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
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