Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca0010-il-200000 Airfoil,naca0010-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,44.4062 Max Cl/Cd alpha,4.25 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca0010-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.750,-0.7617,0.10155,0.09799,0.0000,1.0000,0.0494 -11.500,-0.8675,0.07010,0.06617,-0.0236,1.0000,0.0379 -11.250,-0.8918,0.06396,0.05989,-0.0267,1.0000,0.0375 -11.000,-0.9154,0.05906,0.05480,-0.0272,1.0000,0.0373 -10.750,-0.9373,0.05491,0.05041,-0.0254,1.0000,0.0371 -10.500,-0.9524,0.05047,0.04564,-0.0236,1.0000,0.0371 -10.250,-0.9607,0.04627,0.04103,-0.0215,1.0000,0.0374 -10.000,-0.9614,0.04295,0.03725,-0.0193,1.0000,0.0380 -9.750,-0.9624,0.03858,0.03237,-0.0171,1.0000,0.0392 -9.500,-0.9494,0.03597,0.02968,-0.0162,1.0000,0.0410 -9.250,-0.9324,0.03436,0.02796,-0.0152,1.0000,0.0428 -9.000,-0.9169,0.03218,0.02546,-0.0138,1.0000,0.0446 -8.750,-0.8995,0.03048,0.02341,-0.0124,1.0000,0.0470 -8.500,-0.8824,0.02830,0.02084,-0.0109,1.0000,0.0491 -8.250,-0.8622,0.02622,0.01871,-0.0102,1.0000,0.0516 -8.000,-0.8405,0.02518,0.01757,-0.0094,1.0000,0.0545 -7.750,-0.8182,0.02414,0.01635,-0.0084,1.0000,0.0575 -7.500,-0.7953,0.02328,0.01523,-0.0075,1.0000,0.0595 -7.250,-0.7736,0.02129,0.01323,-0.0067,1.0000,0.0629 -7.000,-0.7508,0.02041,0.01233,-0.0059,1.0000,0.0660 -6.750,-0.7276,0.01954,0.01137,-0.0050,1.0000,0.0689 -6.500,-0.7041,0.01891,0.01062,-0.0041,1.0000,0.0718 -6.250,-0.6833,0.01759,0.00935,-0.0030,1.0000,0.0755 -6.000,-0.6614,0.01684,0.00861,-0.0019,1.0000,0.0795 -5.750,-0.6391,0.01620,0.00790,-0.0008,1.0000,0.0843 -5.500,-0.6189,0.01532,0.00712,0.0006,1.0000,0.0921 -5.250,-0.5982,0.01456,0.00641,0.0018,1.0000,0.1048 -5.000,-0.5782,0.01367,0.00571,0.0032,1.0000,0.1334 -4.750,-0.5583,0.01280,0.00516,0.0044,1.0000,0.1879 -4.500,-0.5375,0.01214,0.00480,0.0054,1.0000,0.2474 -4.250,-0.5160,0.01162,0.00450,0.0065,1.0000,0.3041 -4.000,-0.4944,0.01115,0.00428,0.0075,1.0000,0.3600 -3.750,-0.4725,0.01075,0.00411,0.0085,1.0000,0.4151 -3.500,-0.4503,0.01041,0.00397,0.0095,1.0000,0.4676 -3.250,-0.4281,0.01008,0.00386,0.0106,1.0000,0.5230 -3.000,-0.4060,0.00979,0.00381,0.0118,1.0000,0.5809 -2.750,-0.3834,0.00955,0.00379,0.0129,1.0000,0.6323 -2.500,-0.3604,0.00937,0.00378,0.0141,1.0000,0.6777 -2.250,-0.3373,0.00923,0.00381,0.0152,1.0000,0.7208 -2.000,-0.3143,0.00915,0.00387,0.0165,1.0000,0.7644 -1.750,-0.2921,0.00912,0.00399,0.0180,1.0000,0.8068 -1.500,-0.2705,0.00916,0.00416,0.0197,1.0000,0.8465 -1.250,-0.2491,0.00928,0.00435,0.0214,1.0000,0.8838 -1.000,-0.2245,0.00946,0.00457,0.0224,1.0000,0.9182 -0.750,-0.1738,0.00969,0.00478,0.0180,0.9943,0.9431 -0.500,-0.1201,0.00986,0.00492,0.0129,0.9881,0.9610 -0.250,-0.0607,0.01000,0.00503,0.0066,0.9838,0.9715 0.000,0.0000,0.01004,0.00506,0.0000,0.9778,0.9778 0.250,0.0607,0.01000,0.00503,-0.0066,0.9715,0.9838 0.500,0.1201,0.00986,0.00492,-0.0130,0.9609,0.9881 0.750,0.1738,0.00969,0.00478,-0.0180,0.9431,0.9943 1.000,0.2245,0.00946,0.00457,-0.0224,0.9181,1.0000 1.250,0.2491,0.00928,0.00435,-0.0214,0.8838,1.0000 1.500,0.2705,0.00916,0.00416,-0.0197,0.8465,1.0000 1.750,0.2921,0.00912,0.00399,-0.0180,0.8068,1.0000 2.000,0.3143,0.00915,0.00387,-0.0164,0.7643,1.0000 2.250,0.3373,0.00923,0.00380,-0.0152,0.7208,1.0000 2.500,0.3604,0.00936,0.00378,-0.0141,0.6778,1.0000 2.750,0.3834,0.00955,0.00379,-0.0129,0.6324,1.0000 3.000,0.4060,0.00979,0.00381,-0.0118,0.5811,1.0000 3.250,0.4281,0.01008,0.00386,-0.0106,0.5230,1.0000 3.500,0.4503,0.01041,0.00397,-0.0095,0.4676,1.0000 3.750,0.4725,0.01075,0.00411,-0.0085,0.4152,1.0000 4.000,0.4944,0.01115,0.00428,-0.0075,0.3601,1.0000 4.250,0.5160,0.01162,0.00450,-0.0065,0.3041,1.0000 4.500,0.5375,0.01214,0.00479,-0.0054,0.2474,1.0000 4.750,0.5583,0.01280,0.00516,-0.0044,0.1879,1.0000 5.000,0.5782,0.01367,0.00571,-0.0032,0.1333,1.0000 5.250,0.5982,0.01456,0.00641,-0.0018,0.1048,1.0000 5.500,0.6189,0.01532,0.00712,-0.0006,0.0922,1.0000 5.750,0.6391,0.01620,0.00790,0.0007,0.0843,1.0000 6.000,0.6614,0.01683,0.00861,0.0019,0.0795,1.0000 6.250,0.6833,0.01759,0.00935,0.0030,0.0755,1.0000 6.500,0.7041,0.01891,0.01062,0.0041,0.0718,1.0000 6.750,0.7276,0.01954,0.01137,0.0050,0.0689,1.0000 7.000,0.7508,0.02041,0.01233,0.0059,0.0660,1.0000 7.250,0.7736,0.02129,0.01323,0.0067,0.0629,1.0000 7.500,0.7953,0.02328,0.01523,0.0075,0.0595,1.0000 7.750,0.8183,0.02413,0.01634,0.0084,0.0575,1.0000 8.000,0.8405,0.02518,0.01757,0.0094,0.0545,1.0000 8.250,0.8623,0.02622,0.01871,0.0102,0.0516,1.0000 8.500,0.8825,0.02831,0.02085,0.0109,0.0491,1.0000 8.750,0.8996,0.03049,0.02342,0.0123,0.0470,1.0000 9.000,0.9169,0.03218,0.02546,0.0138,0.0446,1.0000 9.250,0.9325,0.03436,0.02796,0.0152,0.0428,1.0000 9.500,0.9495,0.03595,0.02966,0.0162,0.0409,1.0000 9.750,0.9624,0.03860,0.03240,0.0171,0.0391,1.0000 10.000,0.9615,0.04296,0.03725,0.0193,0.0380,1.0000 10.250,0.9609,0.04628,0.04104,0.0214,0.0374,1.0000 10.500,0.9526,0.05049,0.04566,0.0235,0.0371,1.0000 10.750,0.9374,0.05494,0.05045,0.0253,0.0371,1.0000 11.000,0.9156,0.05910,0.05485,0.0271,0.0372,1.0000 11.250,0.8920,0.06403,0.05996,0.0265,0.0375,1.0000 11.500,0.8678,0.07018,0.06626,0.0234,0.0379,1.0000