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Point(1001) = {0.180594157118+0.001,-0.01722604,0,0.001799970964};
Point(1239) = {0.172158652+0.001,-0.037026971,0,0.001799970964};
Spline(1) = {121,122,123,124,125,126,127,128,129,130,131,132,133,134,135,136,137,138,139,140,141,142,143,144,145,146,147,148,149,150,151,152,153,154,155,156,157,158,159,160,161,162,163,164,165,166,167,168,169,170,171,172,173,174,175,176,177,178,179,180,181,182,183,184,185,186,187,188,189,190,191,192,193,194,195,196,197,198,199,200,201,202,203,204,205,206,207,208,209,210,211,212,213,214,215,216,217,218,219,220,221,222,223,224,225,226,227,228,229,230,231,232,233,234,235,236,237,238,239,240,241}; //
Spline(2) = {1,2,3,4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19,20,21,22,23,24,25,26,27,28,29,30,31,32,33,34,35,36,37,38,39,40,41,42,43,44,45,46,47,48,49,50,51,52,53,54,55,56,57,58,59,60,61,62,63,64,65,66,67,68,69,70,71,72,73,74,75,76,77,78,79,80,81,82,83,84,85,86,87,88,89,90,91,92,93,94,95,96,97,98,99,100,101,102,103,104,105,106,107,108,109,110,111,112,113,114,115,116,117,118,119,120,121}; ////
Line(3) = {241, 1};
Line Loop(1000) = {3,2,1};

// flow field boundaries
Point(242) = {1.08,-3.6+3.4200,0,0.01};
Point(243) = {-0.9+4*0.18,-3.6+3.4200,0,0.02};
Point(244) = {-0.9+4*0.18,3.6-3.4200,0,0.02};
Point(245) = {1.08,3.6-3.4200,0,0.01};
Line(12) = {242,243};
Line(13) = {243,244};
Line(14) = {244,245};
Line(15) = {245,242};
Line Loop(1001) = {-15,-14,-13,-12};
Plane Surface(1002) = {1001,1000};

// line for wake refinement
coordChordTop[] = Point{1};
coordChordBottom[] = Point{241};
Point(251) = {(coordChordBottom[0]+coordChordTop[0])/2,(coordChordBottom[1]+coordChordTop[1])/2,0,0.1799970964};
Point(252) = {1.079985482,(coordChordBottom[1]+coordChordTop[1])/2,0,0.1799970964};
Line(17) = {251,252};

//Define Boundary Layer
Field[6] = BoundaryLayer;
Field[6].EdgesList = {1,2}; //,3, 1009
Field[6].NodesList = {2,240};
Field[6].FanNodesList = {1,241};
Field[6].hfar = 1e-3;
Field[6].hwall_n = 0.1e-4;
Field[6].thickness = 0.005;
Field[6].ratio = 1.05;
Field[6].AnisoMax = 0.1;
Field[6].Quads = 1;
Field[6].IntersectMetrics = 0;
BoundaryLayer Field = 6;

//Recombine Surface{1,2} = 0;
j1[] = Extrude {0,0,-0.0018} {Surface{1002};Layers{1};Recombine;};
Physical Surface("inlet") = {j1[4]};
Physical Surface("outlet") = {j1[2]};
Physical Surface("topAndBottom") = {j1[3], j1[5]};
Physical Surface("airfoil") = {j1[6],j1[7],1038};
Physical Surface("frontAndBack") = {j1[0],1002};
Physical Volume("Volumen") = {j1[1]};

