SHOCK-INDUCED SEPARATION OF A LAMINAR BOUNDARY LAYER IN SUPERSONIC FLOW PAST A CONVEX CORNER

被引：1

|

作者：

CURLE, N

机构：

来源：

AERONAUTICAL QUARTERLY | 1965年 / 16卷

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D O I：

10.1017/S0001925900003267

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

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页码：33 / &

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