COMPARISON OF THEORETICAL AND EXPERIMENTAL RESULTS FOR THE TURBULENT BOUNDARY LAYER IN SUPERSONIC FLOW ALONG A FLAT PLATE

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作者：
FERRARI, C
机构：
来源：
JOURNAL OF THE AERONAUTICAL SCIENCES | 1951年 / 18卷 / 08期
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D O I：
10.2514/8.2035
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
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页码：555 / 564
页数：10
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