Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m10-il-200000-n5 Airfoil,m10-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,54.9417 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-m10-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.5816,0.09642,0.09302,0.0099,1.0000,0.0131 -8.250,-0.5820,0.09164,0.08828,0.0069,1.0000,0.0128 -8.000,-0.5838,0.08661,0.08330,0.0031,1.0000,0.0125 -7.750,-0.5817,0.08068,0.07738,-0.0029,1.0000,0.0123 -7.500,-0.5756,0.07455,0.07123,-0.0085,1.0000,0.0122 -7.250,-0.5664,0.06887,0.06550,-0.0132,1.0000,0.0122 -7.000,-0.5543,0.06369,0.06023,-0.0170,1.0000,0.0124 -6.750,-0.5387,0.06037,0.05683,-0.0192,1.0000,0.0133 -6.500,-0.5221,0.05583,0.05217,-0.0219,1.0000,0.0143 -6.250,-0.5047,0.05000,0.04612,-0.0246,1.0000,0.0150 -6.000,-0.4864,0.04348,0.03929,-0.0266,1.0000,0.0153 -5.750,-0.4670,0.03634,0.03168,-0.0277,1.0000,0.0159 -5.500,-0.4476,0.02739,0.02185,-0.0276,1.0000,0.0176 -5.250,-0.4248,0.02340,0.01722,-0.0272,1.0000,0.0199 -5.000,-0.4001,0.02259,0.01629,-0.0271,1.0000,0.0217 -4.750,-0.3749,0.02111,0.01447,-0.0267,1.0000,0.0246 -4.500,-0.3489,0.01960,0.01252,-0.0262,1.0000,0.0290 -4.250,-0.3233,0.01813,0.01068,-0.0257,1.0000,0.0314 -4.000,-0.2984,0.01740,0.00993,-0.0255,1.0000,0.0348 -3.750,-0.2729,0.01654,0.00888,-0.0251,1.0000,0.0373 -3.500,-0.2476,0.01587,0.00803,-0.0245,1.0000,0.0402 -3.250,-0.2226,0.01504,0.00704,-0.0239,1.0000,0.0414 -3.000,-0.1983,0.01419,0.00610,-0.0232,1.0000,0.0426 -2.750,-0.1746,0.01335,0.00525,-0.0225,1.0000,0.0445 -2.500,-0.1416,0.01279,0.00464,-0.0238,0.9933,0.0464 -2.250,-0.1063,0.01231,0.00413,-0.0256,0.9825,0.0482 -2.000,-0.0712,0.01196,0.00376,-0.0273,0.9698,0.0516 -1.750,-0.0367,0.01161,0.00335,-0.0287,0.9554,0.0539 -1.500,-0.0029,0.01129,0.00297,-0.0300,0.9394,0.0551 -1.250,0.0290,0.01095,0.00262,-0.0308,0.9211,0.0589 -1.000,0.0590,0.01073,0.00237,-0.0310,0.9013,0.0671 -0.750,0.0869,0.01045,0.00218,-0.0309,0.8811,0.0985 -0.500,0.1128,0.00998,0.00206,-0.0306,0.8605,0.2095 -0.250,0.1259,0.00783,0.00211,-0.0269,0.8421,0.8762 0.250,0.2052,0.00785,0.00197,-0.0314,0.8037,1.0000 0.500,0.2303,0.00794,0.00192,-0.0307,0.7846,1.0000 0.750,0.2559,0.00803,0.00190,-0.0300,0.7657,1.0000 1.000,0.2816,0.00813,0.00190,-0.0295,0.7474,1.0000 1.250,0.3075,0.00823,0.00192,-0.0289,0.7298,1.0000 1.500,0.3336,0.00835,0.00196,-0.0284,0.7124,1.0000 1.750,0.3598,0.00846,0.00202,-0.0280,0.6948,1.0000 2.000,0.3861,0.00859,0.00209,-0.0276,0.6772,1.0000 2.250,0.4122,0.00873,0.00218,-0.0271,0.6550,1.0000 2.500,0.4379,0.00891,0.00226,-0.0266,0.6247,1.0000 2.750,0.4636,0.00911,0.00234,-0.0261,0.5893,1.0000 3.000,0.4895,0.00932,0.00248,-0.0256,0.5568,1.0000 3.250,0.5154,0.00956,0.00263,-0.0252,0.5208,1.0000 3.500,0.5409,0.00987,0.00279,-0.0247,0.4729,1.0000 3.750,0.5659,0.01030,0.00301,-0.0243,0.4080,1.0000 4.000,0.5904,0.01088,0.00329,-0.0239,0.3301,1.0000 4.250,0.6130,0.01194,0.00376,-0.0236,0.1968,1.0000 4.500,0.6350,0.01330,0.00449,-0.0233,0.0743,1.0000 4.750,0.6601,0.01398,0.00511,-0.0230,0.0546,1.0000 5.000,0.6854,0.01455,0.00576,-0.0227,0.0444,1.0000 5.250,0.7102,0.01523,0.00650,-0.0223,0.0358,1.0000 5.500,0.7338,0.01616,0.00749,-0.0218,0.0295,1.0000 5.750,0.7587,0.01679,0.00826,-0.0214,0.0242,1.0000 6.000,0.7821,0.01775,0.00932,-0.0208,0.0207,1.0000 6.250,0.8037,0.01911,0.01076,-0.0199,0.0179,1.0000 6.500,0.8270,0.02017,0.01197,-0.0192,0.0160,1.0000 6.750,0.8494,0.02163,0.01358,-0.0183,0.0146,1.0000 7.000,0.8719,0.02322,0.01535,-0.0174,0.0135,1.0000 7.250,0.8945,0.02440,0.01666,-0.0168,0.0122,1.0000 7.500,0.9137,0.02684,0.01936,-0.0159,0.0108,1.0000 7.750,0.9329,0.02966,0.02261,-0.0148,0.0103,1.0000 8.000,0.9510,0.03242,0.02580,-0.0135,0.0100,1.0000 8.250,0.9658,0.03576,0.02961,-0.0121,0.0097,1.0000 8.500,0.9765,0.03964,0.03398,-0.0106,0.0096,1.0000 8.750,0.9825,0.04399,0.03880,-0.0090,0.0095,1.0000 9.000,0.9836,0.04859,0.04382,-0.0074,0.0094,1.0000 9.250,0.9806,0.05318,0.04878,-0.0060,0.0093,1.0000 9.500,0.9727,0.05774,0.05364,-0.0049,0.0092,1.0000 9.750,0.9578,0.06202,0.05815,-0.0039,0.0092,1.0000 10.000,0.9395,0.06677,0.06308,-0.0048,0.0092,1.0000 10.250,0.9205,0.07286,0.06932,-0.0087,0.0094,1.0000 10.500,0.9015,0.08071,0.07729,-0.0152,0.0096,1.0000