|
[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 | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
mass flow in is not equal to mass flow out | saii | CFX | 12 | March 19, 2018 05:21 |
Eul-Eul flow, k-e-kp-ep-Theta Turbulence model | us | FLUENT | 5 | April 5, 2011 02:29 |
Ho to model the flow in a Regenerator | alexandrepereira | OpenFOAM Running, Solving & CFD | 2 | August 25, 2010 17:35 |
Cavitation model with non-isothermal flow | pitisrisuk | CFX | 0 | July 14, 2009 14:30 |
TCL model for channel flow | Hui | Main CFD Forum | 2 | July 25, 2008 23:28 |