Hypersonic Lifting Body Windward Surface Flow-Field Analysis for High Angles of Incidence
- 1 February 1973
- report
- Published by Defense Technical Information Center (DTIC)
Abstract
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.Keywords
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