THE IMPACT OF A SHOCK-WAVE ON A THIN 2-DIMENSIONAL AEROFOIL MOVING AT SUPERSONIC SPEED

被引：26

作者：

SMYRL, JL

机构：

来源：

关键词：

D O I：

10.1017/S0022112063000197

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

页码：223 / &

共 8 条

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