|
[Sponsors] | |||||
|
|
|
#1 |
|
Guest
Posts: n/a
|
Hi I am trying to generate a shockwave around a circle in 2d using fluent 5.5. However once I go above mach 2 divergence occurs and I can't seem to get the velocity any higher. I am using a far field pressure boundary and a coupled implicit solver. Does anyone have any pointers for me?
|
|
|
||
![]() |
| Thread Tools | Search this Thread |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Supersonic flow over a flat plate and a blunt body. | Maddy | FLUENT | 0 | August 31, 2010 17:35 |
| demo free flow blunt body in cfx ansys 11 | jan | CFX | 1 | July 31, 2007 20:44 |
| recirculation region after blunt body | Zhihua | FLUENT | 0 | August 11, 2004 14:52 |
| Grid singularity in blunt body simulations | Stefan | Main CFD Forum | 8 | August 4, 2001 23:33 |
| finite volume method for CFD analysis of 2D blunt body | Aditya Vaze | Main CFD Forum | 1 | January 19, 2000 14:55 |