Simulating Laminar flow through a pipe using Hagen Poiseuille equation and comparing the results
clear all
close all
clc
f1 = fopen(\'blockMeshDict\',\'w\');
theta = 2.5; % half of required angle of wedge
d = 0.125; % diameter of cylinder in meters
vx_1 = sind(theta);
vx_2 = cosd(theta);
fprintf(f1,\'convertToMeters 1 \\n\\n\');
fprintf(f1,\'vertices\\n\');
fprintf(f1,\'(\\n\');
fprintf(f1,\' (0 0 0)\\n\');
fprintf(f1,\' (%f %f %f)\\n\',0,d*vx_2,-d*vx_1);
fprintf(f1,\' (%f %f %f)\\n\',0,d*vx_2,d*vx_1);
fprintf(f1,\' (30 0 0)\\n\');
fprintf(f1,\' (%f %f %f)\\n\',30,d*vx_2,-d*vx_1);
fprintf(f1,\' (%f %f %f)\\n\',30,d*vx_2,d*vx_1);
fprintf(f1,\');\\n\\n\');
fprintf(f1,\'blocks\\n\');
fprintf(f1,\'(\\n\');
fprintf(f1,\' hex (0 1 2 0 3 4 5 3) (50 1 500) simpleGrading (1 1 1)\\n\');
fprintf(f1,\');\\n\\n\');
fprintf(f1,\'edges\\n\');
fprintf(f1,\'(\\n\');
fprintf(f1,\' arc 1 2 (0 %f 0)\\n\',d);
fprintf(f1,\' arc 4 5 (30 %f 0)\\n\',d);
fprintf(f1,\');\\n\\n\');
fprintf(f1,\'boundary\\n\');
fprintf(f1,\'(\\n\');
fprintf(f1,\' axis\\n\');
fprintf(f1,\' {\\n\');
fprintf(f1,\' type empty\\n\');
fprintf(f1,\' faces ((0 3 3 0));\\n\');
fprintf(f1,\' }\\n\\n\');
fprintf(f1,\' inlet\\n\');
fprintf(f1,\' {\\n\');
fprintf(f1,\' type patch\\n\');
fprintf(f1,\' faces ((0 0 2 1));\\n\');
fprintf(f1,\' }\\n\\n\');
fprintf(f1,\' outlet\\n\');
fprintf(f1,\' {\\n\');
fprintf(f1,\' type patch\\n\');
fprintf(f1,\' faces ((3 4 5 3));\\n\');
fprintf(f1,\' }\\n\\n\');
fprintf(f1,\' Wall\\n\');
fprintf(f1,\' {\\n\');
fprintf(f1,\' type wall\\n\');
fprintf(f1,\' faces ((2 5 4 1));\\n\');
fprintf(f1,\' }\\n\\n\');
fprintf(f1,\' front\\n\');
fprintf(f1,\' {\\n\');
fprintf(f1,\' type wedge\\n\');
fprintf(f1,\' faces ((0 3 5 2));\\n\');
fprintf(f1,\' }\\n\\n\');
fprintf(f1,\' back\\n\');
fprintf(f1,\' {\\n\');
fprintf(f1,\' type wedge\\n\');
fprintf(f1,\' faces ((1 4 3 0));\\n\');
fprintf(f1,\' }\\n\\n\');
fprintf(f1,\');\\n\\n\');
fprintf(f1,\'mergePatchPairs\\n\');
fprintf(f1,\'(\\n\');
fprintf(f1,\');\\n\');
fclose(f1);
Velocity profiles at different points:
As the velocity near the center of the pipe is approximately twice of the starting velocity (i.e 8.4e-03), we can say that the velocity profile is fully developed, and the solution is converged.
Comparison of Velocity profiles from Hagen-Poiseullie Equation and from Icofoam solution:
Shear stress variation along the radial axis at the end of the pipe: