Structure of coherent instabilities in a supersonic shear layer

Detailed measurements have been made of the instabilities present in supersonic shear layers. A high-speed stream of Mach number 3 or 4 and a low-speed stream of Mach number 1.2 are produced and begin mixing at the trailing edge of the dividing centerbody.

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Bibliographische Detailangaben
Veröffentlicht in:	AIAA journal 1996-08, Vol.34 (8), p.1555-1561
Hauptverfasser:	Martens, Steven, Kinzie, Kevin W, McLaughlin, Dennis K
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Compressible flows shock and detonation phenomena Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Hydrodynamic stability Instability of shear flows Physics Supersonic and hypersonic flows
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Beschreibung
Zusammenfassung:	Detailed measurements have been made of the instabilities present in supersonic shear layers. A high-speed stream of Mach number 3 or 4 and a low-speed stream of Mach number 1.2 are produced and begin mixing at the trailing edge of the dividing centerbody.
ISSN:	0001-1452 1533-385X
DOI:	10.2514/3.13271