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};