|
[Sponsors] |
December 26, 2006, 01:57 |
need information regarding nozzle flow
|
#1 |
Guest
Posts: n/a
|
hi, i am doing a nozzle flow analysis and i want to find out normal shock wave generated . can anybody help me in this regards
|
|
December 26, 2006, 13:35 |
Re: need information regarding nozzle flow
|
#2 |
Guest
Posts: n/a
|
do the geometry mesh it
use wall (boundary condition) for walls pressure inlet for the inlet pressure oulet for the outlet get your values for Mach_0, total pressure and total temperature. use K-W turbulence model with compressible correction. have fun, regards, |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
information from saved data files:Unsteady flow | Atul | FLUENT | 5 | July 27, 2008 20:05 |
Axisymmetirc Compressible Flow in a C/c and Nozzle | Nauman | FLUENT | 0 | December 21, 2004 07:40 |
Compressible flow in the nozzle | Saturn | FLUENT | 2 | November 29, 2004 04:22 |
NEED HELP! Flow through nozzle vanes with clerance | C K Tang | Fidelity CFD | 2 | July 29, 2003 13:07 |
Inviscid Drag at subsonic, subcritical Mach # | Axel Rohde | Main CFD Forum | 1 | November 19, 2001 12:19 |