Pfv lid driven cavity
From CFD-Wiki
Matlab script LDCW.m for lid-driven cavity.
%LDCW LID-DRIVEN CAVITY % Finite element solution of the 2D Navier-Stokes equation using 4-node, 12 DOF, % (3-DOF/node), simple-cubic-derived rectangular Hermite basis for % the Lid-Driven Cavity problem. % % This could also be characterized as a VELOCITY-STREAM FUNCTION or % STREAM FUNCTION-VELOCITY method. % % Reference: "A Hermite finite element method for incompressible fluid flow", % Int. J. Numer. Meth. Fluids, 64, P376-408 (2010). % % Simplified Wiki version % The rectangular problem domain is defined between Cartesian % coordinates Xmin & Xmax and Ymin & Ymax. % The computational grid has NumEx elements in the x-direction % and NumEy elements in the y-direction. % The nodes and elements are numbered column-wise from the % upper left corner to the lower right corner. % %This script calls the user-defined functions: % regrade - to regrade the mesh % DMatW - to evaluate element diffusion matrix % CMatW - to evaluate element convection matrix % GetPresW - to evaluate the pressure % ilu_gmres_with_EBC - to solve the system with essential/Dirichlet BCs % % Jonas Holdeman August 2007, revised June 2011 clear all; disp('Lid-driven cavity'); disp(' Four-node, 12 DOF, simple-cubic stream function basis.'); % ------------------------------------------------------------- nd = 3; nd2=nd*nd; % Number of DOF per node - do not change!! % ------------------------------------------------------------- ETstart=clock; % Parameters for GMRES solver GMRES.Tolerance=1.e-14; GMRES.MaxIterates=20; GMRES.MaxRestarts=6; % Optimal relaxation parameters for given Reynolds number % (see IJNMF reference) % Re 100 1000 3200 5000 7500 10000 12500 % RelxFac: 1.04 1.11 .860 .830 .780 .778 .730 % ExpCR1 1.488 .524 .192 .0378 -- -- -- % ExpCRO 1.624 .596 .390 .331 .243 .163 .133 % CritFac: 1.82 1.49 1.14 1.027 .942 .877 .804 % Define the problem geometry, set mesh bounds: Xmin = 0.0; Xmax = 1.0; Ymin = 0.0; Ymax = 1.0; % Set mesh grading parameters (set to 1 if no grading). % See below for explanation of use of parameters. xgrd = .75; ygrd=.75; % (xgrd = 1, ygrd=1 for uniform mesh) % Set " RefineBoundary=1 " for additional refinement at boundary, % i.e., split first element along boundary into two. RefineBoundary=1; % DEFINE THE MESH % Set number of elements in each direction NumEx = 16; NumEy = NumEx; % PLEASE CHANGE OR SET NUMBER OF ELEMENTS TO CHANGE/SET NUMBER OF NODES! NumNx=NumEx+1; NumNy=NumEy+1; % Define problem parameters: % Lid velocity Vlid=1.; % Reynolds number Re=1000.; % factor for under/over-relaxation starting at iteration RelxStrt RelxFac = 1.; % % Number of nonlinear iterations MaxNLit=10; % %-------------------------------------------------------- % Viscosity for specified Reynolds number nu=Vlid*(Xmax-Xmin)/Re; % Grade the mesh spacing if desired, call regrade(x,agrd,e). % if e=0: refine both sides, 1: refine upper, 2: refine lower % if agrd=xgrd|ygrd is the parameter which controls grading, then % if agrd=1 then leave array unaltered. % if agrd<1 then refine (make finer) towards the ends % if agrd>1 then refine (make finer) towards the center. % % Generate equally-spaced nodal coordinates and refine if desired. if (RefineBoundary==1) XNc=linspace(Xmin,Xmax,NumNx-2); XNc=[XNc(1),(.62*XNc(1)+.38*XNc(2)),XNc(2:end-1),(.38*XNc(end-1)+.62*XNc(end)),XNc(end)]; YNc=linspace(Ymax,Ymin,NumNy-2); YNc=[YNc(1),(.62*YNc(1)+.38*YNc(2)),YNc(2:end-1),(.38*YNc(end-1)+.62*YNc(end)),YNc(end)]; else XNc=linspace(Xmin,Xmax,NumNx); YNc=linspace(Ymax,Ymin,NumNy); end if xgrd ~= 1 XNc=regrade(XNc,xgrd,0); end; % Refine mesh if desired if ygrd ~= 1 YNc=regrade(YNc,ygrd,0); end; [Xgrid,Ygrid]=meshgrid(XNc,YNc);% Generate the x- and y-coordinate meshes. % Allocate storage for fields psi0=zeros(NumNy,NumNx); u0=zeros(NumNy,NumNx); v0=zeros(NumNy,NumNx); %--------------------Begin grid plot----------------------- % ********************** FIGURE 1 ************************* % Plot the grid figure(1); clf; orient portrait; orient tall; subplot(2,2,1); hold on; plot([Xmax;Xmin],[YNc;YNc],'k'); plot([XNc;XNc],[Ymax;Ymin],'k'); hold off; axis([Xmin,Xmax,Ymin,Ymax]); axis equal; axis image; title([num2str(NumNx) 'x' num2str(NumNy) ... ' node mesh for Lid-driven cavity']); pause(.1); %-------------- End plotting Figure 1 ---------------------- %Contour levels, Ghia, Ghia & Shin, Re=100, 400, 1000, 3200, ... clGGS=[-.1175,-.1150,-.11,-.1,-.09,-.07,-.05,-.03,-.01,-1.e-4,-1.e-5,-1.e-7,-1.e-10,... 1.e-8,1.e-7,1.e-6,1.e-5,5.e-5,1.e-4,2.5e-4,5.e-4,1.e-3,1.5e-3,3.e-3]; CL=clGGS; % Select contour level option if (Vlid<0) CL=-CL; end NumNod=NumNx*NumNy; % total number of nodes MaxDof=nd*NumNod; % maximum number of degrees of freedom EBC.Mxdof=nd*NumNod; % maximum number of degrees of freedom nn2nft=zeros(2,NumNod); % node number -> nf & nt NodNdx=zeros(2,NumNod); % Generate lists of active nodal indices, freedom number & type ni=0; nf=-nd+1; nt=1; % ________ for nx=1:NumNx % | | for ny=1:NumNy % | | ni=ni+1; % |________| NodNdx(:,ni)=[nx;ny]; nf=nf+nd; % all nodes have 4 dofs nn2nft(:,ni)=[nf;nt]; % dof number & type (all nodes type 1) end; end; %NumNod=ni; % total number of nodes nf2nnt=zeros(2,MaxDof); % (node, type) associated with dof ndof=0; dd=[1:nd]; for n=1:NumNod for k=1:nd nf2nnt(:,ndof+k)=[n;k]; end ndof=ndof+nd; end NumEl=NumEx*NumEy; % Generate element connectivity, from upper left to lower right. Elcon=zeros(4,NumEl); ne=0; LY=NumNy; for nx=1:NumEx for ny=1:NumEy ne=ne+1; Elcon(1,ne)=1+ny+(nx-1)*LY; Elcon(2,ne)=1+ny+nx*LY; Elcon(3,ne)=1+(ny-1)+nx*LY; Elcon(4,ne)=1+(ny-1)+(nx-1)*LY; end % loop on ny end % loop on nx % Begin essential boundary conditions, allocate space MaxEBC = nd*2*(NumNx+NumNy-2); EBC.dof=zeros(MaxEBC,1); % Degree-of-freedom index EBC.typ=zeros(MaxEBC,1); % Dof type (1,2,3) EBC.val=zeros(MaxEBC,1); % Dof value X1=XNc(2); X2=XNc(NumNx-1); nc=0; for nf=1:MaxDof ni=nf2nnt(1,nf); nx=NodNdx(1,ni); ny=NodNdx(2,ni); x=XNc(nx); y=YNc(ny); if(x==Xmin | x==Xmax | y==Ymin) nt=nf2nnt(2,nf); switch nt; case {1, 2, 3} nc=nc+1; EBC.typ(nc)=nt; EBC.dof(nc)=nf; EBC.val(nc)=0; % psi, u, v end % switch (type) elseif (y==Ymax) nt=nf2nnt(2,nf); switch nt; case {1, 3} nc=nc+1; EBC.typ(nc)=nt; EBC.dof(nc)=nf; EBC.val(nc)=0; % psi, v case 2 nc=nc+1; EBC.typ(nc)=nt; EBC.dof(nc)=nf; EBC.val(nc)=Vlid; % u end % switch (type) end % if (boundary) end % for nf EBC.num=nc; if (size(EBC.typ,1)>nc) % Truncate arrays if necessary EBC.typ=EBC.typ(1:nc); EBC.dof=EBC.dof(1:nc); EBC.val=EBC.val(1:nc); end % End ESSENTIAL (Dirichlet) boundary conditions % partion out essential (Dirichlet) dofs p_vec = [1:EBC.Mxdof]'; % List of all dofs EBC.p_vec_undo = zeros(1,EBC.Mxdof); % form a list of non-diri dofs EBC.ndro = p_vec(~ismember(p_vec, EBC.dof)); % list of non-diri dofs % calculate p_vec_undo to restore Q to the original dof ordering EBC.p_vec_undo([EBC.ndro;EBC.dof]) = [1:EBC.Mxdof]; %p_vec'; Q=zeros(MaxDof,1); % Allocate space for solution (dof) vector % Initialize fields to boundary conditions for k=1:EBC.num Q(EBC.dof(k))=EBC.val(k); end; errpsi=zeros(NumNy,NumNx); % error correct for iteration MxNL=max(1,MaxNLit); np0=zeros(1,MxNL); % Arrays for convergence info nv0=zeros(1,MxNL); Qs=[]; Dmat = spalloc(MaxDof,MaxDof,36*MaxDof); % to save the diffusion matrix Vdof=zeros(nd,4); Xe=zeros(2,4); % coordinates of element corners NLitr=0; ND=1:nd; while (NLitr<MaxNLit), NLitr=NLitr+1; % <<< BEGIN NONLINEAR ITERATION tclock=clock; % Start assembly time <<<<<<<<< % Generate and assemble element matrices Mat=spalloc(MaxDof,MaxDof,36*MaxDof); RHS=spalloc(MaxDof,1,MaxDof); %RHS = zeros(MaxDof,1); Emat=zeros(1,16*nd2); % Values 144=4*4*(nd*nd) % BEGIN GLOBAL MATRIX ASSEMBLY for ne=1:NumEl for k=1:4 ki=NodNdx(:,Elcon(k,ne)); Xe(:,k)=[XNc(ki(1));YNc(ki(2))]; end if NLitr == 1 % Fluid element diffusion matrix, save on first iteration [DEmat,Rndx,Cndx] = DMatW(Xe,Elcon(:,ne),nn2nft); Dmat=Dmat+sparse(Rndx,Cndx,DEmat,MaxDof,MaxDof); % Global diffusion mat end if (NLitr>1) % Get stream function and velocities for n=1:4 Vdof(ND,n)=Q((nn2nft(1,Elcon(n,ne))-1)+ND); % Loop over local element nodes end % Fluid element convection matrix, first iteration uses Stokes equation. [Emat,Rndx,Cndx] = CMatW(Xe,Elcon(:,ne),nn2nft,Vdof); Mat=Mat+sparse(Rndx,Cndx,-Emat,MaxDof,MaxDof); % Global convection assembly end end; % loop ne over elements % END GLOBAL MATRIX ASSEMBLY Mat = Mat -nu*Dmat; % Add in cached/saved global diffusion matrix disp(['(' num2str(NLitr) ') Matrix assembly complete, elapsed time = '... num2str(etime(clock,tclock)) ' sec']); % Assembly time <<<<<<<<<<< pause(1); Q0 = Q; % Save dof values % Solve system tclock=clock; %disp('start solution'); % Start solution time <<<<<<<<<<<<<< RHSr=RHS(EBC.ndro)-Mat(EBC.ndro,EBC.dof)*EBC.val; Matr=Mat(EBC.ndro,EBC.ndro); Qs=Q(EBC.ndro); Qr=ilu_gmres_with_EBC(Matr,RHSr,[],GMRES,Qs); Q=[Qr;EBC.val]; % Augment active dofs with esential (Dirichlet) dofs Q=Q(EBC.p_vec_undo); % Restore natural order stime=etime(clock,tclock); % Solution time <<<<<<<<<<<<<< % ****** APPLY RELAXATION FACTOR ********************* if(NLitr>1) Q=RelxFac*Q+(1-RelxFac)*Q0; end % **************************************************** % Compute change and copy dofs to field arrays dsqp=0; dsqv=0; for k=1:MaxDof ni=nf2nnt(1,k); nx=NodNdx(1,ni); ny=NodNdx(2,ni); switch nf2nnt(2,k) % switch on dof type case 1 dsqp=dsqp+(Q(k)-Q0(k))^2; psi0(ny,nx)=Q(k); errpsi(ny,nx)=Q0(k)-Q(k); case 2 dsqv=dsqv+(Q(k)-Q0(k))^2; u0(ny,nx)=Q(k); case 3 dsqv=dsqv+(Q(k)-Q0(k))^2; v0(ny,nx)=Q(k); end % switch on dof type end % for np0(NLitr)=sqrt(dsqp); nv0(NLitr)=sqrt(dsqv); if (np0(NLitr)<=1e-15|nv0(NLitr)<=1e-15) MaxNLit=NLitr; np0=np0(1:MaxNLit); nv0=nv0(1:MaxNLit); end; disp(['(' num2str(NLitr) ') Solution time for linear system = '... num2str(etime(clock,tclock)) ' sec']); % Solution time <<<<<<<<<<<< %---------- Begin plot of intermediate results ---------- % ********************** FIGURE 2 ************************* figure(1); % Stream function (intermediate) subplot(2,2,3); contour(Xgrid,Ygrid,psi0,8,'k'); % Plot contours (trajectories) axis([Xmin,Xmax,Ymin,Ymax]); title(['Lid-driven cavity, Re=' num2str(Re)]); axis equal; axis image; % Plot convergence info subplot(2,2,2); semilogy(1:NLitr,nv0(1:NLitr),'k-+',1:NLitr,np0(1:NLitr),'k-o'); xlabel('Nonlinear iteration number'); ylabel('Nonlinear correction'); axis square; title(['Iteration conv., Re=' num2str(Re)]); legend('U','Psi'); % Plot nonlinear iteration correction contours subplot(2,2,4); contour(Xgrid,Ygrid,errpsi,8,'k'); % Plot contours (trajectories) axis([Xmin,Xmax,Ymin,Ymax]); axis equal; axis image; title(['Iteration correction']); pause(1); % ********************** END FIGURE 2 ************************* %---------- End plot of intermediate results --------- if (nv0(NLitr)<1e-15) break; end % Terminate iteration if non-significant end; % <<< (while) END NONLINEAR ITERATION format short g; disp('Convergence results by iteration: velocity, stream function'); disp(['nv0: ' num2str(nv0)]); disp(['np0: ' num2str(np0)]); % >>>>>>>>>>>>>> BEGIN PRESSURE RECOVERY <<<<<<<<<<<<<<<<<< % Essential pressure boundary condition % Index of node to apply pressure BC, value at node PBCnx=fix((NumNx+1)/2); % Apply at center of mesh PBCny=fix((NumNy+1)/2); PBCnod=0; for k=1:NumNod if (NodNdx(1,k)==PBCnx & NodNdx(2,k)==PBCny) PBCnod=k; break; end end if (PBCnod==0) error('Pressure BC node not found'); else EBCp.nodn = [PBCnod]; % Pressure BC node number EBCp.val = [0]; % set P = 0. end % Cubic pressure [P,Px,Py] = GetPresW(NumNod,NodNdx,Elcon,nn2nft,Xgrid,Ygrid,Q,EBCp,nu); % ******************** END PRESSURE RECOVERY ********************* % ********************** CONTINUE FIGURE 1 ************************* figure(1); % Stream function (final) subplot(2,2,3); [CT,hn]=contour(Xgrid,Ygrid,psi0,CL,'k'); % Plot contours (trajectories) clabel(CT,hn,CL([1,3,5,7,9,10,11,19,23])); hold on; plot([Xmin,Xmin,Xmax,Xmax,Xmin],[Ymax,Ymin,Ymin,Ymax,Ymax],'k'); hold off; axis([Xmin,Xmax,Ymin,Ymax]); axis equal; axis image; title(['Stream lines, ' num2str(NumNx) 'x' num2str(NumNy) ... ' mesh, Re=' num2str(Re)]); % Plot pressure contours (final) subplot(2,2,4); CPL=[-.002,0,.02,.05,.07,.09,.11,.12,.17,.3]; [CT,hn]=contour(Xgrid,Ygrid,P,CPL,'k'); % Plot pressure contours clabel(CT,hn,CPL([3,5,7,10])); hold on; plot([Xmin,Xmin,Xmax,Xmax,Xmin],[Ymax,Ymin,Ymin,Ymax,Ymax],'k'); hold off; axis([Xmin,Xmax,Ymin,Ymax]); axis equal; axis image; title(['Simple cubic pressure contours, Re=' num2str(Re)]); % ********************* END FIGURE 1 ************************* disp(['Total elapsed time = '... num2str(etime(clock,ETstart)/60) ' min']); % Elapsed time from start <<<