Optimization design of dual microjets for the shock wave/boundary layer interaction control in the supersonic flow
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DOI: 10.1063/5.0149490
Abstract: The shock wave/boundary layer interaction phenomenon is harmful to the performance improvement of the hypersonic vehicle, and the microjet flow control scheme was introduced to minimize the total volume of the separation bubble and maximize… read more here.
Keywords: wave boundary; layer interaction; boundary layer; shock wave ... See more keywords