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

被引：26

作者：

DAVIDOR, W

PENNER, SS

机构：

来源：

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

页码：1651 / &

共 9 条

[1] ABDELHAMID AN, 1969, AIAA69665 PAP
[2] ON THE STRUCTURE OF JETS FROM HIGHLY UNDEREXPANDED NOZZLES INTO STILL AIR
ADAMSON, TC
NICHOLLS, JA
[J]. JOURNAL OF THE AEROSPACE SCIENCES, 1959, 26 (01): : 16 - 24
[3] BOWYER J, 1963, GDA630586
[4] STUDY OF HIGHLY UNDEREXPANDED SONIC JET
CRIST, S
SHERMAN, PM
GLASS, DR
[J]. AIAA JOURNAL, 1966, 4 (01) : 68 - &
[5] LOCATION OF THE NORMAL SHOCK WAVE IN THE EXHAUST PLUME OF A JET
EASTMAN, DW
RADTKE, LP
[J]. AIAA JOURNAL, 1963, 1 (04) : 918 - 919
[6] NORMAL SHOCK LOCATION IN UNDEREXPANDED GAS AND GAS-PARTICLE JETS
LEWIS, CH
CARLSON, DJ
[J]. 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
WEGENER, PP
[J]. PHYSICS OF FLUIDS, 1959, 2 (03) : 264 - 275