MACH REFLECTION ASSOCIATED WITH OVER-EXPANDED NOZZLE FREE JET FLOWS

被引:16
作者
CHOW, WL
CHANG, IS
机构
[1] UNIV ILLINOIS,URBANA,IL 61801
[2] LOCKHEED MISSILES & SPACE CO,HUNTSVILLE,AL
关键词
D O I
10.2514/3.60434
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:762 / 766
页数:5
相关论文
共 15 条
[1]   MACH DISK IN UNDEREXPANDED EXHAUST PLUMES [J].
ABBETT, M .
AIAA JOURNAL, 1971, 9 (03) :512-&
[2]  
Ashratov E.A, 1966, FLUID DYN, V1, P113
[3]   INTERACTION OF SHOCK WAVES [J].
BLEAKNEY, W ;
TAUB, AH .
REVIEWS OF MODERN PHYSICS, 1949, 21 (04) :584-605
[4]  
BUSEMAN A, 1949, TN1858 NACA
[5]   MACH DISK FROM UNDEREXPANDED AXISYMMETRIC NOZZLE-FLOW [J].
CHANG, IS ;
CHOW, WL .
AIAA JOURNAL, 1974, 12 (08) :1079-1082
[6]  
CHANG IS, 1973, THESIS U ILLINOIS
[7]   INTERACTION BETWEEN PRIMARY AND SECONDARY STREAMS OF SUPERSONIC EJECTOR SYSTEMS AND THEIR PERFORMANCE CHARACTERISTICS [J].
CHOW, WL ;
ADDY, AL .
AIAA JOURNAL, 1964, 2 (04) :686-695
[8]   MACH REFLECTION FROM OVEREXPANDED NOZZLE FLOWS [J].
CHOW, WL ;
CHANG, IS .
AIAA JOURNAL, 1972, 10 (09) :1261-&
[9]  
FERRI A, 1949, ELEMENTS AERODYNAMIC, P177
[10]   STRUCTURE OF JET PLUMES [J].
FOX, JH .
AIAA JOURNAL, 1974, 12 (01) :105-107