ON THE EFFECT OF REYNOLDS NUMBER UPON THE PEAK PRESSURE-RISE COEFFICIENT ASSOCIATED WITH THE SEPARATION OF A TURBULENT BOUNDARY LAYER IN SUPERSONIC FLOW

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LOVE, ES
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JOURNAL OF THE AERONAUTICAL SCIENCES | 1955年 / 22卷 / 05期
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V [航空、航天];
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08 ; 0825 ;
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页码：345 / 345
页数：1
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