|
[Sponsors] |
June 13, 2001, 11:54 |
supersonic flow
|
#1 |
Guest
Posts: n/a
|
mi problema es definir el volumen de calculo necesario para solucionar un problema de un transbordador que entra a la atmosfera a velocidad de dos Mach.
My problem is to define the fisic volume necesary to "solucionar" a problem of a transbordator that in to atmosfere a velocity of two Mach |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
back pressure at exit for supersonic flow | BigFrank | FLUENT | 6 | April 24, 2014 15:13 |
Probelm with supersonic exhaust to ambient | newj | CFX | 2 | August 9, 2012 18:01 |
Boundary Condition at outlet for supersonic flow | Benjamin Zachariah | FLUENT | 4 | April 22, 2007 23:47 |
Modeling Bleed in Supersonic Flow | Mohd Yousuf Ali | FLUENT | 0 | March 17, 2007 03:51 |
Inviscid Drag at subsonic, subcritical Mach # | Axel Rohde | Main CFD Forum | 1 | November 19, 2001 12:19 |