SHOCK STANDOFF DISTANCES AND MACH-DISK DIAMETERS IN UNDEREXPANDED SONIC JETS

被引:26
作者
DAVIDOR, W
PENNER, SS
机构
关键词
D O I
10.2514/3.6410
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:1651 / &
相关论文
共 9 条
[1]  
ABDELHAMID AN, 1969, AIAA69665 PAP
[2]   ON THE STRUCTURE OF JETS FROM HIGHLY UNDEREXPANDED NOZZLES INTO STILL AIR [J].
ADAMSON, TC ;
NICHOLLS, JA .
JOURNAL OF THE AEROSPACE SCIENCES, 1959, 26 (01) :16-24
[3]  
BOWYER J, 1963, GDA630586
[4]   STUDY OF HIGHLY UNDEREXPANDED SONIC JET [J].
CRIST, S ;
SHERMAN, PM ;
GLASS, DR .
AIAA JOURNAL, 1966, 4 (01) :68-&
[5]   LOCATION OF THE NORMAL SHOCK WAVE IN THE EXHAUST PLUME OF A JET [J].
EASTMAN, DW ;
RADTKE, LP .
AIAA JOURNAL, 1963, 1 (04) :918-919
[6]   NORMAL SHOCK LOCATION IN UNDEREXPANDED GAS AND GAS-PARTICLE JETS [J].
LEWIS, CH ;
CARLSON, DJ .
AIAA JOURNAL, 1964, 2 (04) :776-777
[7]  
Love E.S., 1959, TRR6 NASA
[8]  
PENNER SS, TO BE PUBLISHED
[9]   SUPERSONIC NOZZLE FLOW WITH A REACTING GAS MIXTURE [J].
WEGENER, PP .
PHYSICS OF FLUIDS, 1959, 2 (03) :264-275