EFFECT OF MASS INJECTION ON THE DRAG OF A SLENDER CONE IN HYPERSONIC FLOW

被引：11

|

作者：

KING, HH

TALBOT, L

机构：

来源：

AIAA JOURNAL | 1964年 / 2卷 / 05期

关键词：

D O I：

10.2514/3.2439

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

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页码：836 / 844

页数：9

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