Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-s1010-il-1000000-n5 Airfoil,s1010-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,69.2076 Max Cl/Cd alpha,7 Url,http://www.airfoiltools.com/polar/csv?polar=xf-s1010-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.750,-0.9092,0.10699,0.10526,0.0181,1.0000,0.0025 -13.500,-1.0247,0.07966,0.07783,0.0013,1.0000,0.0021 -13.250,-1.1632,0.04517,0.04300,-0.0243,1.0000,0.0017 -13.000,-1.1967,0.03985,0.03746,-0.0231,1.0000,0.0018 -12.750,-1.2085,0.03627,0.03365,-0.0212,1.0000,0.0018 -12.500,-1.2096,0.03320,0.03034,-0.0198,1.0000,0.0018 -12.250,-1.2058,0.03044,0.02733,-0.0184,1.0000,0.0019 -12.000,-1.1963,0.02823,0.02490,-0.0173,1.0000,0.0019 -11.750,-1.1828,0.02646,0.02294,-0.0163,1.0000,0.0020 -11.500,-1.1668,0.02495,0.02127,-0.0153,1.0000,0.0021 -11.250,-1.1494,0.02357,0.01972,-0.0145,1.0000,0.0022 -11.000,-1.1301,0.02244,0.01846,-0.0138,1.0000,0.0023 -10.750,-1.1106,0.02128,0.01714,-0.0130,1.0000,0.0024 -10.500,-1.0907,0.02011,0.01579,-0.0122,1.0000,0.0024 -10.250,-1.0694,0.01916,0.01470,-0.0116,1.0000,0.0025 -10.000,-1.0477,0.01822,0.01362,-0.0109,1.0000,0.0026 -9.750,-1.0253,0.01739,0.01267,-0.0103,1.0000,0.0028 -9.500,-1.0026,0.01657,0.01172,-0.0097,1.0000,0.0029 -9.250,-0.9795,0.01583,0.01086,-0.0091,1.0000,0.0030 -9.000,-0.9560,0.01513,0.01005,-0.0085,1.0000,0.0031 -8.750,-0.9319,0.01453,0.00936,-0.0080,1.0000,0.0032 -8.500,-0.9076,0.01398,0.00872,-0.0075,1.0000,0.0033 -8.250,-0.8841,0.01317,0.00776,-0.0068,1.0000,0.0040 -8.000,-0.8597,0.01262,0.00718,-0.0063,1.0000,0.0048 -7.750,-0.8348,0.01219,0.00672,-0.0058,1.0000,0.0057 -7.500,-0.8097,0.01180,0.00628,-0.0054,1.0000,0.0063 -7.250,-0.7849,0.01135,0.00578,-0.0049,1.0000,0.0077 -7.000,-0.7598,0.01098,0.00541,-0.0044,1.0000,0.0092 -6.750,-0.7345,0.01069,0.00508,-0.0039,1.0000,0.0104 -6.500,-0.7092,0.01042,0.00476,-0.0034,1.0000,0.0111 -6.250,-0.6840,0.01016,0.00446,-0.0029,1.0000,0.0116 -6.000,-0.6593,0.00979,0.00405,-0.0022,1.0000,0.0132 -5.750,-0.6347,0.00948,0.00374,-0.0016,1.0000,0.0150 -5.500,-0.6101,0.00921,0.00346,-0.0009,1.0000,0.0164 -5.250,-0.5855,0.00898,0.00320,-0.0002,1.0000,0.0175 -5.000,-0.5612,0.00868,0.00292,0.0005,1.0000,0.0219 -4.750,-0.5371,0.00842,0.00266,0.0013,1.0000,0.0281 -4.500,-0.5131,0.00817,0.00245,0.0021,1.0000,0.0361 -4.250,-0.4825,0.00794,0.00226,0.0015,0.9982,0.0434 -4.000,-0.4509,0.00777,0.00209,0.0006,0.9961,0.0490 -3.750,-0.4190,0.00757,0.00193,-0.0003,0.9941,0.0576 -3.500,-0.3885,0.00739,0.00179,-0.0009,0.9914,0.0653 -3.000,-0.3259,0.00705,0.00152,-0.0024,0.9859,0.0866 -2.750,-0.2938,0.00688,0.00142,-0.0034,0.9832,0.1008 -2.500,-0.2613,0.00669,0.00131,-0.0044,0.9743,0.1189 -2.250,-0.2269,0.00654,0.00117,-0.0056,0.9481,0.1328 -2.000,-0.2016,0.00649,0.00106,-0.0047,0.9072,0.1454 -1.750,-0.1766,0.00644,0.00097,-0.0038,0.8773,0.1610 -1.500,-0.1510,0.00636,0.00089,-0.0032,0.8503,0.1849 -1.250,-0.1249,0.00628,0.00081,-0.0027,0.8248,0.2103 -1.000,-0.0989,0.00618,0.00075,-0.0023,0.7964,0.2457 -0.750,-0.0734,0.00614,0.00069,-0.0017,0.7498,0.2832 -0.500,-0.0493,0.00624,0.00064,-0.0010,0.6531,0.3351 -0.250,-0.0250,0.00640,0.00063,-0.0004,0.5456,0.3925 0.000,0.0000,0.00641,0.00063,0.0000,0.4678,0.4680 0.250,0.0249,0.00641,0.00063,0.0004,0.3909,0.5460 0.500,0.0493,0.00624,0.00064,0.0009,0.3348,0.6523 0.750,0.0734,0.00614,0.00069,0.0017,0.2826,0.7499 1.000,0.0990,0.00618,0.00075,0.0023,0.2459,0.7965 1.250,0.1249,0.00628,0.00081,0.0027,0.2104,0.8247 1.500,0.1510,0.00636,0.00089,0.0032,0.1847,0.8500 1.750,0.1766,0.00644,0.00097,0.0038,0.1613,0.8771 2.000,0.2017,0.00649,0.00106,0.0047,0.1454,0.9072 2.250,0.2270,0.00654,0.00117,0.0056,0.1328,0.9481 2.500,0.2614,0.00669,0.00131,0.0043,0.1189,0.9744 2.750,0.2940,0.00687,0.00142,0.0033,0.1024,0.9833 3.000,0.3261,0.00705,0.00152,0.0024,0.0864,0.9859 3.500,0.3887,0.00739,0.00179,0.0008,0.0655,0.9916 3.750,0.4193,0.00757,0.00193,0.0002,0.0574,0.9942 4.000,0.4512,0.00777,0.00209,-0.0007,0.0490,0.9962 4.250,0.4828,0.00795,0.00226,-0.0015,0.0433,0.9984 4.500,0.5127,0.00817,0.00245,-0.0020,0.0362,1.0000 4.750,0.5366,0.00842,0.00266,-0.0012,0.0282,1.0000 5.000,0.5608,0.00868,0.00292,-0.0005,0.0220,1.0000 5.250,0.5851,0.00898,0.00320,0.0003,0.0176,1.0000 5.500,0.6098,0.00921,0.00346,0.0010,0.0165,1.0000 5.750,0.6344,0.00948,0.00374,0.0017,0.0150,1.0000 6.000,0.6591,0.00979,0.00405,0.0023,0.0132,1.0000 6.250,0.6838,0.01016,0.00446,0.0029,0.0115,1.0000 6.500,0.7091,0.01043,0.00476,0.0034,0.0111,1.0000 6.750,0.7345,0.01069,0.00508,0.0039,0.0104,1.0000 7.000,0.7599,0.01098,0.00541,0.0044,0.0092,1.0000 7.250,0.7850,0.01135,0.00579,0.0048,0.0078,1.0000 7.500,0.8099,0.01180,0.00627,0.0054,0.0063,1.0000 7.750,0.8350,0.01219,0.00672,0.0058,0.0057,1.0000 8.000,0.8598,0.01263,0.00719,0.0063,0.0048,1.0000 8.250,0.8843,0.01317,0.00776,0.0068,0.0040,1.0000 8.500,0.9079,0.01397,0.00871,0.0074,0.0033,1.0000 8.750,0.9322,0.01453,0.00935,0.0079,0.0032,1.0000 9.000,0.9562,0.01514,0.01006,0.0085,0.0031,1.0000 9.250,0.9798,0.01582,0.01086,0.0090,0.0030,1.0000 9.500,1.0031,0.01654,0.01168,0.0096,0.0029,1.0000 9.750,1.0259,0.01734,0.01261,0.0102,0.0027,1.0000 10.000,1.0481,0.01822,0.01362,0.0108,0.0026,1.0000 10.250,1.0699,0.01914,0.01467,0.0115,0.0025,1.0000 10.500,1.0909,0.02017,0.01585,0.0122,0.0024,1.0000 10.750,1.1116,0.02117,0.01702,0.0128,0.0023,1.0000 11.000,1.1312,0.02234,0.01834,0.0136,0.0023,1.0000 11.250,1.1497,0.02362,0.01978,0.0144,0.0022,1.0000 11.500,1.1677,0.02491,0.02122,0.0152,0.0021,1.0000 11.750,1.1841,0.02637,0.02283,0.0161,0.0020,1.0000 12.000,1.1967,0.02829,0.02497,0.0171,0.0019,1.0000 12.250,1.2062,0.03050,0.02739,0.0183,0.0019,1.0000 12.500,1.2112,0.03311,0.03024,0.0196,0.0019,1.0000 12.750,1.2095,0.03628,0.03366,0.0210,0.0018,1.0000 13.000,1.1886,0.04075,0.03840,0.0232,0.0017,1.0000 13.250,1.1499,0.04722,0.04512,0.0231,0.0017,1.0000 13.500,1.0185,0.08114,0.07931,-0.0025,0.0021,1.0000 13.750,0.9106,0.10708,0.10534,-0.0183,0.0025,1.0000