Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-lwk80100-il-1000000 Airfoil,lwk80100-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,60.4825 Max Cl/Cd alpha,7.5 Url,http://airfoiltools.com/polar/csv?polar=xf-lwk80100-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.750,-0.9745,0.06924,0.06738,-0.0168,1.0000,0.0060 -13.500,-0.9899,0.06141,0.05942,-0.0230,1.0000,0.0060 -13.250,-1.0389,0.05044,0.04813,-0.0290,1.0000,0.0059 -13.000,-1.0376,0.04790,0.04551,-0.0298,1.0000,0.0059 -12.750,-1.0779,0.04075,0.03800,-0.0299,1.0000,0.0058 -12.500,-1.0628,0.04024,0.03747,-0.0297,1.0000,0.0062 -12.250,-1.0802,0.03634,0.03331,-0.0280,1.0000,0.0062 -12.000,-1.0849,0.03393,0.03070,-0.0260,1.0000,0.0063 -11.750,-1.0869,0.03184,0.02842,-0.0235,1.0000,0.0064 -11.500,-1.0820,0.03042,0.02686,-0.0212,1.0000,0.0065 -11.250,-1.0699,0.02940,0.02572,-0.0196,1.0000,0.0068 -11.000,-1.0600,0.02781,0.02396,-0.0178,1.0000,0.0069 -10.750,-1.0505,0.02596,0.02190,-0.0159,1.0000,0.0070 -10.500,-1.0284,0.02588,0.02176,-0.0153,1.0000,0.0072 -10.250,-1.0281,0.02222,0.01769,-0.0122,1.0000,0.0075 -10.000,-1.0126,0.02083,0.01614,-0.0107,1.0000,0.0075 -9.750,-0.9990,0.01911,0.01424,-0.0089,1.0000,0.0078 -9.500,-0.9807,0.01814,0.01316,-0.0077,1.0000,0.0081 -9.250,-0.9614,0.01729,0.01223,-0.0066,1.0000,0.0083 -9.000,-0.9406,0.01665,0.01154,-0.0057,1.0000,0.0088 -8.750,-0.9254,0.01608,0.01092,-0.0034,0.9943,0.0092 -8.500,-0.8885,0.01518,0.00992,-0.0061,0.9748,0.0097 -8.250,-0.8471,0.01452,0.00917,-0.0096,0.9644,0.0102 -8.000,-0.8036,0.01396,0.00853,-0.0136,0.9564,0.0107 -7.750,-0.7648,0.01254,0.00693,-0.0169,0.9441,0.0120 -7.500,-0.7268,0.01203,0.00635,-0.0196,0.9318,0.0131 -7.250,-0.6955,0.01161,0.00585,-0.0208,0.9192,0.0142 -7.000,-0.6676,0.01137,0.00554,-0.0210,0.9087,0.0156 -6.750,-0.6447,0.01083,0.00492,-0.0203,0.8991,0.0197 -6.500,-0.6200,0.01064,0.00469,-0.0198,0.8917,0.0216 -6.250,-0.5970,0.01026,0.00428,-0.0190,0.8853,0.0264 -6.000,-0.5726,0.01006,0.00406,-0.0185,0.8797,0.0297 -5.750,-0.5487,0.00979,0.00376,-0.0177,0.8742,0.0341 -5.500,-0.5244,0.00956,0.00351,-0.0172,0.8693,0.0394 -5.250,-0.5001,0.00935,0.00329,-0.0165,0.8647,0.0446 -5.000,-0.4758,0.00914,0.00309,-0.0159,0.8604,0.0529 -4.750,-0.4514,0.00891,0.00289,-0.0154,0.8564,0.0650 -4.500,-0.4273,0.00867,0.00270,-0.0147,0.8525,0.0791 -4.250,-0.4038,0.00839,0.00250,-0.0140,0.8484,0.1016 -4.000,-0.3802,0.00811,0.00232,-0.0132,0.8447,0.1316 -3.750,-0.3572,0.00779,0.00215,-0.0124,0.8412,0.1758 -3.500,-0.3367,0.00730,0.00195,-0.0112,0.8376,0.2485 -3.250,-0.3165,0.00681,0.00176,-0.0099,0.8338,0.3300 -3.000,-0.2979,0.00624,0.00156,-0.0082,0.8303,0.4350 -2.750,-0.2816,0.00561,0.00138,-0.0061,0.8267,0.5598 -2.500,-0.2617,0.00528,0.00132,-0.0044,0.8234,0.6407 -2.250,-0.2377,0.00516,0.00132,-0.0035,0.8201,0.6814 -2.000,-0.2118,0.00512,0.00130,-0.0031,0.8170,0.7007 -1.750,-0.1853,0.00512,0.00129,-0.0027,0.8142,0.7161 -1.500,-0.1587,0.00512,0.00130,-0.0024,0.8112,0.7294 -1.250,-0.1320,0.00512,0.00129,-0.0021,0.8078,0.7393 -1.000,-0.1052,0.00510,0.00130,-0.0018,0.8043,0.7477 -0.750,-0.0789,0.00512,0.00131,-0.0013,0.8003,0.7592 -0.500,-0.0525,0.00515,0.00132,-0.0009,0.7952,0.7679 -0.250,-0.0264,0.00512,0.00132,-0.0004,0.7887,0.7756 0.000,-0.0001,0.00516,0.00132,0.0000,0.7823,0.7829 0.250,0.0263,0.00512,0.00132,0.0005,0.7750,0.7889 0.500,0.0527,0.00515,0.00132,0.0009,0.7682,0.7949 0.750,0.0789,0.00512,0.00130,0.0014,0.7588,0.8000 1.000,0.1052,0.00510,0.00129,0.0018,0.7474,0.8043 1.250,0.1320,0.00512,0.00129,0.0021,0.7390,0.8078 1.500,0.1588,0.00512,0.00130,0.0024,0.7292,0.8112 1.750,0.1851,0.00512,0.00128,0.0028,0.7142,0.8142 2.000,0.2117,0.00513,0.00129,0.0031,0.6999,0.8171 2.250,0.2378,0.00516,0.00131,0.0035,0.6821,0.8201 2.500,0.2628,0.00524,0.00133,0.0042,0.6515,0.8234 2.750,0.2818,0.00561,0.00138,0.0061,0.5604,0.8267 3.000,0.2972,0.00629,0.00157,0.0084,0.4252,0.8303 3.250,0.3164,0.00682,0.00176,0.0099,0.3290,0.8338 3.500,0.3365,0.00732,0.00196,0.0112,0.2449,0.8375 3.750,0.3573,0.00779,0.00215,0.0125,0.1758,0.8412 4.000,0.3802,0.00811,0.00232,0.0132,0.1313,0.8447 4.250,0.4039,0.00839,0.00250,0.0140,0.1025,0.8484 4.500,0.4275,0.00866,0.00270,0.0147,0.0811,0.8525 4.750,0.4515,0.00890,0.00288,0.0154,0.0654,0.8564 5.000,0.4759,0.00912,0.00308,0.0159,0.0534,0.8604 5.250,0.5006,0.00931,0.00326,0.0165,0.0464,0.8647 5.500,0.5246,0.00955,0.00350,0.0172,0.0397,0.8694 5.750,0.5488,0.00979,0.00374,0.0177,0.0334,0.8742 6.000,0.5730,0.01002,0.00402,0.0184,0.0295,0.8796 6.250,0.5971,0.01025,0.00424,0.0190,0.0256,0.8853 6.500,0.6209,0.01056,0.00460,0.0197,0.0209,0.8915 7.000,0.6683,0.01130,0.00545,0.0209,0.0148,0.9085 7.250,0.6955,0.01161,0.00584,0.0208,0.0139,0.9192 7.500,0.7270,0.01202,0.00632,0.0196,0.0124,0.9319 7.750,0.7638,0.01283,0.00723,0.0170,0.0112,0.9449 8.000,0.8035,0.01405,0.00863,0.0136,0.0105,0.9566 8.250,0.8464,0.01474,0.00943,0.0097,0.0101,0.9647 8.500,0.8877,0.01542,0.01019,0.0062,0.0093,0.9754 8.750,0.9249,0.01626,0.01112,0.0035,0.0089,0.9953 9.000,0.9399,0.01676,0.01164,0.0058,0.0085,1.0000 9.250,0.9596,0.01756,0.01252,0.0069,0.0083,1.0000 9.500,0.9785,0.01847,0.01351,0.0081,0.0080,1.0000 9.750,0.9964,0.01954,0.01471,0.0094,0.0078,1.0000 10.000,1.0107,0.02114,0.01648,0.0110,0.0075,1.0000 10.250,1.0201,0.02354,0.01915,0.0132,0.0074,1.0000 10.500,1.0275,0.02606,0.02196,0.0155,0.0073,1.0000 10.750,1.0347,0.02830,0.02446,0.0176,0.0071,1.0000 11.000,1.0545,0.02857,0.02479,0.0184,0.0070,1.0000 11.250,1.0594,0.03077,0.02722,0.0206,0.0069,1.0000 11.500,1.0573,0.03303,0.02971,0.0237,0.0068,1.0000 11.750,1.0638,0.03421,0.03101,0.0256,0.0067,1.0000 12.000,1.0759,0.03486,0.03172,0.0267,0.0064,1.0000 12.250,1.0748,0.03692,0.03393,0.0283,0.0062,1.0000 12.500,1.0522,0.04144,0.03874,0.0299,0.0064,1.0000 12.750,1.0487,0.04413,0.04156,0.0302,0.0060,1.0000 13.000,1.0322,0.04868,0.04632,0.0295,0.0060,1.0000 13.250,1.0058,0.05532,0.05318,0.0268,0.0059,1.0000 13.750,0.9615,0.07279,0.07100,0.0138,0.0062,1.0000