THE EFFECTS OF HEAT TRANSFER ON LAMINAR-BOUNDARY-LAYER SEPARATION IN SUPERSONIC FLOW

被引：14

作者：

CURLE, N

机构：

来源：

AERONAUTICAL QUARTERLY | 1961年 / 12卷 / 04期

关键词：

D O I：

10.1017/S0001925900002122

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：309 / 336

页数：28

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