Heat transfer in the shock impingement zone around a cylinder in a hypersonic flow

被引：0
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作者：
Borovoi, V.Ya.
Struminskaya, I.V.
机构：
来源：
Fluid Dynamics | 1991年 / 26卷 / 03期
关键词：
Aerodynamics--Hypersonic - Cylinders - Flow of Fluids--Hypersonic - Shock Tubes - Shock Waves;
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摘要：
A systematic experimental investigation was made of the heat transfer in the shock interference zone for a laminar air boundary layer at high Mach numbers (15.5). The experiments were conducted over a broad range of variation of the slip angle embracing various types of shock wave interaction. The cylinder had a diameter of d = 25 mm, hemispheric ends of the same diameter, and the total length of 205 mm. The experiments were carried out in a shock tube. Experimental heat transfer data are presented.
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页码：415 / 420
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