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：

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 17 条

[1]

ADAMS JC, 1971, AEDCTR71215 ARN ENG

[2]

Allen H. J., 1951, TR1048 NACA

[3]

Boltz FW, 1960, EFFECTS SWEEP ANGLE

[4]

Bursnall W.J., 1951, EXPT INVESTIGATION P

[5]

CHAPMAN GT, 1961, D1075 NASA TN

[6]

CLARKSON MH, 1976, J AIRCRAFT, V13, P565

GREGORY, N ;

STUART, JT ;

WALKER, WS .

[8]

MALCOLM GN, 1976, 9TH P AIAA AER TEST, P143

[9]

MCDEVITT JB, 1969, D5346 NASA TN

[10]

OWEN PR, 1952, TM277 ROYAL AIRCR ES