NUMERICAL ANALYSIS OF HEAT TRANSFER ON THE SURFACE OF A DELTA WING IN A HYPERSONIC AIR FLOW AT LARGE ANGLES OF ATTACK.

被引：0
|
作者：
Afonina, N.E.
Vlasov, A.Yu.
Gromov, V.G.
机构：
来源：
Fluid Dynamics | 1984年 / 19卷 / 05期
关键词：
AERODYNAMICS - Hypersonic - GASES - Thermodynamics - HEAT TRANSFER - Boundary Layer - SHOCK WAVES - Mathematical Models;
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学科分类号：
摘要：
The heat transfer on a delta wing with blunt edges and various catalytic surface properties in a hypersonic air flow at 40 degree and 60 degree angles of attack has been investigated by a numerical flow model for a viscous reacting gas in the shock layer near the windward side of blunt elongated bodies.
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页码：845 / 848
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