Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m7-il-500000-n5 Airfoil,m7-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,75.0962 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-m7-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.250,-0.4967,0.10165,0.09884,0.0369,0.6722,0.0040 -7.000,-0.4914,0.09839,0.09556,0.0345,0.6658,0.0041 -6.750,-0.4816,0.09485,0.09200,0.0316,0.6598,0.0042 -6.500,-0.4701,0.09128,0.08839,0.0287,0.6535,0.0043 -6.250,-0.4569,0.08767,0.08474,0.0257,0.6477,0.0044 -6.000,-0.4421,0.08403,0.08105,0.0227,0.6417,0.0046 -5.750,-0.4255,0.08038,0.07734,0.0198,0.6358,0.0048 -5.500,-0.4070,0.07673,0.07362,0.0169,0.6302,0.0052 -5.250,-0.3844,0.07317,0.06999,0.0137,0.6243,0.0055 -4.750,-0.3304,0.06642,0.06303,0.0068,0.6134,0.0057 -1.000,0.0665,0.02430,0.01871,-0.0016,0.5336,0.0089 -0.500,0.1216,0.01901,0.01288,-0.0006,0.5239,0.0100 -0.250,0.1493,0.01787,0.01156,-0.0006,0.5186,0.0116 0.250,0.2090,0.01435,0.00741,0.0009,0.5088,0.0080 0.500,0.2379,0.01310,0.00589,0.0012,0.5036,0.0075 0.750,0.2665,0.01214,0.00474,0.0016,0.4967,0.0072 1.000,0.2946,0.01143,0.00385,0.0018,0.4860,0.0073 1.250,0.3223,0.01091,0.00320,0.0021,0.4743,0.0079 1.500,0.3497,0.01051,0.00272,0.0023,0.4648,0.0098 1.750,0.3769,0.01015,0.00230,0.0024,0.4575,0.0106 2.000,0.4047,0.00994,0.00203,0.0025,0.4493,0.0118 2.250,0.4326,0.00985,0.00185,0.0025,0.4404,0.0146 2.500,0.4608,0.00982,0.00169,0.0024,0.4301,0.0174 2.750,0.4889,0.00978,0.00165,0.0023,0.4212,0.0328 3.000,0.5166,0.00970,0.00171,0.0022,0.4108,0.1208 3.250,0.5446,0.00974,0.00177,0.0019,0.3973,0.1653 3.750,0.6181,0.00832,0.00212,-0.0025,0.3628,0.9904 4.250,0.7029,0.00936,0.00262,-0.0102,0.2575,0.9994 4.500,0.7335,0.01150,0.00374,-0.0129,0.0478,1.0000 4.750,0.7591,0.01172,0.00394,-0.0128,0.0423,1.0000 5.000,0.7847,0.01193,0.00416,-0.0126,0.0412,1.0000 5.250,0.8101,0.01214,0.00438,-0.0123,0.0405,1.0000 5.500,0.8355,0.01237,0.00463,-0.0121,0.0399,1.0000 5.750,0.8608,0.01262,0.00490,-0.0119,0.0394,1.0000 6.000,0.8860,0.01289,0.00522,-0.0118,0.0389,1.0000 6.250,0.9110,0.01317,0.00554,-0.0116,0.0384,1.0000 6.500,0.9360,0.01349,0.00590,-0.0114,0.0380,1.0000 6.750,0.9608,0.01383,0.00631,-0.0112,0.0375,1.0000 7.000,0.9854,0.01420,0.00674,-0.0110,0.0370,1.0000 7.250,1.0098,0.01462,0.00723,-0.0108,0.0364,1.0000 7.500,1.0339,0.01508,0.00776,-0.0107,0.0357,1.0000 7.750,1.0575,0.01562,0.00839,-0.0105,0.0349,1.0000 8.000,1.0804,0.01628,0.00915,-0.0103,0.0339,1.0000 8.250,1.1024,0.01705,0.01002,-0.0100,0.0326,1.0000 8.500,1.1274,0.01705,0.01005,-0.0098,0.0314,1.0000 8.750,1.1518,0.01722,0.01029,-0.0096,0.0288,1.0000 9.000,1.1757,0.01747,0.01057,-0.0094,0.0246,1.0000 9.250,1.1988,0.01784,0.01094,-0.0092,0.0173,1.0000 9.500,1.2153,0.01926,0.01226,-0.0088,0.0049,1.0000 9.750,1.2318,0.02051,0.01363,-0.0082,0.0036,1.0000 10.000,1.2493,0.02152,0.01477,-0.0076,0.0031,1.0000 10.250,1.2647,0.02267,0.01606,-0.0069,0.0027,1.0000 10.500,1.2772,0.02406,0.01759,-0.0062,0.0024,1.0000 10.750,1.2853,0.02585,0.01957,-0.0056,0.0022,1.0000 11.000,1.2900,0.02768,0.02153,-0.0050,0.0021,1.0000 11.250,1.2947,0.02964,0.02362,-0.0046,0.0019,1.0000 11.500,1.2993,0.03180,0.02590,-0.0045,0.0017,1.0000 11.750,1.3035,0.03408,0.02829,-0.0045,0.0015,1.0000 12.000,1.3052,0.03669,0.03102,-0.0046,0.0014,1.0000 12.250,1.3039,0.03971,0.03415,-0.0048,0.0014,1.0000 12.500,1.2995,0.04312,0.03769,-0.0051,0.0013,1.0000 12.750,1.2939,0.04671,0.04140,-0.0055,0.0013,1.0000 13.000,1.2917,0.04994,0.04477,-0.0058,0.0012,1.0000 13.250,1.2885,0.05333,0.04830,-0.0062,0.0012,1.0000 13.500,1.2839,0.05696,0.05207,-0.0068,0.0012,1.0000 13.750,1.2782,0.06076,0.05601,-0.0074,0.0011,1.0000 14.000,1.2721,0.06476,0.06015,-0.0082,0.0011,1.0000 14.250,1.2656,0.06900,0.06453,-0.0092,0.0011,1.0000 14.500,1.2585,0.07349,0.06917,-0.0104,0.0010,1.0000 14.750,1.2507,0.07824,0.07407,-0.0119,0.0010,1.0000 15.000,1.2420,0.08324,0.07923,-0.0135,0.0010,1.0000 15.250,1.2326,0.08853,0.08466,-0.0153,0.0010,1.0000 15.500,1.2226,0.09410,0.09039,-0.0174,0.0010,1.0000 15.750,1.2118,0.09992,0.09636,-0.0196,0.0010,1.0000 16.000,1.2002,0.10610,0.10268,-0.0222,0.0010,1.0000 16.250,1.1881,0.11257,0.10930,-0.0250,0.0010,1.0000 16.500,1.1757,0.11925,0.11611,-0.0279,0.0010,1.0000 16.750,1.1628,0.12628,0.12329,-0.0312,0.0010,1.0000 17.000,1.1502,0.13351,0.13065,-0.0346,0.0010,1.0000