Flowfield surveys and computations of a crossing-shock wave/boundary-layer interaction

A joint experimental and computational study that examined the flowfield structure created by two crossing oblique shock waves interacting with a turbulent boundary layer is described.

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Bibliographische Detailangaben
Veröffentlicht in:	AIAA journal 1996-01, Vol.34 (1), p.50-56
Hauptverfasser:	Garrison, T. J, Settles, G. S, Narayanswami, N, Knight, D, Horstman, C. C
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft Aviation Boundary layer and shear turbulence Boundary layers Compressible flows shock and detonation phenomena Computational fluid dynamics Dynamic response Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Mathematical models Physics Shock waves Shock-wave interactions and shock effects Shock-wave interactions and shockeffects Turbulence Turbulent flows, convection, and heat transfer Viscosity Wind tunnels
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Beschreibung
Zusammenfassung:	A joint experimental and computational study that examined the flowfield structure created by two crossing oblique shock waves interacting with a turbulent boundary layer is described.
ISSN:	0001-1452 1533-385X
DOI:	10.2514/3.13020