THE EFFECT OF A SIMPLE THROAT DISTORTION ON THE FLOW IN A HYPERSONIC WIND-TUNNEL NOZZLE

被引：0

作者：

OLIVER, RE

CUMMINGS, BE

机构：

来源：

JOURNAL OF THE AERONAUTICAL SCIENCES | 1957年 / 24卷 / 06期

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暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：466 / 467

页数：2

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