EFFECT OF SHOCK-INDUCED VORTICITY ON THE COMPRESSIBLE BOUNDARY LAYER ALONG A FLAT PLATE

被引：0

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作者：

TING, L

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来源：

AIAA JOURNAL | 1964年 / 2卷 / 03期

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D O I：

10.2514/3.2342

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

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页码：490 / 493

页数：4

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