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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