INFLUENCE OF SHOCK-WAVE ATTENUATION BY BOUNDARY-LAYER GROWTH ON CONTACT-SURFACE MOTION IN A SHOCK TUBE

被引：5

|

作者：

ROSCISZEWSKI, J

机构：

来源：

JOURNAL OF THE AEROSPACE SCIENCES | 1959年 / 26卷 / 06期

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D O I：

10.2514/8.8098

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：388 / 389

页数：2

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