Shock boundary layer interaction under the influence of a normal suction slot
作者： A. Weiss , H. Olivier
DOI: 10.1007/S00193-013-0456-5
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摘要: The phenomenon of shock boundary layer interaction a train under the influence normal suction slot is studied. In previous work, it was found that normal, circumferential sufficient to stabilize primary in as much back pressure can be increased until gradually changes into single shock. Based on experimental and numerical results, flow model derived which explains transition suction. this validated against cases with different upstream Mach Reynolds numbers. For purpose three nozzle flows are investigated at various total levels. second step, extended oblique case, correlating mass distribution incoming static downstream Finally, cavity onto considered.
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