cl__1 = 1;
Point(1) = {0, 2.5, 0, cl__1};
Point(2) = {0.1, 1.96, 0, cl__1};
Point(3) = {0.2, 1.54, 0, cl__1};
Point(5) = {0.3, 1.24, 0, cl__1};
Point(6) = {0.4, 1.06, 0, cl__1};
Point(7) = {0.5, 1, 0, cl__1};
Point(8) = {0.6, 1.02, 0, cl__1};
Point(9) = {0.7, 1.08, 0, cl__1};
Point(10) = {0.8, 1.18, 0, cl__1};
Point(11) = {0.9, 1.32, 0, cl__1};
Point(12) = {1, 1.5, 0, cl__1};
Point(13) = {0, 0, 0, cl__1};
Point(14) = {1, 0, 0, cl__1};
Bezier(1) = {1, 2};
Transfinite Line {1} = 50 Using Progression 1;
Bezier(2) = {2, 3};
Transfinite Line {2} = 50 Using Progression 1;
Bezier(3) = {3, 5};
Transfinite Line {3} = 50 Using Progression 1;
Bezier(4) = {5, 6};
Transfinite Line {4} = 50 Using Progression 1;
Bezier(5) = {6, 7};
Transfinite Line {5} = 50 Using Progression 1;
Bezier(6) = {7, 8};
Transfinite Line {6} = 50 Using Progression 1;
Bezier(7) = {8, 9};
Transfinite Line {7} = 50 Using Progression 1;
Bezier(8) = {9, 10};
Transfinite Line {8} = 50 Using Progression 1;
Bezier(9) = {10, 11};
Transfinite Line {9} = 50 Using Progression 1;
Bezier(10) = {11, 12};
Transfinite Line {10} = 50 Using Progression 1;
Line(11) = {13, 14};
Line(12) = {13, 1};
Line(13) = {14, 12};
Curve Loop(1) = {1, 2, 3, 4, 5, 6, 7, 8, 9, 10, -13, -11, 12};
Plane Surface(1) = {1};
Physical Curve("axis") = {11};
Physical Curve("inlet") = {12};
Physical Curve("outlet") = {13};
Physical Curve("wall") = {1, 2, 3, 4, 5, 6, 7, 8, 9, 10};
Physical Surface("flowfield") = {1};