THE PRESSURE RISE AT SHOCK-INDUCED TURBULENT BOUNDARY-LAYER SEPARATION IN 3-DIMENSIONAL SUPERSONIC FLOW

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作者：

STALKER, RJ

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JOURNAL OF THE AERONAUTICAL SCIENCES | 1957年 / 24卷 / 07期

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V [航空、航天];

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08 ; 0825 ;

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页码：547 / 547

页数：1

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