Computational study of plume-induced separation on a hypersonic powered model

The computation of hypersonic air-breathing vehicle flowfields under simulated powered conditions is discussed. Evidence shows that for representative conditions at a freestream Mach 10, the flow separation was predicted on a generic configuration and resulted in a negligible difference in lift and...

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Veröffentlicht in:	Journal of aircraft 1994-11, Vol.31 (6), p.1429-1431
1. Verfasser:	Huebner, L. D
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Applied sciences Energy Energy. Thermal use of fuels Engines and turbines Equipments for energy generation and conversion: thermal, electrical, mechanical energy, etc Exact sciences and technology
Online-Zugang:	Volltext
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Beschreibung
Zusammenfassung:	The computation of hypersonic air-breathing vehicle flowfields under simulated powered conditions is discussed. Evidence shows that for representative conditions at a freestream Mach 10, the flow separation was predicted on a generic configuration and resulted in a negligible difference in lift and thrust.
ISSN:	0021-8669 1533-3868
DOI:	10.2514/3.46673