Brennkammerwandkühlung. Vorlesungsreihe Raumfahrtantriebe I, 11. Jun. 2021, Aachen, D. Volltext nicht online.

  Suslov, Dmitry (2022) Brennkammerwandkühlung. Vorlesungsreihe "Raumfahrtantriebe I", 24. Jun. 2022, online. Volltext nicht online.

T

  Tonti, Federica and Perovšek, Jaka and Usandivaras, José Z. and Karl, Sebastian and Hardi, Justin and Morii, Youhi and Oschwald, Michael (2021) Obtaining pseudo-OH∗ radiation images from CFD solutions of transcritical flames. Combustion and Flame. Elsevier. doi: 10.1016/j.combustflame.2021.111614. ISSN 0010-2180. file

  Tonti, Federica and Trotta, Luca and Hardi, Justin and Oschwald, Michael (2022) ACOUSTIC CHARACTERIZATION OF AN EXPERIMENTAL COMBUSTOR USING A COMBINED APPROACH WITH RANS SIMULATION AND AN ACOUSTIC LNS SOLVER. 2nd International Conference on Flight Vehicles, Aerothermodynamics and Re-entry Missions Engineering (FAR), 19. - 23. Juni 2022, Heilbronn. Volltext nicht online.

  Tonti, Federica and Usandivaras, José Z. and Perovšek, Jaka and Karl, Sebastian and Hardi, Justin and Oschwald, Michael (2021) Numerical reproduction of OH* radiation measurements of unsteady supercritical LOx/H2 combustion. In: Proceedings of the Symposium of Thermoaccoustics in Combustion 2021: Industry meets Academia. Symposium on Thermoacoustics in Combustion: Industry meets Academia (SoTiC 2021), 6. - 10. Sept. 2021, Munich, Germany. file

  Tonti, Federica and Usandivaras, José Zapata and Perovšek, Jaka and Karl, Sebastian and Hardi, Justin and Oschwald, Michael (2022) REST HF-9 Test Case: Numerical reproduction of OH*radiation measurements of unsteady supercritical LOx/H2 combustion. In: 9ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS). 9ᵀᴴ EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS), 27. Jun. - 1. Jul. 2022, Lille, F. file

  Traudt, Tobias and Börner, Michael and Suslov, Dmitry and Dos Santos Hahn, Robson Henrique and Saraf, Anirudh Mukund and Klein, Sebastian and Deeken, Jan C. and Hardi, Justin and Oschwald, Michael and Schlechtriem, Stefan (2022) Liquid Upper Stage Demonstrator Engine (LUMEN): Component Test Results and Project Progress. 73rd International Astronautical Congress, 18. - 22. Sep. 2022, Paris, France. file

  Traudt, Tobias and Börner, Michael and Suslov, Dmitry and Dos Santos Hahn, Robson Henrique and Saraf, Anirudh Mukund and Klein, Sebastian and Deeken, Jan C. and Hardi, Justin and Oschwald, Michael and Schlechtriem, Stefan (2022) Liquid Upper Stage Demonstrator Engine (LUMEN): A test bed for space propulsion components. In: 3rd Ground-based space facilities symposium 2022. 3rd Ground-Based Space Facilities Symposium, 6. - 8. Dez. 2022, Marseille, France. Volltext nicht online.

  Trotta, Luca (2022) Aeroacoustic modeling of a LOX/CH4 rocket engine for high-frequency combustion instability prediction analyses. Master's, Delft University of Technology. Volltext nicht online.

V

  Van Schyndel, Jan and Goos, Elke and Naumann, Clemens and Hardi, Justin and Oschwald, Michael (2022) Effects of Compounds in Liquefied Methane on Rocket Engine Operation. Aerospace. Multidisciplinary Digital Publishing Institute (MDPI). doi: 10.3390/aerospace9110698. ISSN 2226-4310. file

  Van Schyndel, Jan and Kaya, Dogan and Martin, Jan and Hardi, Justin (2022) Modification of a cryogenic rocket combustor informed by transcritical oxygen-methane combustion modelling. 4th International Seminar on Non-Ideal Compressible Fluid Dynamics (NICFD2022), 3. - 4. Nov. 2022, London, GB. Volltext nicht online.

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