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...
Gespeichert in:
Veröffentlicht in: | Journal of aircraft 1994-11, Vol.31 (6), p.1429-1431 |
---|---|
1. Verfasser: | |
Format: | Artikel |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Schreiben Sie den ersten Kommentar!