|
[Sponsors] |
Accuracy when using upwind for interpolationSchemes in hypersonic flow |
|
LinkBack | Thread Tools | Search this Thread | Display Modes |
January 30, 2018, 21:30 |
Accuracy when using upwind for interpolationSchemes in hypersonic flow
|
#1 |
Senior Member
TWB
Join Date: Mar 2009
Posts: 414
Rep Power: 19 |
Hi,
I'm now running some hypersonic problems, such as double cone, concave ramp etc. In the interpolationSchemes, I used: reconstruct(rho) upwind; reconstruct(U) upwind; reconstruct(T) upwind; I tried all others but they caused the solution to diverge rather quickly. I even tried changing the scheme after running the upwind solution for a while, but the solution still diverges. 1st of all, am I restricted to using upwind scheme because it is upwind? Secondly, is using the upwind scheme acceptable for accuracy? Lastly, is there any other option I can do if my current accuracy is not acceptable? Thanks. |
|
February 1, 2018, 19:32 |
|
#2 |
Member
Hilbert
Join Date: Aug 2015
Location: Australia
Posts: 50
Rep Power: 11 |
Hi quarkz,
I assume you are running rhoCentral? I have found that Gamma schemes work best for the interpolation schemes. With the standard vanLeer interpolation the temperature solution isn't that great. If your solution diverges with the other schemes then there is probably an other issue, which is hard to diagnose without more info. |
|
February 6, 2018, 08:30 |
|
#3 |
Senior Member
TWB
Join Date: Mar 2009
Posts: 414
Rep Power: 19 |
Hi Hillie,
Thanks for the reply. I have tried most other changes, except for y+. The current grid is still too coarse in terms of y+. However, to reach y+ of even 50 at our Re, we will need maybe a few hundred millions to a billion, which is beyond our capability. We will try to see what else can be done. |
|
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
How is the accuracy using VOF (pressure based solver) on supersonic flow | air_fun | Fluent Multiphase | 1 | August 25, 2021 01:59 |
Hypersonic Flow simulation using Fluent | beanlee999 | FLUENT | 16 | February 5, 2020 21:09 |
Review: Reversed flow | CRT | FLUENT | 1 | May 7, 2018 06:36 |
Solver for hypersonic flow in OpenFoam | Santos-Dumont | OpenFOAM Running, Solving & CFD | 19 | October 21, 2012 02:42 |
Hypersonic flow scramjet | ishaninair | OpenFOAM Running, Solving & CFD | 0 | March 10, 2011 08:45 |