|
[Sponsors] | |||||
|
|
|
#1 |
|
Guest
Posts: n/a
|
Hi, I am trying to model hypersonic flow around a blunt body. I could go upto Mach number 3.5 after which the solution diverges. Any thoughts please? I am using the following Operating pressure 101325 Pa
If I make the operating pressure to 0 I get floating point error. I am relatively new to CFD and FLUENT. Thanks, Subramani |
|
|
||
![]() |
| Thread Tools | Search this Thread |
| Display Modes | |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| mass flow in is not equal to mass flow out | saii | CFX | 12 | March 19, 2018 06:21 |
| Eul-Eul flow, k-e-kp-ep-Theta Turbulence model | us | FLUENT | 5 | April 5, 2011 03:29 |
| Ho to model the flow in a Regenerator | alexandrepereira | OpenFOAM Running, Solving & CFD | 2 | August 25, 2010 18:35 |
| Cavitation model with non-isothermal flow | pitisrisuk | CFX | 0 | July 14, 2009 15:30 |
| TCL model for channel flow | Hui | Main CFD Forum | 2 | July 26, 2008 00:28 |