Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-s1010-il-1000000 Airfoil,s1010-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,66.3078 Max Cl/Cd alpha,6 Url,http://www.airfoiltools.com/polar/csv?polar=xf-s1010-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.250,-0.9927,0.04542,0.04355,-0.0209,1.0000,0.0048 -11.000,-1.0265,0.03903,0.03682,-0.0196,1.0000,0.0047 -10.750,-1.0229,0.03626,0.03385,-0.0188,1.0000,0.0048 -10.500,-1.0266,0.03199,0.02921,-0.0174,1.0000,0.0048 -10.250,-1.0187,0.02916,0.02609,-0.0162,1.0000,0.0049 -10.000,-1.0058,0.02694,0.02362,-0.0152,1.0000,0.0050 -9.750,-0.9917,0.02474,0.02115,-0.0141,1.0000,0.0051 -9.500,-0.9745,0.02299,0.01916,-0.0131,1.0000,0.0052 -9.250,-0.9552,0.02156,0.01752,-0.0122,1.0000,0.0053 -9.000,-0.9349,0.02025,0.01601,-0.0114,1.0000,0.0054 -8.750,-0.9214,0.01725,0.01258,-0.0098,1.0000,0.0056 -8.500,-0.9013,0.01577,0.01092,-0.0088,1.0000,0.0062 -8.250,-0.8773,0.01515,0.01024,-0.0083,1.0000,0.0066 -8.000,-0.8529,0.01462,0.00965,-0.0078,1.0000,0.0072 -7.750,-0.8286,0.01401,0.00895,-0.0072,1.0000,0.0078 -7.500,-0.8040,0.01347,0.00833,-0.0067,1.0000,0.0083 -7.250,-0.7818,0.01232,0.00700,-0.0057,1.0000,0.0094 -7.000,-0.7575,0.01174,0.00637,-0.0051,1.0000,0.0107 -6.750,-0.7324,0.01135,0.00594,-0.0046,1.0000,0.0120 -6.500,-0.7070,0.01107,0.00562,-0.0041,1.0000,0.0129 -6.250,-0.6836,0.01032,0.00477,-0.0032,1.0000,0.0151 -6.000,-0.6589,0.00994,0.00438,-0.0026,1.0000,0.0172 -5.750,-0.6340,0.00967,0.00407,-0.0020,1.0000,0.0190 -5.500,-0.6098,0.00927,0.00361,-0.0012,1.0000,0.0213 -5.250,-0.5858,0.00888,0.00325,-0.0004,1.0000,0.0266 -5.000,-0.5617,0.00852,0.00293,0.0004,1.0000,0.0353 -4.750,-0.5377,0.00824,0.00269,0.0012,1.0000,0.0459 -4.500,-0.5135,0.00803,0.00249,0.0020,1.0000,0.0537 -4.250,-0.4896,0.00782,0.00230,0.0028,1.0000,0.0618 -4.000,-0.4659,0.00761,0.00212,0.0037,1.0000,0.0706 -3.750,-0.4424,0.00744,0.00197,0.0046,1.0000,0.0795 -3.500,-0.4192,0.00727,0.00184,0.0056,1.0000,0.0900 -3.250,-0.3964,0.00711,0.00172,0.0066,1.0000,0.1030 -3.000,-0.3718,0.00695,0.00162,0.0072,0.9997,0.1176 -2.750,-0.3380,0.00676,0.00152,0.0058,0.9979,0.1377 -2.500,-0.3006,0.00658,0.00143,0.0037,0.9953,0.1599 -2.250,-0.2578,0.00633,0.00131,0.0005,0.9900,0.1913 -2.000,-0.2131,0.00605,0.00118,-0.0032,0.9840,0.2319 -1.750,-0.1797,0.00578,0.00109,-0.0044,0.9756,0.2808 -1.500,-0.1479,0.00541,0.00099,-0.0054,0.9668,0.3581 -1.250,-0.1197,0.00499,0.00090,-0.0055,0.9554,0.4576 -1.000,-0.0955,0.00444,0.00081,-0.0047,0.9413,0.5959 -0.750,-0.0735,0.00393,0.00078,-0.0033,0.9255,0.7414 -0.500,-0.0497,0.00376,0.00079,-0.0021,0.9080,0.8078 -0.250,-0.0248,0.00371,0.00079,-0.0010,0.8898,0.8424 0.000,0.0000,0.00369,0.00079,0.0000,0.8690,0.8690 0.250,0.0249,0.00371,0.00079,0.0010,0.8424,0.8898 0.500,0.0498,0.00376,0.00079,0.0021,0.8082,0.9084 0.750,0.0735,0.00393,0.00078,0.0033,0.7411,0.9256 1.000,0.0955,0.00444,0.00081,0.0047,0.5950,0.9413 1.250,0.1198,0.00499,0.00090,0.0055,0.4571,0.9553 1.500,0.1480,0.00540,0.00099,0.0053,0.3599,0.9668 1.750,0.1798,0.00578,0.00109,0.0044,0.2808,0.9757 2.000,0.2131,0.00605,0.00118,0.0032,0.2319,0.9840 2.250,0.2579,0.00633,0.00131,-0.0005,0.1913,0.9900 2.500,0.3008,0.00658,0.00143,-0.0038,0.1600,0.9953 2.750,0.3381,0.00676,0.00152,-0.0059,0.1378,0.9979 3.000,0.3719,0.00695,0.00162,-0.0073,0.1174,0.9997 3.250,0.3964,0.00711,0.00172,-0.0066,0.1033,1.0000 3.500,0.4192,0.00727,0.00184,-0.0056,0.0902,1.0000 3.750,0.4424,0.00744,0.00197,-0.0046,0.0795,1.0000 4.000,0.4659,0.00761,0.00212,-0.0037,0.0707,1.0000 4.250,0.4896,0.00782,0.00230,-0.0028,0.0618,1.0000 4.500,0.5135,0.00803,0.00249,-0.0020,0.0537,1.0000 4.750,0.5377,0.00824,0.00269,-0.0012,0.0460,1.0000 5.000,0.5618,0.00852,0.00293,-0.0004,0.0353,1.0000 5.250,0.5858,0.00888,0.00325,0.0004,0.0265,1.0000 5.500,0.6099,0.00927,0.00361,0.0012,0.0214,1.0000 5.750,0.6341,0.00967,0.00407,0.0020,0.0190,1.0000 6.000,0.6591,0.00994,0.00438,0.0026,0.0173,1.0000 6.250,0.6837,0.01032,0.00477,0.0032,0.0151,1.0000 6.500,0.7071,0.01107,0.00562,0.0041,0.0129,1.0000 6.750,0.7325,0.01136,0.00595,0.0046,0.0120,1.0000 7.000,0.7576,0.01173,0.00636,0.0051,0.0107,1.0000 7.250,0.7819,0.01232,0.00700,0.0057,0.0094,1.0000 7.500,0.8037,0.01355,0.00841,0.0067,0.0084,1.0000 7.750,0.8287,0.01399,0.00893,0.0072,0.0078,1.0000 8.000,0.8529,0.01464,0.00967,0.0078,0.0073,1.0000 8.250,0.8774,0.01516,0.01025,0.0083,0.0066,1.0000 8.500,0.9014,0.01575,0.01090,0.0088,0.0062,1.0000 8.750,0.9218,0.01717,0.01250,0.0097,0.0057,1.0000 9.000,0.9350,0.02025,0.01600,0.0114,0.0054,1.0000 9.250,0.9555,0.02151,0.01747,0.0122,0.0053,1.0000 9.500,0.9752,0.02286,0.01901,0.0130,0.0052,1.0000 9.750,0.9916,0.02477,0.02117,0.0141,0.0051,1.0000 10.000,1.0069,0.02676,0.02341,0.0151,0.0050,1.0000 10.250,1.0184,0.02924,0.02617,0.0163,0.0049,1.0000 10.500,1.0268,0.03199,0.02921,0.0174,0.0048,1.0000 10.750,1.0236,0.03619,0.03377,0.0188,0.0048,1.0000 11.000,1.0146,0.04068,0.03857,0.0197,0.0048,1.0000 11.250,0.9919,0.04557,0.04370,0.0208,0.0048,1.0000 11.750,0.8393,0.08870,0.08709,-0.0099,0.0054,1.0000 12.000,0.8296,0.09517,0.09356,-0.0133,0.0055,1.0000