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
[7] ON THE STABILITY OF 3-DIMENSIONAL BOUNDARY LAYERS WITH APPLICATION TO THE FLOW DUE TO A ROTATING DISK
GREGORY, N
STUART, JT
WALKER, WS
[J]. PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1955, 248 (943) : 155 - 199
[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