Search results

Create the page "S" on this wiki!

Page title matches

• FAQ's
  :FAQ's about CFD-Wiki. [[Category: FAQ's]]
  1 KB (215 words) - 17:50, 12 December 2017
• Stratford's separation criterion
  ...sess if a turbulent boundary layer is likely to separate or not. Stratford's criteria says that from the start of the pressure recovery where the max ve ... used <math>k = 0.5</math>, which is a bit less conservative than Statford's original values.
  3 KB (543 words) - 11:10, 11 December 2013

Page text matches

• Main Page
  ===[[FAQ's]]===
  6 KB (823 words) - 21:52, 9 December 2017
• Codes
  ! Solver !! Mesh type(s) supported !! Last known version or year ! Generator !! Mesh type(s) supported !! Input filetypes supported
  25 KB (3,558 words) - 08:31, 23 January 2024
• Source code archive
  *[http://www.solvengineer.com/index.html '''SolveEngineer''' - Mihai Pruna's Website]
  1 KB (203 words) - 17:39, 14 June 2012
• Navier-Stokes equations
  ...heat conducting fluid. It is a vector equation obtained by applying Newton's Law of Motion to a fluid element and is also called the ''momentum equation The heat-flux, <math>q_j</math>, is given by Fourier's law:
  29 KB (4,606 words) - 18:17, 28 August 2012
• FAQ's
  :FAQ's about CFD-Wiki. [[Category: FAQ's]]
  1 KB (215 words) - 17:50, 12 December 2017
• Posdat.f
  | S | ...ing the commoned variable CX. If the z-coordinate is greater than the cell's coordinate, it is a "positive" z-beighbour else it could be negative. (ofco
  3 KB (540 words) - 12:13, 3 September 2011
• Reynolds stress model (RSM)
  consideration, a number of turbulent models, such as Rotta's model and Lumley's return-to-isotropy model, have been established.
  8 KB (1,203 words) - 01:47, 18 April 2017
• Near-wall treatment for k-omega models
  ''(For [...] wall functions, each wall-adjacent cell's centroid should be located within the log-law layer, 30 < y+ < 300. A y+ v
  4 KB (581 words) - 10:40, 31 March 2021
• Fluent FAQ
  === Using CFD-Online's Fluent Forum === * Scroll down to "I don't want a collector's account right now. Just give me the download-link." and click it.
  39 KB (6,386 words) - 16:48, 26 April 2013
• Best practice guidelines for turbomachinery CFD
  ...htly better but still do not behave well. More modern variants like Menter's [[SST k-omega model]] also has problems, wheras the [[V2-f models|v2f model ...ons with strong acceleration or deceleration. In the last few years Menter's low-Re <math>SST k-\omega</math> model has gained increased popularity.
  41 KB (6,252 words) - 08:46, 4 March 2023
• Baldwin-Lomax model
  * {{reference-paper|author=Baldwin, B. S. and Lomax, H.|year=1978|title=Thin Layer Approximation and Algebraic Model * {{reference-paper|author=Granville, P. S.|year=1987|title=Baldwin-Lomax Factors for Turbulent Boundary Layers in Pre
  8 KB (1,262 words) - 09:15, 3 January 2012
• Turbulence modeling
  #### [[Prandtl's one-equation model]] ##### [[Wilcox's k-omega model]]
  3 KB (282 words) - 19:16, 10 April 2021
• Introduction to turbulence/Nature of turbulence
  SONNET TO TURBULENCE by S. Corrsin <ref>Stan Corrsin was a famous and much beloved turbulence researc ...visor. </ref> on the occasion of his 70th birthday, with apologies to Bill S. and Liz B.B.
  16 KB (2,597 words) - 21:12, 9 November 2016
• Ansys FAQ
  ...ulation which has converged at a condition close to the problem simulation's condition.</LI> ...tion process, I get the warning message "A wall has been placed at portion(s) of an OUTLET" ====
  27 KB (4,461 words) - 02:03, 18 August 2018
• Numerical methods
  # [[Solution of Poisson's equation]] ### [[Moore's kd-tree algorithm]]
  4 KB (399 words) - 12:42, 26 August 2012
• Incompressible flow
  \frac{\partial u_i}{\partial t} = \pi^S (-u_j \frac{\partial u_i}{\partial x_j} + \nu \Delta u_i) , which result from the Helmholtz decomposition. <math>\pi^S</math> and <math>\pi^I</math> are the solenoidal (divergence-free) and irro
  8 KB (1,427 words) - 18:57, 19 August 2013
• Siemens FAQ
  ...-CCM+ lite version available with more limited functionality and CD-adapco's own 3D CAD tool ( 3D-CAD ) has been integrated into the STAR-CCM+ client. [[Category: FAQ's]]
  8 KB (1,278 words) - 21:48, 9 December 2017
• Large eddy simulation (LES)
  ...technique for simulating turbulent flows. An implication of [[Kolmogorov]]'s (1941) theory of self similarity is that the large eddies of the flow are d *{{reference-paper|author=Kim, W and Menon, S.|year=1995|title=A new dynamic one-equation subgrid-scale model for large e
  6 KB (882 words) - 21:50, 24 June 2013
• Spalart-Allmaras model
  ...\frac{\partial \tilde{\nu}}{\partial x_j} & = & C_{b1} [1 - f_{t2}] \tilde{S} \tilde{\nu} + \frac{1}{\sigma} \{ \nabla \cdot [(\nu + \tilde{\nu}) \nabla \tilde{S} \equiv S + \frac{ \tilde{\nu} }{ \kappa^2 d^2 } f_{v2}, \quad f_{v2} = 1 - \frac{\ch
  4 KB (662 words) - 13:34, 23 April 2015
• Finite volume
  |V_r| \frac{du_r}{dt} + \sum_{s \in N(r)} \int_{V_r \cap V_s} f_i n_i ds = 0
  4 KB (643 words) - 09:15, 3 January 2012
• Standard k-epsilon model
  :<math> P_k = \mu_t S^2 </math> Where <math> S </math> is the modulus of the mean rate-of-strain tensor, defined as : <br>
  3 KB (401 words) - 20:15, 16 December 2014
• Biconjugate gradient stabilized method
  : Allocate temperary vectors p, phat, s, shat, t, v, rtilde <br> :: s = r - alpha * v <br>
  2 KB (281 words) - 17:01, 31 October 2016
• Overset grids
  ...halmesh is freely available. Unfortuately, the other two are subject to U.S. goverment export controls, and are thus not generally available (see [http
  7 KB (1,042 words) - 14:13, 17 August 2021
• Realisable k-epsilon model
  ...lon}}\right) \frac{\partial \epsilon}{\partial x_j} \right ] + \rho \, C_1 S \epsilon - \rho \, C_2 \frac{{\epsilon}^2} {k + \sqrt{\nu \epsilon}} + C_{1 ...a}{\eta + 5}\right] , \;\;\;\;\; \eta = S \frac{k}{\epsilon}, \;\;\;\;\; S =\sqrt{2 S_{ij} S_{ij}} </math> <br>
  2 KB (380 words) - 19:57, 16 December 2014
• Approximation Schemes for convective term - structured grids - Summary of Discretizations Schemes and examples
  Below it's cleary seen the numerical diffusion impact, comparing the contour fields ob ''It's just a scrap. Later I'll correct it, although it's a complete working code''
  9 KB (1,327 words) - 05:56, 21 April 2012
• Approximation Schemes for convective term - structured grids - Common
  J_{h} - J_{l} & + J_{n} - J_{s} & + J_{e}- J_{w} & + \\ + D_{h} - D_{l} & + D_{n} - D_{s} & + D_{e} - D_{s} & = S_{p}
  28 KB (4,096 words) - 13:11, 24 October 2016
• Wall-adapting local eddy-viscosity (WALE) model
  ...lta _s^2 \frac{(S_{ij}^{d} S_{ij}^{d})^{3/2}}{(\overline{S}_{ij} \overline{S}_{ij})^{5/2} + (S_{ij}^{d} S_{ij}^{d})^{5/4}} </math>
  880 B (137 words) - 08:31, 19 May 2018
• Coeff 11.f90 - calculate the coefficients
  !------------------ s face-------------------- !------------------ s face--------------------
  5 KB (957 words) - 17:58, 20 April 2012
• Sample code for solving Smith-Hutton test - Fortran 90
  ''It's just a scrap. Later I'll correct it, although it's a complete working code''
  3 KB (378 words) - 18:02, 20 April 2012
• LU decomposition
  do s = 1, n-j i = j + s
  4 KB (696 words) - 09:22, 21 November 2011
• Tridiagonal matrix algorithm - TDMA (Thomas algorithm)
  ...red by Gaussian Elimination. A first sweep eliminates the <math>a_i</math>'s, and then an (abbreviated) backward substitution produces the solution. Ex #{{reference-book|author=Conte, S.D., and deBoor, C.|year=1972|title=Elementary Numerical Analysis|rest= McGr
  4 KB (658 words) - 22:58, 14 September 2016
• SIMPLE algorithm
  * {{reference-paper|author=Patankar, S. V. and Spalding, D.B.|year=1972|title=A calculation procedure for heat, ma * {{reference-paper|author=Patankar, S. V.|year=1980|title=Numerical Heat Transfer and Fluid Flow|rest=Taylor & Fr
  3 KB (442 words) - 10:42, 11 March 2016
• Approximation Schemes for convective term - structured grids - What we need: Please help
  {{reference-paper | author=B. P. Leonard and S. Mokhtari| year=1990 | title=Beyond first-order upwinding: the ULTRA-SHARP {{reference-paper | author=B. P. Leonard and S. Mokhtari. | year=1990 | title=ULTRA-SHARP nonoscillatory convection scheme
  5 KB (615 words) - 17:27, 7 November 2011
• Sand box Approximation Schemes
  == S.K. Godunov's theorem == ...]] important in the development of the theory of [[high resolution scheme]]s for the numerical solution of [[partial differential equations]].
  26 KB (3,687 words) - 20:19, 7 November 2011
• Aero-acoustics and noise
  ...ustic analogy are the Ffowcs Williams - Hawkins equation and the Kirchhoff's Equation. === Green's Function ===
  5 KB (709 words) - 15:59, 23 June 2013
• V2-f models
  ...x \left[ \min \left( \frac{k}{\varepsilon},\, \frac{0.6}{\sqrt{6} C_{\mu} |S|\zeta} \right), C_T \left( \frac{\nu}{\varepsilon} \right)^{1/2} \right]</ \frac{k^{1/2}}{\sqrt{6} C_{\mu} |S| \zeta} \right), C_{\eta}
  6 KB (917 words) - 05:45, 7 February 2014
• Johnson-King model
  ...for popular turbulence models transport equations are solved which are PDE's). This model solves for a transport equation for the maximum shear stress. *<b>Johnson, D.A. and King, L.S.</b> A mathematically simple turbulence closure model for attached and sepa
  735 B (103 words) - 05:48, 17 January 2012
• Ahmed body
  The Ahmed body was described originally by S. R. Ahmed in 1984 [1]. Three main features were seen in the wake: ...s-section of 1.87x1.4 m2 (width x height) with a bulk [[velocity]] of 40 m/s. The [[test-section]] of the [[wind-tunnel]] was 3/4 open (only ground plat
  4 KB (577 words) - 05:46, 6 October 2015
• General CFD FAQ
  [[Category: FAQ's]]
  7 KB (1,199 words) - 13:47, 5 June 2013
• CHAM FAQ
  ...quation solver for each finite-volume equation is a modified form of Stone's strongly implicit solver, but the option exists to use a Conjugate Gradient * FROMM: FROMM's scheme
  37 KB (5,717 words) - 12:46, 9 December 2019
• Finite element
  where the a's are unknown coefficients that are to be determined. For an initial value, i ...functions, one can generate as many equations as there are unknowns (the a's) thus yielding a albegraic system of equations.
  1 KB (226 words) - 12:09, 31 August 2011
• Hall of fame
  *W.C.S. Wigley *S. Osher
  2 KB (324 words) - 18:33, 27 June 2018
• CFD quotations
  * It's deja-screw all over again <br> --''Gary Montry'' * The world's an exciting place when you know CFD <br>--''John Shadid''
  1 KB (255 words) - 13:45, 28 June 2018
• Gridgen
  Gridgen's end-of-life went into effect in September 2016. #Coon's patch
  2 KB (258 words) - 13:19, 13 June 2018
• Turbulence intensity
  {{reference-paper|author=[1] ANSYS, Inc.|year=2022|title=ANSYS Fluent User's Guide, Release R1|rest=Equation (7.71)}}
  5 KB (661 words) - 16:24, 23 July 2022
• Wall shear stress
  ...is pascal (<math>Pa</math>), which is identical to <math>\frac{kg}{m\cdot s^2}</math>.
  433 B (78 words) - 10:21, 5 December 2012
• Skin friction coefficient
  ...that the flow is laminar for the first part of the plate and using Blasius's equeation, after providing corrective some corrective factors , Schlichting
  4 KB (516 words) - 12:14, 14 January 2016
• Law of the wall
  |<math>\kappa</math> || von Karman's constant (<math>\approx 0.41</math>)
  744 B (111 words) - 08:32, 7 September 2011
• Introduction to turbulence/Statistical analysis/Ensemble average
  ...l result, you probably noticed that the value of the <math> X_{10} </math>'s was also a random variable and differed from ensemble to ensemble. Also the
  8 KB (1,391 words) - 12:29, 2 July 2011
• Introduction to turbulence/Reynolds averaged equations
  ...in reality three separate equations. These three equations are just Newton's second law written for a continuum in a spatial(or Eulerian) reference fram :<math>\tilde{T}_{ij}^{(v)}= 2\mu[\tilde{s}_{ij}-\frac{1}{3}\tilde{s}_{kk}\delta_{ij}] </math>
  45 KB (7,578 words) - 08:35, 21 August 2013
• Flow around a circular cylinder
  [5] D'Alessio, S. J. D. and Dennis, S. C. R., 1994, A vorticity model for viscous flow past a cylinder, Comp. Flu [6] Dennis, S. C. R. and Chang, G.-Z., 1970, Numerical solutions for steady flow past a c
  6 KB (884 words) - 11:31, 8 April 2017
• Introduction to turbulence/Turbulence kinetic energy
  ...now. It’s a lot easier to teach if we just tell you one view, but that’s not very good preparation for the future. '''Example:''' Estimate the Kolmogorov microscale for <math>u = 1 m/s</math> and <math>L = 0.1 m</math> for air and water.
  47 KB (7,664 words) - 12:47, 13 December 2013
• Cavitation modeling
  * CRUNCH - Craft-tech's RANS solver * CAV2DBL - UT's two-dimensional panel method coupled with XFOIL boundary layer solver
  2 KB (250 words) - 05:28, 13 June 2013
• Discontinuous Galerkin
  While the discontinuous Galerkin method was developed in the early 1970's, it was not used for CFD simulations until the early 1990's when it was first used to
  9 KB (1,518 words) - 09:15, 3 January 2012
• K-omega models
  # [[Wilcox's k-omega model]] # [[Wilcox's modified k-omega model]]
  1 KB (148 words) - 12:43, 12 October 2011
• Structured mesh generation
  ...imes easier to add an intermediate parametric space, denoted by <math>\vec{s}</math>, in between the physical space representation of the grid and the c :<math>\vec{x}=\vec{x}\left(\vec{s}\left(\vec{\xi}\right)\right).</math>
  8 KB (1,204 words) - 03:53, 27 April 2012
• One equation turbulence models
  ...the turbulent kinetic energy. The original one-equation model is [[Prandtl's one-equation model]]. Other common one-equation models are:
  418 B (43 words) - 01:07, 8 April 2021
• PHOENICS
  ...quation solver for each finite-volume equation is a modified form of Stone's strongly implicit solver, but the option exists to use a Conjugate Gradient ...centration Heat and Momentum Limited in Wimbledon, London, UK as the world's first general-purpose CFD code. The name PHOENICS itself is an acronym for
  11 KB (1,641 words) - 11:18, 5 July 2013
• SSIIM
  ...s the convection-diffusion equation for sediment transport, using Van Rijn's formula for the bed boundary. Also, a water quality module is included. The ...t is necessary to use SSIIM 2. Otherwise, SSIIM 1 is recommended. The User's Manual gives more information about the versions.
  2 KB (340 words) - 06:27, 19 July 2016
• Tdyn
  *{{reference-book|author=E. Oñate, J. García and S. Idelsohn. |year=2004|title=Encyclopedia of Computational Mechanics (Ship H
  3 KB (388 words) - 09:14, 3 January 2012
• Stratford's separation criterion
  ...sess if a turbulent boundary layer is likely to separate or not. Stratford's criteria says that from the start of the pressure recovery where the max ve ... used <math>k = 0.5</math>, which is a bit less conservative than Statford's original values.
  3 KB (543 words) - 11:10, 11 December 2013
• Introduction to turbulence/Homogeneous turbulence
  .... Yet unbelievably we still don't have enough information to solve it. Let's try. Suppose we use the extanded ideas of Kolmogorov we introduced in Chapt ...lent Reynolds numbers. But before we feel too comfortable about this, let's look at another curve shown in figure 6.2. This one is also due to Sreeniva
  10 KB (1,751 words) - 13:03, 21 March 2012
• Introduction to turbulence/Free turbulent shear flows
  ...n natural and engineering environments. The jet of of air issuing from one's nostrils or mouth upon exhaling, the turbulent plume from a smoldering ciga It may seem strange to be talking about Prandtl’s boundary layer idea in a section about free shear flows, but as we shall se
  67 KB (11,204 words) - 13:42, 19 April 2016
• Sample code for solving Lid-Driven cavity test (Re=1000) - Fortran 90
  ''It's just a scrap. Later I'll correct it, although it's a complete working code -- Michail''
  3 KB (463 words) - 10:04, 20 May 2016
• Solve UV.f90 - Solution of the momentum equations for U and V
  !------------------ s face--------------------
  6 KB (932 words) - 14:58, 19 May 2016
• O-PALM
  ...ion of data assimilation methods: the PALM flow charting approach, Q.J.R.M.S., 127 (2001), 189-207), this approach was the most suitable for a research ...totype was implemented using the available technology at the end of the 90's. At the issue of this phase an MPI1 based version of the coupler was releas
  3 KB (418 words) - 21:45, 27 July 2011
• Turbulence dissipation rate
  ...<math>\mathrm{J} / (\mathrm{kg} \cdot \mathrm{s}) = \mathrm{m}^2 / \mathrm{s}^3</math>. <math>\tau_{ij} = 2 \mu S^*_{ij}</math>
  920 B (145 words) - 01:00, 11 April 2015
• Specific turbulence dissipation rate
  ...sed on dimensional analysis. The SI unit of <math>\omega</math> is <math>1/s</math>.
  1 KB (159 words) - 11:08, 13 June 2011
• Introduction to turbulence/Wall bounded turbulent flows
  to the inviscid Euler’s equations. ...lace. Professor Prandt literally saved fluid mechanics from d’Alembert’s paradox: the fact that there seemed to be no drag in an inviscid fluid (not
  41 KB (7,002 words) - 13:02, 21 March 2012
• Code: Lid driven cavity using pressure free velocity form
  ...}=\Pi^S(-\mathbf{v}\cdot\nabla\mathbf{v}+\nu\nabla^2\mathbf{v})+\mathbf{f}^S </math>, ... are solenoidal and irrotational projection operators satisfying <math>\Pi^S+\Pi^I=1</math> and
  11 KB (1,560 words) - 20:12, 15 March 2013
• Code: Lid-driven cavity using pressure-free velocity form (2)
  ...}=\Pi^S(-\mathbf{v}\cdot\nabla\mathbf{v}+\nu\nabla^2\mathbf{v})+\mathbf{f}^S </math>, ... are solenoidal and irrotational projection operators satisfying <math>\Pi^S+\Pi^I=1</math> and
  12 KB (1,673 words) - 20:07, 15 March 2013
• PFV4 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) - 19:12, 15 March 2013
• PFV4 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) - 19:29, 15 March 2013
• PFV convection matrix 2
  S=zeros(2,nd4); Sx=zeros(2,nd4); Sy=zeros(2,nd4); % Pre-allocate arrays S(:,mm+ND)=Jtd*ZS4424c{m,k}*Ti{m};
  7 KB (1,099 words) - 18:38, 4 July 2011
• PFV 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 (865 words) - 16:06, 15 March 2013
• PFV 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 (1,623 words) - 16:10, 15 March 2013
• PFV GMRES solver
  % Matlab's preconditioned gmres sparse solver. When Dirichlet
  5 KB (689 words) - 04:10, 29 June 2011
• PFV mesh regrade
  % if a<1 then grade towards the edge(s)
  1 KB (199 words) - 04:17, 29 June 2011
• PFV get pressure 2
  S=zeros(2,nd4); Sx=zeros(2,nd4); Sy=zeros(2,nd4); G=zeros(2,np4); S(:,mm+ND) =Jtd*ZS4424pc{m,k}*Ti{m};
  19 KB (3,020 words) - 18:42, 4 July 2011
• Code: Thermal cavity using pressure-free velocity form
  ...}=\Pi^S(-\mathbf{v}\cdot\nabla\mathbf{v}+\nu\nabla^2\mathbf{v})+\mathbf{f}^S </math>, ... are solenoidal and irrotational projection operators satisfying <math>\Pi^S+\Pi^I=1</math> and
  14 KB (1,998 words) - 21:21, 15 March 2013
• PFV Tconvection matrix 2
  TCm=zeros(nfT,nfT); S=zeros(2,nfV); g=zeros(1,nfT); G=zeros(2,nfT); S(:,mv+NDV)= Jtd*ZS4424tc{m,k}*Ti{m}; mv = mv+nV;
  7 KB (1,061 words) - 16:13, 7 July 2011
• PFV Buoyancy matrix 2
  Bm=zeros(nfV,nfT); S=zeros(2,nfV); g=zeros(1,nfT); % Preallocate arrays S(:,mv+NDV)=Jtd*ZS4424b{m,k}*Ti{m}; mv = mv + nV;
  6 KB (874 words) - 16:20, 7 July 2011
• Code: 3D Lid-driven cavity using pressure-free velocity form
  ...}=\Pi^S(-\mathbf{v}\cdot\nabla\mathbf{v}+\nu\nabla^2\mathbf{v})+\mathbf{f}^S </math>, ... are solenoidal and irrotational projection operators satisfying <math>\Pi^S+\Pi^I=1</math> and
  24 KB (3,584 words) - 14:08, 10 August 2011
• PFV 3D diffusion matrix
  function G=GTL(ni,q,r,s) ...*(1+ni(:,2).*r).*(1+ni(:,3).*s), .125*ni(:,2).*(1+ni(:,1).*q).*(1+ni(:,3).*s), ...
  5 KB (815 words) - 12:17, 20 July 2011
• PFV 3D convection matrix
  Cm=zeros(ndfe,ndfe); S=zeros(3,ndfe); % Preallocate arrays S(:,mm3)= JtbD*Z3_V8c{m,k}*Ti{m};
  5 KB (765 words) - 12:20, 20 July 2011
• PFV V8cW 3D linear FE
  function S=V8cW(ni,q,r,s) % V = V8cW(ni,q,r,s)
  2 KB (263 words) - 14:12, 10 August 2011
• PFV V8xyzcW 3D linear FE derivatives
  function [Vx,Vy,Vz]=V8xyzcW(ni,q,r,s) % [Vx,Vy,Vz]=V8xyzcW(ni,q,r,s)
  4 KB (820 words) - 12:12, 20 July 2011
• SIMPLEM algorithm - SIMPLE-Modified
  * {{reference-paper|author=Acharya, S. and Moukalled, F.|year=1989|title=Improvements to Incompressible Flow Calc
  303 B (38 words) - 21:32, 28 December 2011
• Pointwise
  Pointwise's mesh generation employs the following algorithms. ** Steger's formulation for hex extrusion
  3 KB (441 words) - 18:16, 28 August 2018
• What is Open Source?
  ...elines and information related to an Open Source license. From an engineer's standpoint: "Open-source software ... is computer software that is ... prov ...at this [http://www.linkedin.com/groups/What-are-your-experiences-in-66032.S.258407217?view=&gid=66032&item=ANET%3AS%3A258407217&trk=NUS_RITM-title inte
  28 KB (4,443 words) - 05:05, 23 December 2017
• 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