30. Hypersonic Boundary Layers and Flow Fields PDF Download
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Languages : en
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Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel
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Category : Aerodynamics, Hypersonic
Languages : en
Pages : 62
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Category :
Languages : en
Pages :
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Author: AGARD.
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Category :
Languages : en
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Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel
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Category :
Languages : en
Pages :
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Author: Allen H. Whitehead (Jr.)
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Category : Aerodynamics, Hypersonic
Languages : en
Pages : 44
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Flow field and drag characteristics of several laminar boundary layer tripping element in hypersonic flow.
Author: Advisory Group for Aerospace Research and Development
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Category :
Languages : en
Pages : 0
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Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development
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Category :
Languages : en
Pages :
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Author: North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development
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Category :
Languages : en
Pages :
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Author: John C. Adams (Jr.)
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Category : Aerodynamics, Hypersonic
Languages : en
Pages : 240
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Book Description
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.
