Stagnation Temperature Effect on the Prandtl Meyer Function

The Prandtl Meyer (PM) function plays a significant role in the supersonic flows calculation. To design a supersonic nozzle giving a uniform and parallel flow at the exit section [1-3], it is necessary to deviate the nozzle at the throat of an initial expansion angle to have the desired exit Mach nu...

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Veröffentlicht in:	AIAA journal 2007-04, Vol.45 (4), p.952-954
1. Verfasser:	Zebbiche, Toufik
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Air flow Compressible flows shock and detonation phenomena Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Physics Shock-wave interactions and shock effects Temperature Temperature effects Turbulent flow
Online-Zugang:	Volltext
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