Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rae102-il-50000-n5 Airfoil,rae102-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,27.392 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-rae102-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.7472,0.07692,0.06954,-0.0272,1.0000,0.0445 -10.000,-0.7632,0.07278,0.06530,-0.0276,1.0000,0.0443 -9.750,-0.7788,0.06905,0.06142,-0.0267,1.0000,0.0443 -9.500,-0.7904,0.06511,0.05725,-0.0258,1.0000,0.0443 -9.250,-0.7972,0.06125,0.05311,-0.0246,1.0000,0.0443 -9.000,-0.8007,0.05742,0.04893,-0.0232,1.0000,0.0445 -8.750,-0.7993,0.05360,0.04480,-0.0217,1.0000,0.0448 -8.500,-0.7928,0.05000,0.04093,-0.0205,1.0000,0.0455 -8.250,-0.7829,0.04693,0.03761,-0.0192,1.0000,0.0467 -8.000,-0.7702,0.04447,0.03488,-0.0181,1.0000,0.0491 -7.750,-0.7565,0.04188,0.03192,-0.0167,1.0000,0.0520 -7.500,-0.7400,0.03908,0.02861,-0.0152,1.0000,0.0546 -7.250,-0.7194,0.03648,0.02547,-0.0140,1.0000,0.0565 -7.000,-0.6980,0.03422,0.02326,-0.0133,1.0000,0.0602 -6.750,-0.6760,0.03251,0.02132,-0.0123,1.0000,0.0665 -6.500,-0.6517,0.03063,0.01930,-0.0114,1.0000,0.0717 -6.250,-0.6296,0.02914,0.01768,-0.0103,1.0000,0.0792 -6.000,-0.6096,0.02773,0.01626,-0.0090,1.0000,0.0895 -5.750,-0.5908,0.02634,0.01482,-0.0074,1.0000,0.1006 -5.500,-0.5737,0.02502,0.01354,-0.0058,1.0000,0.1196 -5.250,-0.5583,0.02355,0.01223,-0.0041,1.0000,0.1467 -5.000,-0.5453,0.02184,0.01095,-0.0023,1.0000,0.2057 -4.750,-0.5369,0.01995,0.01007,0.0003,1.0000,0.3414 -4.500,-0.5264,0.01921,0.01005,0.0041,1.0000,0.4962 -4.250,-0.5121,0.01902,0.01000,0.0075,1.0000,0.5760 -4.000,-0.4963,0.01898,0.01001,0.0109,1.0000,0.6330 -3.750,-0.4800,0.01899,0.00998,0.0143,1.0000,0.6789 -3.500,-0.4616,0.01906,0.01003,0.0175,1.0000,0.7165 -3.250,-0.4428,0.01907,0.00999,0.0203,1.0000,0.7489 -3.000,-0.4217,0.01907,0.00990,0.0225,1.0000,0.7759 -2.750,-0.3998,0.01900,0.00973,0.0243,1.0000,0.7993 -2.500,-0.3756,0.01891,0.00951,0.0254,1.0000,0.8197 -2.250,-0.3526,0.01877,0.00927,0.0263,1.0000,0.8396 -2.000,-0.3237,0.01870,0.00909,0.0261,1.0000,0.8567 -1.750,-0.2933,0.01863,0.00890,0.0254,1.0000,0.8735 -1.500,-0.2610,0.01859,0.00876,0.0242,1.0000,0.8902 -1.250,-0.2267,0.01856,0.00865,0.0223,1.0000,0.9068 -1.000,-0.1904,0.01855,0.00857,0.0199,1.0000,0.9233 -0.750,-0.1518,0.01856,0.00850,0.0168,1.0000,0.9400 -0.500,-0.1104,0.01859,0.00847,0.0130,1.0000,0.9560 -0.250,-0.0564,0.01861,0.00845,0.0067,0.9905,0.9675 0.000,0.0000,0.01863,0.00845,0.0000,0.9788,0.9789 0.250,0.0565,0.01861,0.00845,-0.0067,0.9675,0.9905 0.500,0.1103,0.01858,0.00847,-0.0130,0.9560,1.0000 0.750,0.1518,0.01856,0.00849,-0.0168,0.9400,1.0000 1.000,0.1904,0.01855,0.00856,-0.0199,0.9234,1.0000 1.250,0.2266,0.01856,0.00865,-0.0223,0.9068,1.0000 1.500,0.2609,0.01858,0.00876,-0.0242,0.8902,1.0000 1.750,0.2932,0.01863,0.00890,-0.0254,0.8735,1.0000 2.000,0.3236,0.01869,0.00909,-0.0261,0.8567,1.0000 2.250,0.3525,0.01877,0.00926,-0.0263,0.8396,1.0000 2.500,0.3754,0.01891,0.00950,-0.0253,0.8197,1.0000 2.750,0.3996,0.01899,0.00973,-0.0242,0.7993,1.0000 3.000,0.4215,0.01906,0.00990,-0.0225,0.7759,1.0000 3.250,0.4426,0.01907,0.00998,-0.0203,0.7490,1.0000 3.500,0.4614,0.01906,0.01003,-0.0174,0.7167,1.0000 3.750,0.4798,0.01899,0.00997,-0.0143,0.6791,1.0000 4.000,0.4961,0.01898,0.01000,-0.0109,0.6332,1.0000 4.250,0.5119,0.01902,0.01000,-0.0075,0.5763,1.0000 4.500,0.5262,0.01921,0.01005,-0.0041,0.4967,1.0000 4.750,0.5367,0.01995,0.01007,-0.0003,0.3407,1.0000 5.000,0.5452,0.02184,0.01095,0.0023,0.2054,1.0000 5.250,0.5583,0.02355,0.01223,0.0041,0.1469,1.0000 5.500,0.5738,0.02502,0.01353,0.0058,0.1197,1.0000 5.750,0.5908,0.02634,0.01482,0.0074,0.1004,1.0000 6.000,0.6097,0.02774,0.01626,0.0090,0.0894,1.0000 6.250,0.6297,0.02914,0.01768,0.0102,0.0791,1.0000 6.500,0.6519,0.03063,0.01930,0.0113,0.0717,1.0000 6.750,0.6761,0.03252,0.02132,0.0123,0.0663,1.0000 7.000,0.6981,0.03423,0.02326,0.0133,0.0602,1.0000 7.250,0.7196,0.03649,0.02548,0.0139,0.0565,1.0000 7.500,0.7402,0.03910,0.02863,0.0152,0.0546,1.0000 7.750,0.7568,0.04188,0.03192,0.0166,0.0520,1.0000 8.000,0.7706,0.04450,0.03492,0.0180,0.0492,1.0000 8.250,0.7833,0.04695,0.03762,0.0192,0.0467,1.0000 8.500,0.7933,0.05002,0.04095,0.0204,0.0455,1.0000 8.750,0.7997,0.05361,0.04482,0.0217,0.0448,1.0000 9.000,0.8013,0.05745,0.04896,0.0231,0.0445,1.0000 9.250,0.7981,0.06125,0.05311,0.0245,0.0444,1.0000 9.500,0.7907,0.06518,0.05733,0.0257,0.0443,1.0000 9.750,0.7798,0.06909,0.06147,0.0266,0.0443,1.0000 10.000,0.7650,0.07284,0.06536,0.0274,0.0444,1.0000 10.250,0.7500,0.07692,0.06953,0.0271,0.0445,1.0000