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Hypersonic Lifting Body Windward Surface Flow-field Analysis for High Angles of Incidence
John C. Adams (Jr.)William R. Martindale
出版Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1973
URLhttp://books.google.com.hk/books?id=mkKkQc5Bgp0C&hl=&source=gbs_api
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註釋Formulation and application of a windward surface flow-field (inviscid and viscous) analysis is presented for general lifting body configurations at high angles of incidence under hypersonic perfect gas conditions. The technique applies a strip theory concept, leading to an infinite extent yawed body treatment applied in the windward surface crossflow plane for both the inviscid and viscous (boundary layer) flow fields. The boundary-layer analysis is based on the governing equations for yawed blunt body boundary layers.