CALCULATION OF FLOW ON A CONE AT HIGH ANGLE OF ATTACK

被引：50

作者：

LUBARD, SC

HELLIWELL, WS

机构：

[1] AEROSP CORP, EL SEGUNDO, CA USA

[2] R&D ASSOC, SANTA MONICA, CA 90403 USA

来源：

AIAA JOURNAL | 1974年 / 12卷 / 07期

关键词：

D O I：

10.2514/3.49388

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：965 / 974

页数：10

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