Hypersonic inviscid and viscous flow over a wedge and cone

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Univ of Oklahoma, Norman, United States ^{[1
]}

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来源：

J Aircr | / 2卷 / 385-391期

关键词：

Boundary layers - Cones - Drag - Heat transfer coefficients - Hypersonic aerodynamics - Laminar flow - Parameter estimation - Pressure - Reynolds number - Specific heat - Temperature - Viscous flow;

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引用

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LEUNG, KK
EMANUEL, G
JOURNAL OF AIRCRAFT, 1995, 32 (02): : 385 - 391
[2] HYPERSONIC VISCOUS FLOW OVER AN INCLINED WEDGE
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RODKIEWICZ, CM
AIAA JOURNAL, 1974, 12 (01) : 7 - 8
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CHEUNG, S
FLORES, J
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[5] Convergence acceleration of viscous and inviscid hypersonic flow calculations
Cheung, S., 1600, (29):
[6] VISCOUS INTERACTION PHENOMENA IN HYPERSONIC WEDGE FLOW
de Luca, L
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de la Chevalerie, DA
Fonteneau, A
AIAA JOURNAL, 1995, 33 (12) : 2293 - 2298
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CHANG, PK
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OH, SK
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[8] Viscous shock layer on a cone in hypersonic flow
Poplavskaya, TV
HIGH TEMPERATURE, 2002, 40 (02) : 228 - 233
[9] Viscous Shock Layer on a Cone in Hypersonic Flow
T. V. Poplavskaya
High Temperature, 2002, 40 : 228 - 233
[10] VISCOUS HYPERSONIC FLOW PAST A SLENDER CONE
STEWARTSON, K
PHYSICS OF FLUIDS, 1964, 7 (05) : 667 - 675

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