Laminar Near Wake of a Circular Cylinder at Hypersonic Speeds

The laminar near-wake flow behind a circular cylinder at hypersonic speeds has been examined experimentally and analytically. Surface pressure and heat flux measurements were obtained in a free-piston shock tunnel at a nominal Mach number of 10. The freestream unit Reynolds numbers were 3:02 x 10......

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Veröffentlicht in:	AIAA journal 2010-01, Vol.48 (1), p.236-248
Hauptverfasser:	Park, Gisu, Gai, Sudhir L, Neely, Andrew J
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Compressible flows shock and detonation phenomena Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Noise Physics Reynolds number Supersonic and hypersonic flows Turbulent flow Turbulent flows, convection, and heat transfer Velocity Wakes
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