Effects of shock wave impingement on supersonic film cooling

被引：0
|
作者：
Takita, Kenichi [1 ]
Masuya, Goro [1 ]
机构：
[1] Tohoku University, Sendai 980-8579, Japan
来源：
Journal of Spacecraft and Rockets | / 36卷 / 04期
关键词：
Mach number - Supersonic film cooling;
D O I：
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学科分类号：
摘要：
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页码：602 / 604
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