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• Rahman-Siikonen-Agarwal Model
  \eta = \alpha_2 T_t S, \quad \xi = \alpha_3 T_t W C_\nu = \frac{1}{2(1+T_t S \sqrt{1+\Re^2})}, \quad \zeta = T_t S max(1,\Re)
  4 KB (637 words) - 19:47, 8 July 2013
• DrivAer Model
  [4] S. Mack, T. Indinger, N. Adams, S. Blume, P. Unterlechner: The Interior Design of a 40% Scaled DrivAer Body a [5] S. Mack, T. Indinger, N. Adams, P. Unterlechner: The Ground Simulation Upgrad
  3 KB (425 words) - 09:32, 6 March 2013
• PFV4 mesh regrade
  % if a<1 then grade towards the edge(s)
  1,020 B (189 words) - 19:51, 15 March 2013
• PFVT convection matrix
  ZZ_Sc{m,k}= eu.S(nn(m,:),xa(k),ya(k)); S=zeros(2,nedofs); Sx=zeros(2,nedofs); Sy=zeros(2,nedofs);
  6 KB (856 words) - 20:59, 15 March 2013
• PFVT Tconvection matrix
  ZZ_Stc{m,k} =eu.S(nn(m,:),xa(k),ya(k)); TCm=zeros(nfT,nfT); S=zeros(2,nfV); g=zeros(1,nfT); G=zeros(2,nfT);
  5 KB (830 words) - 21:04, 15 March 2013
• PFVT Buoyancy matrix
  ZZ_Stb{m,k}= eu.S(nn(m,:),xa(k),ya(k)); Bm=zeros(nfV,nfT); S=zeros(2,nfV); g=zeros(1,nfT); % Allocate arrays
  5 KB (757 words) - 21:07, 15 March 2013
• PFVT get pressure
  ZZ_Spcd{m,k} =eu.S(nn(m,:),xa(k),ya(k)); S=zeros(2,nvdf); Sx=zeros(2,nvdf); Sy=zeros(2,nvdf); G=zeros(2,npdf);
  11 KB (1,613 words) - 21:10, 15 March 2013
• PFVT mesh regrade
  % if a<1 then grade towards the edge(s)
  1,020 B (189 words) - 21:12, 15 March 2013
• Palabos
  * [http://www.palabos.org/documentation/userguide/ Palabos User's Guide]
  1 KB (163 words) - 15:05, 3 April 2013
• COVISE
  since 2015 it s OpenSource and free for both academic and commercial users. Source code is
  416 B (64 words) - 16:01, 8 February 2015
• Sample code for BiCGSTAB - Fortran 90
  real (kind=wp), dimension(1:size(b, dim=1)) :: r, rs, v, p, s, t s = r - alpha*v !-------> LINE 10
  6 KB (451 words) - 07:14, 9 May 2018
• TwinMesh
  TwinMesh's [[Mesh generation|mesh generation]] employs the following meshing technique * [http://www.twinmesh.com TwinMesh's homepage]
  5 KB (676 words) - 09:51, 29 November 2023
• CONVERGE FAQ
  ===Will the triangle count in my CAD file affect my simulation’s runtime?=== ...simulation is than where it started (i.e., residuals). Further, CONVERGE’s variable time-step approach is fundamentally different than the fixed time-
  85 KB (13,492 words) - 15:51, 10 August 2020
• Wray-Agarwal(WA) Turbulence Model
  ..._{2 k \omega} \frac{R}{S} \frac{\partial R}{\partial x_{j}} \frac{\partial S}{\partial x_{j}}\\ ...\frac{\frac{\partial S}{\partial x_{j}} \frac{\partial S}{\partial x_{j}}}{S^{2}}\right), C_{m} \frac{\partial R}{\partial x_{j}} \frac{\partial R}{\par
  3 KB (458 words) - 17:19, 19 February 2021
• Wray-Agarwal(WA) turbulence Model
  ..._{2 k \omega} \frac{R}{S} \frac{\partial R}{\partial x_{j}} \frac{\partial S}{\partial x_{j}}\\ ...\frac{\frac{\partial S}{\partial x_{j}} \frac{\partial S}{\partial x_{j}}}{S^{2}}\right), C_{m} \frac{\partial R}{\partial x_{j}} \frac{\partial R}{\par
  3 KB (458 words) - 16:36, 19 February 2021
• Shuai-Agarwal Turbulence Model
  ...tial S}{\partial x_{i}} \frac{\partial S}{\partial x_{i}} \frac{v_{t}^{2}}{S^{2}}+\frac{\partial}{\partial x_{i}}\left(\left(\sigma v_{t}+v\right) \frac C_{\phi 1}=\left(\zeta_{1}-\zeta_{2}\left(\frac{\sqrt{\nu_{t}}}{L_{k} \sqrt{S}}\right)^{2}\right)
  4 KB (611 words) - 02:52, 8 April 2021
• Shuai-Agarwal turbulence Model
  ...tial S}{\partial x_{i}} \frac{\partial S}{\partial x_{i}} \frac{v_{t}^{2}}{S^{2}}+\frac{\partial}{\partial x_{i}}\left(\left(\sigma v_{t}+v\right) \frac C_{\phi 1}=\left(\zeta_{1}-\zeta_{2}\left(\frac{\sqrt{\nu_{t}}}{L_{k} \sqrt{S}}\right)^{2}\right)
  4 KB (617 words) - 19:43, 10 April 2021
• Ennova
  Ennova's geometry repair module offers automated as well as manual functions. It can
  3 KB (449 words) - 19:34, 15 February 2023
• ICEMCFD
  from Airbus. MULCAD was written in GPL (ICEM DDN's scripting language).
  1 KB (177 words) - 13:39, 17 February 2023