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;

D O I：

暂无

中图分类号：

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.

引用

页码：845 / 848

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