COMPUTATIONS OF SUPERSONIC-FLOW OVER A MISSILE AFTERBODY CONTAINING AN EXHAUST JET

被引：9

|

作者：

SAHU, J

机构：

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1987年 / 24卷 / 05期

关键词：

D O I：

10.2514/3.25931

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：403 / 410

页数：8

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