Homec4science
Diffusion ConSol (master) Browse

ConSol/ConSol/Examples/HybridTest/ShockVortex/shockVortex2QUADsmall.geo
e1e61d7151eamaster

Last Change
Raw File

shockVortex2QUADsmall.geo
View Options

// Variables
boxdim = 1;
N = 2*8+1;
N0 = 2;
gridsize = boxdim/(N-1);
// Points
Point(1) = {0,0,0, gridsize};
Point(2) = {boxdim,0,0, gridsize*3};
Point(3) = {boxdim, boxdim,0, gridsize*3};
Point(4) = {0, boxdim,0, gridsize};
// first line
Point(5) = {boxdim/2,0,0, gridsize};
Point(6) = {boxdim/2, boxdim,0, gridsize};
Point(7) = {boxdim/2-N0*gridsize,0,0, gridsize};
Point(8) = {boxdim/2-N0*gridsize, boxdim,0, gridsize};
// second line
Point(9) = {boxdim*5/8,0,0, gridsize};
Point(10) = {boxdim*5/8,1,0, gridsize};
Point(11) = {boxdim*5/8+N0*gridsize,0,0, gridsize};
Point(12) = {boxdim*5/8+N0*gridsize, 1,0, gridsize};
Line(1) = {1,7};
Line(2) = {7,5};
Line(3) = {5,9};
Line(4) = {9,11};
Line(5) = {11,2};
Line(6) = {2,3};
Line(7) = {3,12};
Line(8) = {12,10};
Line(9) = {10,6};
Line(10) = {6,8};
Line(11) = {8,4};
Line(12) = {4,1};
Line(13) = {8,7};
Line(14) = {6,5};
Line(15) = {10,9};
Line(16) = {12,11};
Line Loop(1) = {1,-13,11,12};
Line Loop(2) = {2,-14,10,13};
Line Loop(3) = {3,-15,9,14};
Line Loop(4) = {4,-16,8,15};
Line Loop(5) = {5,6,7,16};
Plane Surface(1) = {1};
Plane Surface(2) = {2};
Plane Surface(3) = {3};
Plane Surface(4) = {4};
Plane Surface(5) = {5};
Physical Surface("tri_0") = {3};
Physical Surface("qdr_0") = {1};
Physical Surface("mid_0") = {2};
Physical Surface("qdr_1") = {5};
Physical Surface("mid_1") = {4};
Physical Line("inflow") = {12};
Physical Line("outflow") = {6};
Physical Line("slipWall") = {1,2,3,4,5,7,8,9,10,11};
Physical Line("q2i") = {13,16};
Physical Line("t2i") = {14,15};
Transfinite Curve{1,11} = (N-1)/2+1 - N0;
Transfinite Curve{5,7} = (N-1)/2+1 - N0 - (N-1)/8;
Transfinite Curve{2,10,4,8} = N0+1;
Transfinite Curve{12,13,14,15,16,6} = (N);
Transfinite Surface{1,2,4,5};
Recombine Surface{1,2,4,5};
c4science · Help