A DOUBLE-DIAPHRAGM SHOCK TUBE TO PRODUCE TRANSIENT HIGH MACH NUMBER FLOWS

被引：4

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作者：

BERNSTEIN, H

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1953年 / 20卷 / 11期

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D O I：

10.2514/8.2844

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

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页码：790 / 791

页数：2

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