SECONDARY FLOW EFFECTS ON GAS EXIT ANGLES IN RECTILINEAR CASCADES

被引:3
作者
BARDON, MF
MOFFATT, WC
RANDALL, JL
机构
[1] CANADIAN ARMED FORCES,FORCES BASE,CALGARY,ALBERTA,CANADA
[2] ROY MIL COLL CANADA,DEPT MECH ENGN,KINGSTON,ONTARIO,CANADA
[3] CANADIAN ARMED FORCES,AEROSP ENGN & TEST ESTAB,COLD LAKE,ALBERTA,CANADA
来源
JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME | 1975年 / 97卷 / 01期
关键词
D O I
10.1115/1.3445929
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
引用
收藏
页码:93 / 100
页数:8
相关论文
共 21 条
[11]  
Lakshminarayana B., 1963, INT J MECH SCI, V5, P287, DOI [10.1016/0020-7403(63)90055-9, DOI 10.1016/0020-7403(63)90055-9]
[12]  
LAKSHMINARAYANA B, 1963, THESIS LIVERPOOL U
[13]  
LAKSHMINARAYANA B, 1967, T ASME D, V89, P191
[14]  
LOOS HG, 1952, J AERONAUT SCI, V19, P646
[15]  
LOOS HG, 1953, 3 CAL I TECHN TECHN
[16]  
LOUIS JF, 1960, 3136 AER RES COUNC R
[17]   A SIMPLE APPROACH TO THE THEORY OF SECONDARY FLOWS [J].
PRESTON, JH .
AERONAUTICAL QUARTERLY, 1954, 5 (03) :218-234
[18]  
SCHLICHTING H, 1966, T ASME D, V88, P221
[19]   THE SECONDARY FLOW IN A CASCADE OF AIRFOILS IN A NONUNIFORM STREAM [J].
SQUIRE, HB ;
WINTER, KG .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1951, 18 (04) :271-277
[20]  
STRATFORD BS, 1967, ASME67WAGT7 PAP