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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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.

引用

页码：19 / 24

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