METHOD FOR CALCULATING 3-DIMENSIONAL TURBULENT BOUNDARY-LAYER BY USING STREAMLINE COORDINATES

被引：0
作者：
HOTTA, T [1 ]
机构：
[1] HIROSHIMA UNIV,FAC ENGN,DEPT NAVAL ARCHITECTURE,HIROSHIMA,JAPAN
来源：
JAPANESE JOURNAL OF APPLIED PHYSICS | 1973年 / 12卷 / 06期
关键词：
D O I：
10.1143/JJAP.12.908
中图分类号：
O59 [应用物理学];
学科分类号：
摘要：
引用
收藏
页码：908 / 915
页数：8
相关论文
共 12 条
[1]  
BURI A, 1931, THESIS TH ZURICH
[2]  
COOKE JC, 1962, PROGR AERONAUTICAL S, V2
[3]  
COOKE JC, 1958, 3199 AER RES COUN RE
[4]   CALCULATION OF 3-DIMENSIONAL TURBULENT BOUNDARY LAYERS .I. FLOW OVER REAR OF AN INFINITE SWEPT WING [J].
CUMPSTY, NA ;
HEAD, MR .
AERONAUTICAL QUARTERLY, 1967, 18 :55-&
[5]  
HATANO S, 1971, J SOC NAV ARCH JAPAN, V130, P1
[6]  
HEAD MR, 1958, 3152 AER RES COUN RE
[7]  
INUI T, 1953, J SOC NAV ARCH JAPAN, V93, P11
[8]  
Ludwieg H., 1949, ING ARCH, V17, P288
[9]  
MAGER A, 1067 NAT ADV COMM AE
[10]  
TIMMAN R, 1955, P S BOUNDARY LAYER E
12