HEAT TRANSFER IN THE ZONE OF INTERACTION BETWEEN A SHOCK AND THE BOUNDARY LAYER.

被引：0
|
作者：
Baryshev, Yu.V.
Roxhdestvenskiy, V.I.
Leont'yev, A.I.
机构：
来源：
Heat Transfer - Soviet Research | 1975年 / 7卷 / 06期
关键词：
641 Heat and Mass Transfer; Thermodynamics;
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暂无
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学科分类号：
摘要：
A study of heat transfer rates for high temperature gas turbines was made. The results indicate a sharp increase of heat transfer rates in the downstream region of a shock. The effect of shock strength and the boundary layer thickness on increase in heat transfer is investigated. Data are obtained on the effect of a shock on the efficiency of a thermal-protection gas blanket. Practical recommndations are given for calculating the heat transfer in the zone of interaction between a shock and a turbulent boundary layer.
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页码：19 / 24
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