Plane-parallel supersonic flow with a discontinuity
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This article considers a plant-parallel supersonic flow, with a shock wave terminating within the flow; the shock wave is regarded as a distortion. A line of discontinuity is located ahead of the shock wave in the supersonic zone. The problem is solved by the method of indeterminate coefficients.
KeywordsShock Wave Supersonic Flow Supersonic Zone Indeterminate Coefficient
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