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Oblique shock wave with sweep
Authors:G. Emanuel
Affiliation:(1) School of Mechanical and Aerospace Engineering, University of Oklahoma, 73019-0601 Norman Oklahoma, USA
Abstract:An attached planar, oblique shock with sweep is investigated for the inviscid flow of a perfect gas. The ratio of specific heats, freestream Mach number, and wedge angle in the plane of the freestream velocity are prescribed, with the sweep angle as a free parameter. Explicit relations are provided for jump and detachment conditions. A number of trends, some non-intuitive, are discussed, e.g., the downstream Mach number may increase with sweep.
Keywords:Oblique shock wave  Shock wave detachment  Jump conditions with sweep
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