Jorge Gonzalez
05f5adcfe1
Bugs fixed: - Solved an issue with particles being injected with infinite velocity resulting in Inf velocity in some cells of the output files. - Particles are now equally distributed in cylindrical geometry along the radial direction. New features: - Particles now have their own weight that is recalculated when the particle moves to a new cell. This avoid the reduction of density at r = 0. Cases: - Added a case of Argon flow around a cylinder to measure performance and future improvements.
79 lines
2.1 KiB
GLSL
79 lines
2.1 KiB
GLSL
cl__1 = 1;
|
|
cyl_h = 0.005;
|
|
cyl_l = 0.02;
|
|
cyl_s = 0.03;
|
|
cyl_e = cyl_s + cyl_l;
|
|
dom_h = 0.03;
|
|
dom_l = 0.07;
|
|
|
|
Lcell = 0.001;
|
|
|
|
Point(1) = {0, 0, 0, cl__1};
|
|
Point(2) = {cyl_s, 0, 0, cl__1};
|
|
Point(3) = {cyl_s, cyl_h, 0, cl__1};
|
|
Point(4) = {cyl_e, cyl_h, 0, cl__1};
|
|
Point(5) = {cyl_e, 0, 0, cl__1};
|
|
Point(6) = {dom_l, 0, 0, cl__1};
|
|
Point(7) = {dom_l, cyl_h, 0, cl__1};
|
|
Point(8) = {dom_l, dom_h, 0, cl__1};
|
|
Point(9) = {cyl_e, dom_h, 0, cl__1};
|
|
Point(10) = {cyl_s, dom_h, 0, cl__1};
|
|
Point(11) = {0, dom_h, 0, cl__1};
|
|
Point(12) = {0, cyl_h, 0, cl__1};
|
|
|
|
Line(1) = {1, 2};
|
|
Line(2) = {2, 3};
|
|
Line(3) = {3, 4};
|
|
Line(4) = {4, 5};
|
|
Line(5) = {5, 6};
|
|
Line(6) = {6, 7};
|
|
Line(7) = {7, 8};
|
|
Line(8) = {8, 9};
|
|
Line(9) = {9, 10};
|
|
Line(10) = {10, 11};
|
|
Line(11) = {11, 12};
|
|
Line(12) = {12, 1};
|
|
Line(13) = {12, 3};
|
|
Line(14) = {4, 7};
|
|
Line(15) = {4, 9};
|
|
Line(16) = {10, 3};
|
|
|
|
Line Loop(1) = {1, 2, -13, 12};
|
|
Plane Surface(1) = {1};
|
|
Line Loop(2) = {13, -16, 10, 11};
|
|
Plane Surface(2) = {2};
|
|
Line Loop(3) = {3, 15, 9, 16};
|
|
Plane Surface(3) = {3};
|
|
Line Loop(4) = {5, 6, -14, 4};
|
|
Plane Surface(4) = {4};
|
|
Line Loop(5) = {14, 7, 8, -15};
|
|
Plane Surface(5) = {5};
|
|
|
|
Physical Line(1) = {12, 11};
|
|
Physical Line(2) = {10, 9, 8};
|
|
Physical Line(3) = {7, 6};
|
|
Physical Line(4) = {2, 3, 4};
|
|
Physical Line(5) = {1, 5};
|
|
|
|
Physical Surface(1) = {1};
|
|
Physical Surface(2) = {2};
|
|
Physical Surface(3) = {3};
|
|
Physical Surface(4) = {4};
|
|
Physical Surface(5) = {5};
|
|
|
|
Transfinite Line {12, 2, 4, 6} = cyl_h/Lcell + 1 Using Progression 1;
|
|
Transfinite Line {1, 13, 10} = cyl_s/Lcell + 1 Using Progression 1;
|
|
Transfinite Line {11, 16, 15, 7} = (dom_h - cyl_h)/Lcell + 1 Using Progression 1;
|
|
Transfinite Line {3, 9} = cyl_l/Lcell + 1 Using Progression 1;
|
|
Transfinite Line {5, 14, 8} = (dom_l - cyl_e)/Lcell + 1 Using Progression 1;
|
|
|
|
Transfinite Surface{1};
|
|
Recombine Surface {1};
|
|
Transfinite Surface{2};
|
|
Recombine Surface {2};
|
|
Transfinite Surface{3};
|
|
Recombine Surface {3};
|
|
Transfinite Surface{4};
|
|
Recombine Surface {4};
|
|
Transfinite Surface{5};
|
|
Recombine Surface {5};
|