Viscous interaction phenomena in hypersonic wedge flow

An experimental investigation carried out to study some aspects of shock/boundary-layer interaction in a nominally two-dimensional hypersonic wedge flow is described.

Bibliographische Detailangaben

Veröffentlicht in:	AIAA journal 1995-12, Vol.33 (12), p.2293-2298
Hauptverfasser:	de Luca, Luigi, Cardone, Gennaro, de la Chevalerie, Dominique Aymer, Fonteneau, Alain
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Aviation Compressible flows shock and detonation phenomena Exact sciences and technology Experiments Fluid dynamics Fundamental areas of phenomenology (including applications) Physics Shock-wave interactions and shock effects Shock-wave interactions and shockeffects
Online-Zugang:	Volltext
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