scholarly journals Effect of Pressure Gradients on the Initiation of PBX-9502 via Irregular (Mach) Reflection of Low Pressure Curved Shock Waves

2016 ◽  
Author(s):  
Lawrence Mark Hull ◽  
Phillip Isaac Miller ◽  
Erik Allan Moro

2014 ◽  
Author(s):  
Carlo Lancellotti ◽  
Yubei Yue


2017 ◽  
Vol 24 (6) ◽  
pp. 063520 ◽  
Author(s):  
Rimpei Chiba ◽  
Yuta Ishikawa ◽  
Jun Hasegawa ◽  
Kazuhiko Horioka


1982 ◽  
Vol 123 ◽  
pp. 155-164 ◽  
Author(s):  
H. G. Hornung ◽  
M. L. Robinson

It is shown experimentally that, in steady flow, transition to Mach reflection occurs at the von Neumann condition in the strong shock range (Mach numbers from 2.8 to 5). This criterion applies with both increasing and decreasing shock angle, so that the hysteresis effect predicted by Hornung, Oertel & Sandeman (1979) could not be observed. However, evidence of the effect is shown to be displayed in an unsteady experiment of Henderson & Lozzi (1979).





Shock Waves ◽  
1998 ◽  
Vol 8 (2) ◽  
pp. 93-103 ◽  
Author(s):  
B.E. Milton ◽  
K. Takayama
Keyword(s):  


1979 ◽  
Vol 33 (4) ◽  
pp. 265-280 ◽  
Author(s):  
R. M. Bowen ◽  
P. J. Chen


Shock Waves ◽  
1996 ◽  
Vol 6 (1) ◽  
pp. 29-39
Author(s):  
B.E. Milton ◽  
R.D. Archer
Keyword(s):  


Sign in / Sign up

Export Citation Format

Share Document