Simulation of Supersonic Combustion Using Variable Turbulent Prandtl/Schmidt Number Formulation (Englisch)
- Neue Suche nach: Keistler, P.
- Neue Suche nach: Xiao, X.
- Neue Suche nach: Hassan, H.
- Neue Suche nach: Rodriguez, C.
- Neue Suche nach: American Institute of Aeronautics and Astronautics
- Neue Suche nach: Keistler, P.
- Neue Suche nach: Xiao, X.
- Neue Suche nach: Hassan, H.
- Neue Suche nach: Rodriguez, C.
- Neue Suche nach: American Institute of Aeronautics and Astronautics
In:
Aerodynamic measurement technology and ground testing conference
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AIAA Paper 2006-3733-2006-3902
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2006
- Aufsatz (Konferenz) / Print
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Titel:Simulation of Supersonic Combustion Using Variable Turbulent Prandtl/Schmidt Number Formulation
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Beteiligte:Keistler, P. ( Autor:in ) / Xiao, X. ( Autor:in ) / Hassan, H. ( Autor:in ) / Rodriguez, C. ( Autor:in ) / American Institute of Aeronautics and Astronautics
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Kongress:25th, Aerodynamic measurement technology and ground testing conference ; 2006 ; San Francisco, CA
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Erschienen in:Aerodynamic measurement technology and ground testing conference ; AIAA Paper 2006-3733-2006-3902AIAA MEETING PAPERS ON DISC -CD ROM EDITION- ; AIAA Paper 2006-3733-2006-3902
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Verlag:
- Neue Suche nach: AIAA,
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Erscheinungsdatum:01.01.2006
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Format / Umfang:AIAA Paper 2006-3733-2006-3902
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Anmerkungen:Including 25th AIAA aerodynamic measurement technology and ground testing conference 24th AIAA applied aerodynamics conference; 3rd AIAA flow control conference; 36th AIAA fluid dynamics conference and exhibit; 37th AIAA plasmadynamics and lasers conference; 9th AIAA/ASME joint thermophysics and heat transfer conference.; Paper numbers 2006-2805 to 2006-3925 with gaps held. Held on CD-ROM.; Shelved in Conference Index - see disc 11 for papers from the 25th Aerodynamic measurement technology and ground testing conference
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Medientyp:Aufsatz (Konferenz)
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Format:Print
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Sprache:Englisch
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Schlagwörter:
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Datenquelle:
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