INFLUENCE OF THE LEADING-EDGE SHOCK WAVE ON THE LAMINAR BOUNDARY LAYER AT HYPERSONIC SPEEDS

被引：7

|

作者：

LEES, L

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1956年 / 23卷 / 06期

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D O I：

10.2514/8.3614

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

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页码：594 / &

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