INTERPRETATION OF PRESSURE MEASUREMENTS BEHIND REFLECTED SHOCK IN A RECTANGULAR SHOCK TUBE

被引：12

|

作者：

SANDERSON, RJ

机构：

来源：

AIAA JOURNAL | 1969年 / 7卷 / 07期

关键词：

D O I：

10.2514/3.5352

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：1370 / +

页数：1

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