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#41 |
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Member
Xinguang Wang
Join Date: Feb 2015
Posts: 45
Rep Power: 12 ![]() |
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 |
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#42 | |
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New Member
Aaron
Join Date: Apr 2016
Posts: 24
Rep Power: 11 ![]() |
Hi, foamers,
when I search the "neg", the officical document show this: Quote:
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#43 | ||
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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 |
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