Drawing streamlines for lid-driven cavity flow

2 views (last 30 days)
Hello, I want to know how I can plot streamlines when i know u and v components of velocity. Any help will be appreciated. The figure should be like this: http://dsec.pku.edu.cn/~tanghz/Lid-drivencavityflow.htm My code is for lid-driven cavity as follows:
if true
%%%%%%%%%%%%%%%
% Script file: LidDrivenCavity.m
%
% Lattice structure:
% c4 c3 c2
% \ | /
% c5 -c9 - c1
% / | \
% c6 c7 c8
%
tic; hold on; clc; clear; nx=100; ny=100; tstep=400; alpha=0.01; omega=1.0; u_ini=0.1; v_ini=0; Re=u_ini*nx/alpha w1=4/9; w2=1/9; w3=1/36; f=ones(nx,ny,9); f_eq=f; density=2.7;
for ii=1:tstep
% Propegate (This part of code [propegate] is always constant for all LBM
% problems.)
f(:,:,4)=f([2:nx 1],[ny 1:ny-1],4); f(:,:,3)=f(:,[ny 1:ny-1],3);
f(:,:,2)=f([nx 1:nx-1],[ny 1:ny-1],2); f(:,:,5)=f([2:nx 1],:,5);
f(:,:,1)=f([nx 1:nx-1],:,1); f(:,:,6)=f([2:nx 1],[2:ny 1],6);
f(:,:,7)=f(:,[2:ny 1],7); f(:,:,8)=f([nx 1:nx-1],[2:ny 1],8);
% Boundary Conditions
%At i=1, Bounceback
f(1,:,1)=f(1,:,5); f(1,:,2)=f(1,:,6); f(1,:,8)=f(1,:,4);
%At i=nx, Bounceback
f(nx,:,4)=f(nx,:,8); f(nx,:,5)=f(nx,:,1); f(nx,:,6)=f(nx,:,2);
%At j=1, Bounceback
f(:,1,2)=f(:,1,6); f(:,1,3)=f(:,1,7); f(:,1,4)=f(:,1,8);
%At j=ny, Know Velocity
densityN=f(:,ny,9)+f(:,ny,1)+f(:,ny,5)+2*(f(:,ny,3)+f(:,ny,4)+f(:,ny,2));
f(:,ny,7)=f(:,ny,3);
f(:,ny,6)=f(:,ny,2)+0.5*(f(:,ny,1)-f(:,ny,5))-u_ini.*densityN/2;
f(:,ny,8)=f(:,ny,4)+0.5*(f(:,ny,5)-f(:,ny,1))+u_ini.*densityN/2;
density=sum(f,3);
u=(sum(f(:,:,[1 2 8]),3)-sum(f(:,:,[4 5 6]),3))./density;
v=(sum(f(:,:,[2 3 4]),3)-sum(f(:,:,[6 7 8]),3))./density;
f_eq(:,:,1)=w2*density.*(1+3*u+9/2*u.^2-3/2*(u.^2+v.^2));
f_eq(:,:,3)=w2*density.*(1+3*v+9/2*v.^2-3/2*(u.^2+v.^2));
f_eq(:,:,5)=w2*density.*(1-3*u+9/2*u.^2-3/2*(u.^2+v.^2));
f_eq(:,:,7)=w2*density.*(1-3*v+9/2*v.^2-3/2*(u.^2+v.^2));
f_eq(:,:,2)=w3*density.*(1+3*(u+v)+9/2*(u+v).^2-3/2*(u.^2+v.^2));
f_eq(:,:,4)=w3*density.*(1+3*(-u+v)+9/2*(-u+v).^2-3/2*(u.^2+v.^2));
f_eq(:,:,6)=w3*density.*(1-3*(u+v)+9/2*(u+v).^2-3/2*(u.^2+v.^2));
f_eq(:,:,8)=w3*density.*(1+3*(u-v)+9/2*(u-v).^2-3/2*(u.^2+v.^2));
f_eq(:,:,9)=w1*density.*(1-3/2*(u.^2+v.^2));
f=omega*f_eq+(1-omega)*f;
end
u_final=sqrt(u.^2+v.^2); toc; end

Answers (0)

Categories

Find more on Fluid Dynamics in Help Center and File Exchange

Community Treasure Hunt

Find the treasures in MATLAB Central and discover how the community can help you!

Start Hunting!