SUBSONIC, HIGH-ANGLE-OF-ATTACK FLOW INVESTIGATION AT SEVERAL REYNOLDS-NUMBERS

被引：8

作者：

CLARKSON, MH ^{[1
]}

MALCOLM, GN ^{[1
]}

CHAPMAN, GT ^{[1
]}

机构：

[1] NASA,AMES RES CTR,AERODYNAM RES BRANCH,MOFFETT FIELD,CA 94035

来源：

AIAA JOURNAL | 1978年 / 16卷 / 01期

关键词：

D O I：

10.2514/3.60856

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：53 / 60

页数：8

共 50 条

[1] A NUMERICAL INVESTIGATION FOR CURVED FLOW AT HIGH REYNOLDS-NUMBERS
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[9] FLOW IN CYLINDRICAL CHANNELS WITH OBSTRUCTIONS AT HIGH REYNOLDS-NUMBERS
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[10] STEADY FLOW IN A SUDDEN EXPANSION AT HIGH REYNOLDS-NUMBERS
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