Boundary-Layer Displacement and Leading-Edge Bluntness Effects in High-Temperature Hypersonic Flow
作者： H. K. CHENG , J. GORDON HALL , T. C. GOLIAN , A. HERTZBERG
DOI: 10.2514/8.9002
关键词:
摘要: … flow model consisting of a laminar boundary layer adjacent to the body and an in viscid outer flow … the bodies thin, the lateral extent of the flow field bounded by the bow shock is small. …
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