TRANSITION FROM REGULAR TO MACH REFLECTION OF SHOCK-WAVES .2. THE STEADY-FLOW CRITERION

被引：132

作者：

HORNUNG, HG

ROBINSON, ML

机构：

[1] DEF RES CTR,WEAPONS SYST RES LAB,SALISBURY,SOUTH AFRICA

[2] AUSTRALIAN NATL UNIV,FAC SCI,DEPT PHYS,CANBERRA,ACT 2600,AUSTRALIA

来源：

关键词：

D O I：

10.1017/S0022112082003000

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

页码：155 / 164

页数：10

共 14 条

[1]

Becker E., 1966, GASDYNAMIK

[2]

Courant R., 1948, SUPERSONIC FLOW SHOC

[3] EXPERIMENTS ON TRANSITION OF MACH REFLECTION [J].

HENDERSON, LF ;

LOZZI, A .

[4] FURTHER EXPERIMENTS ON TRANSITION TO MACH REFLECTION [J].

HENDERSON, LF ;

LOZZI, A .

[5]

HORNUNG HG, 1979, J FLUID MECH, V53, P149

[6]

HORNUNG HG, 1977, 11TH P INT S SHOCK T, P296

[7]

Landau L.D., 2013, COURSE THE ORETICAL

[8]

Liepmann H. W., 1957, ELEMENTS GASDYNAMICS

[9]

ROBINSON ML, 1980, 7TH P AUSTR FLUID ME

[10]

ROBINSON ML, 1970, HSA171 AUSTR WEAP RE