Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m17-il-100000 Airfoil,m17-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,55.174 Max Cl/Cd alpha,7.75 Url,http://airfoiltools.com/polar/csv?polar=xf-m17-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.4342,0.09935,0.09499,-0.0008,1.0000,0.0662 -7.750,-0.4320,0.09642,0.09213,-0.0050,1.0000,0.0686 -7.500,-0.4280,0.09498,0.09068,-0.0154,1.0000,0.0704 -7.250,-0.4190,0.09121,0.08689,-0.0212,1.0000,0.0713 -7.000,-0.4090,0.08487,0.08068,-0.0149,1.0000,0.0739 -6.750,-0.3969,0.08126,0.07710,-0.0160,1.0000,0.0769 -6.500,-0.3833,0.07779,0.07364,-0.0195,1.0000,0.0807 -6.250,-0.3588,0.07795,0.07342,-0.0315,1.0000,0.0853 -6.000,-0.3539,0.07127,0.06699,-0.0297,1.0000,0.0866 -5.750,-0.3613,0.06922,0.06505,-0.0266,0.9981,0.0877 -5.500,-0.3263,0.06460,0.06036,-0.0316,0.9864,0.0942 -5.250,-0.2846,0.05990,0.05540,-0.0402,0.9729,0.1027 -5.000,-0.2494,0.05613,0.05150,-0.0446,0.9593,0.1111 -4.750,-0.2165,0.05224,0.04739,-0.0491,0.9444,0.1181 -4.500,-0.1842,0.05025,0.04498,-0.0523,0.9286,0.1304 -4.250,-0.1671,0.04672,0.04154,-0.0515,0.9138,0.1362 -4.000,-0.1462,0.04450,0.03911,-0.0516,0.8989,0.1485 -3.750,-0.1254,0.04260,0.03697,-0.0514,0.8850,0.1617 -3.500,-0.1053,0.04075,0.03493,-0.0508,0.8720,0.1760 -3.250,-0.0858,0.03877,0.03281,-0.0500,0.8599,0.1912 -3.000,-0.0666,0.03680,0.03074,-0.0489,0.8490,0.2079 -2.750,-0.0479,0.03515,0.02895,-0.0477,0.8389,0.2358 -2.500,-0.0292,0.03359,0.02734,-0.0465,0.8277,0.2740 -2.250,-0.0116,0.03194,0.02560,-0.0451,0.8179,0.3195 -2.000,0.0060,0.02960,0.02325,-0.0433,0.8095,0.3536 -1.750,0.0781,0.02768,0.01947,-0.0465,0.8003,0.1268 -1.500,0.1063,0.02577,0.01711,-0.0453,0.7927,0.1097 -1.250,0.1343,0.02445,0.01548,-0.0448,0.7833,0.1055 -1.000,0.1614,0.02357,0.01437,-0.0443,0.7749,0.1065 -0.750,0.1890,0.02262,0.01313,-0.0435,0.7669,0.1045 -0.500,0.2171,0.02188,0.01222,-0.0432,0.7584,0.1040 -0.250,0.2438,0.02121,0.01145,-0.0424,0.7512,0.1054 0.000,0.2715,0.02073,0.01095,-0.0423,0.7425,0.1086 0.250,0.2976,0.02027,0.01039,-0.0414,0.7360,0.1136 0.500,0.3243,0.01991,0.01017,-0.0413,0.7273,0.1264 0.750,0.3505,0.01949,0.00975,-0.0404,0.7211,0.1466 1.000,0.4346,0.01708,0.00928,-0.0515,0.7123,1.0000 1.250,0.4586,0.01729,0.00928,-0.0504,0.7061,1.0000 1.500,0.4842,0.01767,0.00958,-0.0504,0.6976,1.0000 1.750,0.5083,0.01789,0.00967,-0.0494,0.6915,1.0000 2.000,0.5337,0.01833,0.01008,-0.0494,0.6834,1.0000 2.250,0.5579,0.01857,0.01022,-0.0485,0.6773,1.0000 2.500,0.5828,0.01904,0.01070,-0.0484,0.6694,1.0000 2.750,0.6072,0.01933,0.01094,-0.0477,0.6632,1.0000 3.000,0.6317,0.01981,0.01144,-0.0474,0.6558,1.0000 3.250,0.6561,0.02015,0.01176,-0.0468,0.6492,1.0000 3.500,0.6804,0.02061,0.01225,-0.0463,0.6423,1.0000 3.750,0.7046,0.02101,0.01269,-0.0458,0.6350,1.0000 4.000,0.7287,0.02142,0.01312,-0.0452,0.6285,1.0000 4.250,0.7526,0.02186,0.01362,-0.0446,0.6204,1.0000 4.500,0.7763,0.02220,0.01401,-0.0438,0.6125,1.0000 4.750,0.8005,0.02222,0.01407,-0.0426,0.6037,1.0000 5.000,0.8237,0.02254,0.01447,-0.0418,0.5930,1.0000 5.250,0.8485,0.02248,0.01442,-0.0405,0.5857,1.0000 5.500,0.8719,0.02290,0.01498,-0.0399,0.5758,1.0000 5.750,0.8956,0.02327,0.01549,-0.0392,0.5668,1.0000 6.000,0.9208,0.02328,0.01556,-0.0381,0.5589,1.0000 6.250,0.9438,0.02373,0.01620,-0.0375,0.5482,1.0000 6.500,0.9683,0.02384,0.01644,-0.0365,0.5388,1.0000 6.750,0.9931,0.02295,0.01563,-0.0345,0.5209,1.0000 7.000,1.0181,0.02122,0.01380,-0.0318,0.4937,1.0000 7.250,1.0417,0.02025,0.01285,-0.0298,0.4665,1.0000 7.500,1.0634,0.01960,0.01232,-0.0280,0.4295,1.0000 7.750,1.0781,0.01954,0.01196,-0.0254,0.3210,1.0000 8.000,1.0677,0.02341,0.01417,-0.0219,0.1139,1.0000 8.250,1.0695,0.02604,0.01638,-0.0193,0.0797,1.0000 8.500,1.0765,0.02786,0.01824,-0.0171,0.0700,1.0000 8.750,1.0810,0.02973,0.02015,-0.0147,0.0642,1.0000 9.000,1.0871,0.03139,0.02187,-0.0124,0.0596,1.0000 9.250,1.0906,0.03319,0.02365,-0.0098,0.0570,1.0000 9.500,1.1030,0.03517,0.02555,-0.0075,0.0547,1.0000 9.750,1.1265,0.03680,0.02728,-0.0063,0.0529,1.0000 10.000,1.1502,0.03864,0.02922,-0.0054,0.0500,1.0000 10.250,1.1736,0.04075,0.03141,-0.0047,0.0474,1.0000 10.500,1.2019,0.04351,0.03432,-0.0044,0.0466,1.0000 10.750,1.2249,0.04657,0.03765,-0.0036,0.0465,1.0000 11.000,1.2410,0.04985,0.04133,-0.0023,0.0471,1.0000 11.250,1.2447,0.05330,0.04529,-0.0002,0.0480,1.0000 11.500,1.2431,0.05683,0.04924,0.0020,0.0487,1.0000 11.750,1.2354,0.06021,0.05297,0.0045,0.0491,1.0000 12.000,1.2233,0.06370,0.05677,0.0066,0.0496,1.0000 12.250,1.2083,0.06751,0.06086,0.0079,0.0501,1.0000 12.500,1.1911,0.07175,0.06537,0.0084,0.0507,1.0000 12.750,1.1722,0.07644,0.07030,0.0081,0.0513,1.0000 13.000,1.1522,0.08160,0.07567,0.0071,0.0519,1.0000 13.250,1.1316,0.08723,0.08149,0.0054,0.0526,1.0000 13.500,1.1111,0.09334,0.08776,0.0032,0.0533,1.0000 13.750,1.0928,0.09985,0.09439,0.0008,0.0541,1.0000 14.000,1.0929,0.10554,0.10015,0.0002,0.0556,1.0000