AERODYNAMIC HEATING IN THE REGION OF SHOCK AND TURBULENT BOUNDARY LAYER INTERACTION INDUCED BY A CYLINDER

被引：1
|
作者：
唐贵明 [1 ]
俞鸿儒 [1 ]
机构：
[1] Institute of Mechanics,Chinese Academy of Sciences,Beijing 100080,China
来源：
Acta Mechanica Sinica | 1992年 / 03期
关键词：
shock wave; boundary layer; aerodynamic heating;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Detailed distributions of heat flux in the region of shock wave and turbulent boundary layerinteraction induced by a cylinder were measured in the shock tunnel Oil flow patterns and Schlieren photo-graphs were taken.Empirical relations were given for determining separation shock angle,peaks of heat fluxand their locations on both cylinder leading edge and flat plate surface,and other characteristic parameters ofthe interaction region.
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页码：224 / 230
页数：7
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