Three-dimensional viscous flow computations of high area ratio nozzles for hypersonic propulsion

The PARC3D code was selected by the authors to analyze a variety of complex and high-speed flow configurations. Geometries considered for code validation include ramps and corner flows, which are characteristic of inlets and nozzles. Flows with Mach numbers of 3-14 were studied. Both two- and three-...

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Veröffentlicht in:	Journal of propulsion and power 1991-01, Vol.7 (2), p.84-89
Hauptverfasser:	Reddy, DR, Harloff, G J
Format:	Artikel
Sprache:	eng
Schlagworte:	nozzles supersonic flow viscous flow
Online-Zugang:	Volltext
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