CALCULATION OF 3-DIMENSIONAL TURBULENT BOUNDARY LAYERS .2. ATTACHMENT-LINE FLOW ON AN INFINITE SWEPT WING

被引：21

作者：

CUMPSTY, NA

HEAD, MR

机构：

来源：

AERONAUTICAL QUARTERLY | 1967年 / 18卷

关键词：

D O I：

10.1017/S0001925900004169

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：150 / &

共 10 条

[1] CALCULATION OF 3-DIMENSIONAL TURBULENT BOUNDARY LAYERS .I. FLOW OVER REAR OF AN INFINITE SWEPT WING
CUMPSTY, NA
HEAD, MR
[J]. AERONAUTICAL QUARTERLY, 1967, 18 : 55 - &
[2] GARDOW EB, 1958, 42 MASS I TECHN GAS
[3] ON FLOW ALONG SWEPT LEADING EDGES
GASTER, M
[J]. AERONAUTICAL QUARTERLY, 1967, 18 : 165 - &
[4] GRAY WE, 1952, ARC15021
[5] HEAD MR, 1958, RM3152 ARC
[6] JOHNSTON JP, 1957, 39 MASS I TECHN GAS
[7] MAGER A, 1952, NACA1067 REP
[8] PRESTON JH, 1957, J FLUID MECH, V3, P373
[9] ROSENHEAD L, 1963, LAMINAR BOUNDARY ED
[10] THOMPSON BGJ, 1965, ARC26830