Oblique shock wave with sweep |
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Authors: | G. Emanuel |
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Affiliation: | (1) School of Mechanical and Aerospace Engineering, University of Oklahoma, 73019-0601 Norman Oklahoma, USA |
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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. |
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Keywords: | Oblique shock wave Shock wave detachment Jump conditions with sweep |
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