SHOCK TUBE TEST TIME LIMITATION DUE TO TURBULENT-WALL BOUNDARY LAYER

被引：134

作者：

MIRELS, H

机构：

来源：

关键词：

D O I：

10.2514/3.2218

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：84 / 93

页数：10

共 16 条

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JOURNAL OF THE AEROSPACE SCIENCES, 1960, 27 (08) :587-594

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JONES JJ, 1957, NACA TN4072

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[9] TEST TIME IN LOW-PRESSURE SHOCK TUBES [J].

MIRELS, H .

[10]

MIRELS H, 1957, NACA TN4021