SERIES SOLUTIONS FOR SHOCK-TUBE LAMINAR BOUNDARY LAYER AND TEST TIME

被引：16

|

作者：

MIRELS, H

KING, WS

机构：

来源：

AIAA JOURNAL | 1966年 / 4卷 / 05期

关键词：

D O I：

10.2514/3.3547

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：782 / &

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