|
[Sponsors] |
November 5, 2015, 05:55 |
|
#41 |
Member
Xinguang Wang
Join Date: Feb 2015
Posts: 45
Rep Power: 11 |
Dear Luca
I ran a supersonic flat plate flow with turbulence, but when I change different limiter of: reconstruct(rho) Minmod; reconstruct(U) Minmod; reconstruct(T) Minmod; such as Minmod, vanLeer, and superBee, the skin friction is quite differnt from each other, the minmod gave the highest value, while the superBee gave the lowest. As for a supersonic flat plate, there is no shock in the boundary layer, i do not know why there is so much difference, when I look into the U file alone y direction, near the wall the limiters influence it. Do you noticed that when you did some simulation? regards, Jason |
|
August 3, 2016, 10:10 |
|
#42 | |
New Member
Aaron
Join Date: Apr 2016
Posts: 24
Rep Power: 10 |
Hi, foamers,
when I search the "neg", the officical document show this: Quote:
|
||
January 25, 2024, 05:05 |
|
#43 | ||
Member
Carmelo Baronetto
Join Date: Dec 2023
Posts: 31
Rep Power: 3 |
Quote:
Good morning, sorry to reopen this old thread, but I'm studying rhoCentraFoam and I would like to understand better how this solver works. I can't understand when David writes: Quote:
rho_neg[i+1/2] = rho[i+1] + drho[i+1]*(x[i+1/2] - x[i+1]) Is it corret, or am I missing something? In general, refers to the article: "Implementation of semi-discrete, non-staggered central schemes in a colocated, polyhedral, finite volume framework, for high-speed viscous flows" by C.J. Greenshields et Al. it is explained how to compute positive interpolation of a general quantity: where: However I can't understand how to compute . I hope someone can help me. Thank you |
|||
|
|
Similar Threads | ||||
Thread | Thread Starter | Forum | Replies | Last Post |
Thermophysicalproperties in rhoCentralFoam | srinath | OpenFOAM Running, Solving & CFD | 12 | October 2, 2012 11:04 |
RhoCentralFoam Steady State | kieranwood85 | OpenFOAM Running, Solving & CFD | 0 | January 9, 2009 19:50 |
RhocentralFoam | ehsan | OpenFOAM Running, Solving & CFD | 0 | November 19, 2008 06:35 |
how to get the detail information about k-e models | limingtiger | Siemens | 1 | July 15, 2005 05:22 |
HVN tell me the detail of relative pressure | chong chee nan | FLUENT | 1 | January 2, 2002 05:55 |