High-speed air-breathing propulsion : papers presented at the AIAA Propulsion and Energy Forum 2021 : online, 9-11 August 2021 (Englisch)
- Neue Suche nach: AIAA Propulsion and Energy Forum
- Weitere Informationen zu AIAA Propulsion and Energy Forum:
- http://d-nb.info/gnd/1253520941
- Neue Suche nach: American Institute of Aeronautics and Astronautics
- Weitere Informationen zu American Institute of Aeronautics and Astronautics:
- http://d-nb.info/gnd/938-6
- Neue Suche nach: AIAA Propulsion and Energy Forum
- Weitere Informationen zu AIAA Propulsion and Energy Forum:
- http://d-nb.info/gnd/1253520941
- Neue Suche nach: American Institute of Aeronautics and Astronautics
- Weitere Informationen zu American Institute of Aeronautics and Astronautics:
- http://d-nb.info/gnd/938-6
2021
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ISBN:
- Konferenzband / Print
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Titel:High-speed air-breathing propulsion : papers presented at the AIAA Propulsion and Energy Forum 2021 : online, 9-11 August 2021
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Beteiligte:AIAA Propulsion and Energy Forum ( Autor:in ) / American Institute of Aeronautics and Astronautics ( Veranstalter:in )
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Kongress:AIAA Propulsion and Energy Forum ; 2021 ; Online
AIAA Propulsion and Energy Forum and Exposition ; 2021 ; Online -
Verlag:
- Neue Suche nach: Curran Associates, Inc.
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Erscheinungsort:Red Hook, NY
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Erscheinungsdatum:2021
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Format / Umfang:281 Seiten
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Anmerkungen:Illustrationen
Literaturangaben
Aufgrund der COVID-19-Pandemie als Online-Konferenz abgehalten (ursprünglicher Veranstaltungsort: Denver, CO) -
ISBN:
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Medientyp:Konferenzband
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Format:Print
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Sprache:Englisch
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Reportnr. / Förderkennzeichen:AIAA-2021-3523/AIAA-2021-3544
- Neue Suche nach: 55.50
- Weitere Informationen zu Basisklassifikation
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Schlagwörter:
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Klassifikation:
BKL: 55.50 Luftfahrzeugtechnik -
Datenquelle:
Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
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CHARACTERIZATION OF SUPERSONIC WIND TUNNEL FLOW QUALITY USING PLANAR LASER CO2 RAYLEIGH SCATTERINGMunoz, Camilo Aguilera / Sosa, Jonathan / Hyde, Evan W. / Goodwin, Gabriel B. / Kessler, David A. / Hess, Andrew M. / Miklosovic, David et al. | 2021
- 17
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CHARACTERIZATION OF THE CALTECH HYPERVELOCITY EXPANSION TUBE VIA TUNABLE DIODE LASER ABSORPTION SPECTROSCOPYSchwartz, Tal / Girard, Julian / Finch, Peter M. / Yu, Wesley / Lawson, Joel M. / Strand, Christopher L. / Austin, Joanna M. / Hornung, Hans G. / Hanson, Ronald K. et al. | 2021
- 26
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CHARACTERIZATION OF THE T5 REFLECTED SHOCK TUNNEL FREESTREAM TEMPERATURE, VELOCITY, AND COMPOSITION USING LASER ABSORPTION SPECTROSCOPYGirard, Julian / Finch, Peter M. / Schwartz, Tal / Yu, Wesley / Strand, Christopher L. / Austin, Joanna M. / Hornung, Hans G. / Hanson, Ronald K. et al. | 2021
- 48
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FUEL DISTRIBUTION MEASUREMENTS IN A HYPERSONIC COMBUSTOR FACILITYRosato, Daniel A. / Thornton, Mason / Reyes, Jonathan / Ahmed, Kareem A. et al. | 2021
- 53
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HIGH-SPEED DRAG MODELS FOR SUPERSONIC SPRAY COMBUSTION APPLICATIONOh, HyeJin / Ladeinde, Foluso et al. | 2021
- 59
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DUMP COMBUSTOR EXPERIMENTS OF MGB2 AND OTHER METAL MICROPARTICLESShin, Kyung-Hoon / Chang, Minwook / Gupta, Ashwani K. / Yu, Kenneth H. et al. | 2021
- 69
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STUDY OF DIRECT GAS INJECTION INTO STAGNATION ZONE OF BLUNT NOSE AT HYPERSONIC FLOWHarmon, Peter / Vashishtha, Ashish / Callaghan, Dean / Nolan, Cathal / Deiterding, Ralf et al. | 2021
- 82
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THERMAL-MECHANICAL DEFLECTION EFFECTS ON AERO-PROPULSIVE PERFORMANCE OF A REFERENCE HIGH-SPEED AIR-BREATHING VEHICLERiley, Logan P. / Zakrajsek, Andrew et al. | 2021
- 95
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INTEGRATED POWER AND THERMAL MANAGEMENT SYSTEM FOR HIGH SPEED AIRCRAFTStoia, Michael F. / Ek, Garrett W. / Bowcutt, Kevin G. / Needels, Jacob T. et al. | 2021
- 101
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COMPUTATIONAL ANALYSIS OF INTERNAL FLOW AND THERMAL ENVIRONMENT IN A SCRAMIJET ENGINE BEFORE IGNITIONKim, Jae-Eun / Jeong, Seung-Min / Choi, JeongYeol et al. | 2021
- 108
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LATERAL WALL TEMPERATURE EFFECTS IN A TRANSPIRATION COOLED SCRAMJET MODEL COMBUSTOR WITH SHOCK-BOUNDARY LAYER INTERACTIONStrauss, Friedolin T. / General, Stephan / Cragg, Patrick A. / Manassis, Konstantin / Schlechtriem, Stefan et al. | 2021
- 148
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PRESSURE EFFECTS IN A SCRAMIJET COMBUSTORLadeinde, Foluso et al. | 2021
- 156
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NUMERICAL SIMULATION OF COMBUSTION INSTABILITY IN A DIRECT-CONNECT SUPERSONIC COMBUSTORJeong, Seung-Min / Han, Hyung-Seok / Sung, Bu-Kyeng / Lee, Eun Sung / Choi, JeongYeol et al. | 2021
- 163
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LES INVESTIGATION OF NONEQUILIBRIUM FLOW IN A CAVITY-FLAMEHOLDING AXISYMMETRIC SCRAMJETLiu, Hang / Yao, Wei et al. | 2021
- 179
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LES MODELING OF DUO-MODEL SCRAMJET BY DYNAMIC ZONE FLAMELET MODELZhang, Zheng / Yao, Wei / Zhao, Wei et al. | 2021
- 190
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IMPLEMENTING A DUAL-MODE SCRAMJET COMBUSTOR MODEL IN NPSSConnolly, Brian J. / Krouse, Charles R. / Musgrove, Grant 0. et al. | 2021
- 199
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DESIGN OF SHAPE TRANSITION NOZZLE FOR DIRECT-CONNECT SUPERSONIC COMBUSTORSung, Bu-Kyeng / Choi, JeongYeol et al. | 2021
- 205
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EFFECT OF RAMP LEADING-EDGE BLUNT ON THE PERFORMANCE OF A MACH4 SCRAMJET INTAKESParamasivam, Senthilkumar / Sarout, Yuvraj / Islam, MD Didarul / R, Thundil Karuppa Raj et al. | 2021
- 219
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RELIABILITY BASED DESIGN OPTIMIZATION OF A SUPERSONIC ENGINE INLETTekaslan, Huseyin E. / Imrak, Rumed / Nikbay, Melike et al. | 2021
- 237
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LES INVESTIGATION OF REAL-FLUID EFFECT ON UNDEREXPANDED JETJin, Yichao / Yao, Wei et al. | 2021
- 247
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NONEQUILIBRIUM EFFECT MODELING IN HIGH-MA SCRAMJET BASED ON DYNAMIC ZONE MODELYao, Wei / Liu, Hang / Li, Long / Yue, Lianjie et al. | 2021
- 267
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NUMERICAL STUDY OF UNSTEADY SHOCK PROPAGATION IN A THERMALLY CHOKED FLOW WITH THE METHOD OF CHARACTERISTICSPee, Xiu Yi / Laurence, Stuart J. et al. | 2021