Base Flow of Circular Cylinder at Hypersonic Speeds

The paper presents a computational and an experimental investigation of base flow of a circular cylinder at hypersonic speeds. Effects of chemistry and wall temperature on the flow in the base region, at low to high enthalpies, are discussed. The experiments were conducted in a shock tunnel at a nom...

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Veröffentlicht in:	AIAA journal 2016-02, Vol.54 (2), p.458-468
Hauptverfasser:	Park, Gisu, Gai, Sudhir L, Neely, Andrew J
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Base flow Circular cylinders Computational fluid dynamics Diameters Enthalpy Fluid flow Heat flux High Reynolds number Hypersonic wind tunnels Low Reynolds number flow Mach number Mathematical models Pressure Reynolds number Shock tunnels Vorticity Wall temperature
Online-Zugang:	Volltext
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