Mode switching in supersonic circular jets

An underexpanded supersonic circular jet was studied experimentally in a pressure ratio range of 2–15, yielding an equivalent Mach number range of 1.1–2.4 downstream of the nozzle. Spark Schlieren photography and near‐field pressure measurements showed large changes in the jet structure for differen...

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Veröffentlicht in:	Physics of fluids. A, Fluid dynamics Fluid dynamics, 1989-05, Vol.1 (5), p.868-873
Hauptverfasser:	Gutmark, E., Schadow, K. C., Bicker, C. J.
Format:	Artikel
Sprache:	eng
Schlagworte:	Compressible flows shock and detonation phenomena Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Physics
Online-Zugang:	Volltext
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