Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca63a210-il-1000000 Airfoil,naca63a210-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,58.5298 Max Cl/Cd alpha,7.5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca63a210-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.5909,0.09156,0.08901,-0.0078,0.4819,0.0066 -8.750,-0.5995,0.08117,0.07862,-0.0195,0.4819,0.0065 -8.500,-0.6164,0.07533,0.07269,-0.0240,0.4819,0.0065 -8.250,-0.6260,0.07145,0.06871,-0.0247,0.4819,0.0065 -8.000,-0.6281,0.06773,0.06489,-0.0252,0.4819,0.0066 -7.750,-0.6260,0.06426,0.06129,-0.0254,0.4819,0.0067 -7.500,-0.6207,0.06086,0.05775,-0.0254,0.4819,0.0068 -7.250,-0.6125,0.05756,0.05429,-0.0251,0.4819,0.0070 -7.000,-0.6018,0.05433,0.05088,-0.0247,0.4819,0.0071 -6.750,-0.5889,0.05121,0.04757,-0.0241,0.4819,0.0073 -6.500,-0.5741,0.04820,0.04436,-0.0233,0.4819,0.0076 -6.250,-0.5575,0.04530,0.04123,-0.0224,0.4819,0.0080 -6.000,-0.5389,0.04257,0.03826,-0.0214,0.4820,0.0085 -5.750,-0.5173,0.04040,0.03585,-0.0203,0.4820,0.0093 -5.500,-0.4906,0.04029,0.03559,-0.0195,0.4820,0.0101 -4.750,-0.4284,0.02458,0.01849,-0.0138,0.4822,0.0065 -4.500,-0.4034,0.02261,0.01643,-0.0131,0.4823,0.0070 -4.250,-0.3768,0.02171,0.01551,-0.0129,0.4825,0.0077 -4.000,-0.3504,0.02088,0.01465,-0.0126,0.4827,0.0085 -3.750,-0.3245,0.02006,0.01378,-0.0121,0.4828,0.0090 -3.500,-0.2988,0.01935,0.01302,-0.0117,0.4831,0.0094 -3.250,-0.2715,0.01915,0.01279,-0.0116,0.4833,0.0101 -3.000,-0.2465,0.01847,0.01205,-0.0111,0.4835,0.0105 -2.750,-0.2217,0.01769,0.01112,-0.0104,0.4837,0.0119 -2.500,-0.1950,0.01743,0.01083,-0.0102,0.4839,0.0147 -2.250,-0.1678,0.01731,0.01068,-0.0101,0.4841,0.0171 -2.000,-0.1440,0.01646,0.01031,-0.0096,0.4844,0.1651 -1.750,-0.1236,0.01521,0.01007,-0.0090,0.4848,0.4551 -1.500,-0.0984,0.01493,0.01010,-0.0087,0.4852,0.5517 -1.250,-0.0732,0.01479,0.01022,-0.0084,0.4856,0.6298 -1.000,-0.0481,0.01477,0.01041,-0.0079,0.4861,0.7008 -0.750,-0.0215,0.01490,0.01059,-0.0077,0.4863,0.7278 -0.500,0.0057,0.01505,0.01076,-0.0077,0.4865,0.7400 -0.250,0.0329,0.01525,0.01096,-0.0077,0.4867,0.7504 0.000,0.0599,0.01553,0.01124,-0.0077,0.4870,0.7616 0.250,0.0869,0.01581,0.01153,-0.0077,0.4871,0.7734 0.500,0.1139,0.01599,0.01175,-0.0076,0.4872,0.7845 0.750,0.1412,0.01611,0.01190,-0.0076,0.4872,0.7957 1.000,0.1684,0.01617,0.01201,-0.0076,0.4872,0.8084 1.250,0.1957,0.01615,0.01205,-0.0075,0.4871,0.8234 1.500,0.2233,0.01589,0.01188,-0.0074,0.4868,0.8406 1.750,0.2507,0.01561,0.01170,-0.0073,0.4861,0.8620 2.000,0.2769,0.01548,0.01168,-0.0069,0.4848,0.8906 2.250,0.3020,0.01579,0.01208,-0.0063,0.4831,0.9259 2.500,0.3281,0.01813,0.01436,-0.0068,0.4820,0.9561 2.750,0.3709,0.01535,0.01168,-0.0089,0.4782,0.9730 3.000,0.4090,0.01452,0.01088,-0.0109,0.4748,0.9834 3.250,0.4489,0.01353,0.00988,-0.0130,0.4562,0.9894 3.500,0.4855,0.01315,0.00943,-0.0148,0.4480,0.9945 3.750,0.5226,0.01321,0.00952,-0.0170,0.4419,0.9980 4.000,0.5550,0.01337,0.00975,-0.0183,0.4361,1.0000 4.250,0.5798,0.01354,0.00995,-0.0178,0.4290,1.0000 4.500,0.6041,0.01388,0.01035,-0.0174,0.4138,1.0000 4.750,0.6294,0.01378,0.00951,-0.0171,0.2693,1.0000 5.000,0.6566,0.01336,0.00867,-0.0169,0.1944,1.0000 5.250,0.6824,0.01328,0.00833,-0.0166,0.1444,1.0000 5.500,0.7076,0.01333,0.00820,-0.0163,0.1078,1.0000 5.750,0.7325,0.01345,0.00817,-0.0159,0.0795,1.0000 6.000,0.7574,0.01362,0.00823,-0.0155,0.0588,1.0000 6.250,0.7825,0.01382,0.00837,-0.0152,0.0442,1.0000 6.500,0.8071,0.01407,0.00853,-0.0148,0.0276,1.0000 6.750,0.8313,0.01438,0.00878,-0.0143,0.0152,1.0000 7.000,0.8559,0.01467,0.00909,-0.0139,0.0108,1.0000 7.250,0.8797,0.01504,0.00952,-0.0133,0.0076,1.0000 7.500,0.9037,0.01544,0.00995,-0.0128,0.0063,1.0000 7.750,0.9258,0.01606,0.01065,-0.0120,0.0054,1.0000 8.000,0.9442,0.01715,0.01190,-0.0106,0.0048,1.0000 8.250,0.9676,0.01765,0.01245,-0.0102,0.0046,1.0000 8.500,0.9886,0.01841,0.01332,-0.0094,0.0045,1.0000 8.750,1.0084,0.01928,0.01429,-0.0084,0.0043,1.0000 9.000,1.0274,0.02022,0.01533,-0.0074,0.0042,1.0000 9.250,1.0458,0.02121,0.01643,-0.0063,0.0040,1.0000 9.500,1.0639,0.02223,0.01754,-0.0053,0.0038,1.0000 9.750,1.0814,0.02330,0.01872,-0.0042,0.0037,1.0000 10.000,1.0989,0.02434,0.01986,-0.0033,0.0035,1.0000 10.250,1.1161,0.02539,0.02099,-0.0024,0.0033,1.0000 10.500,1.1315,0.02657,0.02225,-0.0015,0.0031,1.0000 10.750,1.1390,0.02858,0.02442,0.0002,0.0029,1.0000 11.000,1.1275,0.03252,0.02870,0.0036,0.0027,1.0000 11.250,1.1110,0.03677,0.03327,0.0062,0.0026,1.0000 11.500,1.0992,0.04102,0.03778,0.0063,0.0026,1.0000 11.750,1.0893,0.04623,0.04324,0.0034,0.0026,1.0000 12.000,1.0805,0.05126,0.04845,0.0004,0.0026,1.0000 12.250,1.0697,0.05594,0.05328,-0.0013,0.0026,1.0000 12.500,1.0572,0.06062,0.05809,-0.0031,0.0026,1.0000 12.750,1.0438,0.06546,0.06307,-0.0049,0.0026,1.0000 13.000,1.0298,0.07052,0.06824,-0.0069,0.0027,1.0000 13.250,1.0150,0.07616,0.07400,-0.0096,0.0027,1.0000 13.500,1.0008,0.08234,0.08029,-0.0128,0.0027,1.0000 13.750,0.9866,0.08946,0.08752,-0.0168,0.0027,1.0000