Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca63a210-il-100000-n5 Airfoil,naca63a210-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,40.2035 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-naca63a210-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.5920,0.08842,0.08390,-0.0187,1.0000,0.0280 -9.500,-0.5977,0.08179,0.07731,-0.0234,1.0000,0.0276 -9.250,-0.6082,0.07379,0.06932,-0.0306,1.0000,0.0271 -9.000,-0.6239,0.06753,0.06299,-0.0356,1.0000,0.0267 -8.750,-0.6354,0.06213,0.05743,-0.0384,0.9692,0.0264 -8.500,-0.6401,0.05676,0.05181,-0.0405,0.9478,0.0261 -8.250,-0.6399,0.05172,0.04643,-0.0416,0.9343,0.0260 -8.000,-0.6347,0.04702,0.04133,-0.0421,0.9223,0.0260 -7.750,-0.6251,0.04275,0.03660,-0.0422,0.9109,0.0262 -7.500,-0.6114,0.03929,0.03266,-0.0419,0.9022,0.0274 -7.250,-0.5943,0.03632,0.02916,-0.0414,0.8943,0.0291 -7.000,-0.5752,0.03357,0.02587,-0.0408,0.8867,0.0301 -6.750,-0.5540,0.03099,0.02282,-0.0402,0.8796,0.0305 -6.500,-0.5310,0.02887,0.02026,-0.0397,0.8728,0.0310 -6.250,-0.5083,0.02611,0.01722,-0.0393,0.8654,0.0321 -6.000,-0.4841,0.02442,0.01539,-0.0390,0.8577,0.0339 -5.750,-0.4594,0.02332,0.01416,-0.0387,0.8500,0.0371 -5.500,-0.4340,0.02205,0.01272,-0.0383,0.8428,0.0397 -5.250,-0.4091,0.02081,0.01133,-0.0376,0.8345,0.0416 -5.000,-0.3842,0.01977,0.01012,-0.0370,0.8214,0.0436 -4.750,-0.3613,0.01855,0.00887,-0.0363,0.8028,0.0476 -4.500,-0.3364,0.01785,0.00804,-0.0359,0.7826,0.0553 -4.250,-0.3123,0.01703,0.00713,-0.0353,0.7624,0.0658 -4.000,-0.2881,0.01627,0.00631,-0.0347,0.7438,0.0862 -3.750,-0.2659,0.01517,0.00554,-0.0340,0.7271,0.1571 -3.500,-0.2488,0.01353,0.00505,-0.0329,0.7121,0.4030 -3.250,-0.2278,0.01304,0.00497,-0.0313,0.6948,0.5394 -3.000,-0.2054,0.01289,0.00493,-0.0296,0.6734,0.6169 -2.750,-0.1833,0.01285,0.00493,-0.0278,0.6615,0.6785 -2.500,-0.1610,0.01285,0.00490,-0.0259,0.6558,0.7256 -2.000,-0.1120,0.01271,0.00462,-0.0236,0.6482,0.7775 -1.750,-0.0858,0.01262,0.00444,-0.0231,0.6460,0.7945 -1.500,-0.0593,0.01252,0.00424,-0.0226,0.6439,0.8103 -1.250,-0.0326,0.01243,0.00408,-0.0222,0.6420,0.8261 -1.000,-0.0055,0.01236,0.00395,-0.0218,0.6401,0.8420 -0.750,0.0225,0.01229,0.00385,-0.0216,0.6384,0.8584 -0.500,0.0516,0.01224,0.00375,-0.0217,0.6362,0.8754 -0.250,0.0826,0.01222,0.00368,-0.0222,0.6334,0.8927 0.000,0.1159,0.01221,0.00364,-0.0233,0.6303,0.9104 0.250,0.1515,0.01221,0.00360,-0.0249,0.6270,0.9282 0.500,0.1887,0.01224,0.00358,-0.0269,0.6229,0.9460 0.750,0.2271,0.01226,0.00357,-0.0293,0.6182,0.9640 1.000,0.2659,0.01229,0.00359,-0.0318,0.6141,0.9824 1.250,0.3066,0.01231,0.00362,-0.0349,0.6109,0.9993 1.500,0.3311,0.01237,0.00367,-0.0346,0.6071,1.0000 1.750,0.3555,0.01244,0.00377,-0.0343,0.6031,1.0000 2.000,0.3806,0.01254,0.00393,-0.0340,0.5989,1.0000 2.250,0.4060,0.01263,0.00409,-0.0337,0.5940,1.0000 2.500,0.4315,0.01272,0.00430,-0.0335,0.5869,1.0000 2.750,0.4568,0.01285,0.00450,-0.0332,0.5764,1.0000 3.000,0.4817,0.01309,0.00467,-0.0325,0.5660,1.0000 3.250,0.5072,0.01347,0.00483,-0.0320,0.5566,1.0000 3.500,0.5363,0.01448,0.00541,-0.0322,0.5443,1.0000 3.750,0.5645,0.01687,0.00746,-0.0328,0.5235,1.0000 4.000,0.5849,0.01933,0.01010,-0.0323,0.5004,1.0000 4.250,0.6051,0.01562,0.00716,-0.0300,0.4567,1.0000 4.500,0.6287,0.01626,0.00759,-0.0293,0.4273,1.0000 4.750,0.6521,0.01622,0.00785,-0.0284,0.3451,1.0000 5.000,0.6678,0.01729,0.00808,-0.0269,0.1913,1.0000 5.250,0.6841,0.01866,0.00884,-0.0255,0.1005,1.0000 5.500,0.7028,0.01975,0.00974,-0.0243,0.0697,1.0000 5.750,0.7226,0.02069,0.01066,-0.0232,0.0556,1.0000 6.000,0.7431,0.02155,0.01164,-0.0220,0.0480,1.0000 6.250,0.7617,0.02261,0.01276,-0.0207,0.0434,1.0000 6.500,0.7789,0.02393,0.01413,-0.0191,0.0406,1.0000 6.750,0.7990,0.02505,0.01539,-0.0178,0.0379,1.0000 7.000,0.8195,0.02616,0.01664,-0.0168,0.0346,1.0000 7.250,0.8396,0.02741,0.01794,-0.0159,0.0322,1.0000 7.500,0.8596,0.02909,0.01969,-0.0148,0.0308,1.0000 7.750,0.8797,0.03160,0.02232,-0.0139,0.0296,1.0000 8.000,0.9011,0.03357,0.02453,-0.0129,0.0290,1.0000 8.250,0.9209,0.03580,0.02709,-0.0118,0.0285,1.0000 8.500,0.9384,0.03836,0.03007,-0.0105,0.0280,1.0000 8.750,0.9526,0.04114,0.03328,-0.0090,0.0275,1.0000 9.000,0.9637,0.04388,0.03646,-0.0072,0.0265,1.0000 9.250,0.9717,0.04666,0.03963,-0.0055,0.0252,1.0000 9.500,0.9762,0.04968,0.04302,-0.0037,0.0243,1.0000 9.750,0.9751,0.05328,0.04699,-0.0018,0.0241,1.0000 10.000,0.9685,0.05707,0.05113,0.0001,0.0239,1.0000 10.250,0.9554,0.06085,0.05519,0.0021,0.0239,1.0000 10.500,0.9378,0.06496,0.05955,0.0031,0.0239,1.0000 10.750,0.9171,0.06991,0.06472,0.0022,0.0241,1.0000 11.000,0.8940,0.07624,0.07123,-0.0012,0.0243,1.0000 11.250,0.8685,0.08454,0.07968,-0.0075,0.0247,1.0000