Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca652415-il-200000 Airfoil,naca652415-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,70.8128 Max Cl/Cd alpha,6.75 Url,http://airfoiltools.com/polar/csv?polar=xf-naca652415-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.4881,0.08509,0.08159,-0.0726,1.0000,0.0726 -10.750,-0.5231,0.08247,0.07904,-0.0705,1.0000,0.0726 -10.500,-0.5499,0.08157,0.07822,-0.0653,1.0000,0.0724 -10.250,-0.5821,0.07572,0.07212,-0.0739,0.9887,0.0727 -10.000,-0.5975,0.07221,0.06819,-0.0789,0.9759,0.0732 -9.750,-0.5610,0.06378,0.06015,-0.0808,0.9784,0.0761 -9.500,-0.5425,0.06022,0.05652,-0.0840,0.9731,0.0788 -9.250,-0.5387,0.05628,0.05231,-0.0872,0.9640,0.0828 -9.000,-0.4536,0.03772,0.03384,-0.0950,0.9499,0.0936 -8.500,-0.5226,0.03638,0.02985,-0.0891,0.9413,0.0508 -8.250,-0.5038,0.03275,0.02605,-0.0886,0.9335,0.0495 -8.000,-0.4770,0.03009,0.02307,-0.0893,0.9286,0.0494 -7.750,-0.4506,0.02868,0.02132,-0.0895,0.9233,0.0502 -7.500,-0.4285,0.02703,0.01940,-0.0887,0.9157,0.0508 -7.250,-0.3979,0.02468,0.01688,-0.0894,0.9117,0.0514 -7.000,-0.3708,0.02310,0.01525,-0.0895,0.9063,0.0524 -6.750,-0.3460,0.02207,0.01420,-0.0891,0.8997,0.0540 -6.500,-0.3181,0.02121,0.01329,-0.0892,0.8951,0.0564 -6.250,-0.2953,0.02050,0.01252,-0.0883,0.8881,0.0584 -6.000,-0.2708,0.01977,0.01172,-0.0877,0.8821,0.0600 -5.750,-0.2460,0.01887,0.01078,-0.0872,0.8779,0.0621 -5.500,-0.2294,0.01818,0.01016,-0.0856,0.8702,0.0656 -5.250,-0.2071,0.01764,0.00959,-0.0848,0.8647,0.0702 -5.000,-0.1863,0.01700,0.00891,-0.0839,0.8596,0.0753 -4.750,-0.1675,0.01648,0.00840,-0.0827,0.8525,0.0836 -4.500,-0.1465,0.01568,0.00770,-0.0819,0.8478,0.1078 -4.250,-0.1455,0.01308,0.00699,-0.0794,0.8413,0.4793 -4.000,-0.1232,0.01317,0.00736,-0.0780,0.8357,0.5981 -3.750,-0.0960,0.01338,0.00751,-0.0773,0.8318,0.6335 -3.500,-0.0697,0.01367,0.00777,-0.0765,0.8276,0.6546 -3.250,-0.0457,0.01399,0.00808,-0.0755,0.8218,0.6713 -3.000,-0.0205,0.01446,0.00854,-0.0742,0.8177,0.6938 -2.750,0.0026,0.01531,0.00947,-0.0712,0.8146,0.7189 -2.500,0.0239,0.01587,0.01005,-0.0690,0.8093,0.7338 -2.250,0.0488,0.01601,0.01015,-0.0683,0.8043,0.7409 -2.000,0.0772,0.01590,0.00993,-0.0687,0.8008,0.7475 -1.750,0.1054,0.01590,0.00987,-0.0685,0.7980,0.7512 -1.500,0.1289,0.01600,0.00995,-0.0681,0.7926,0.7558 -1.250,0.1567,0.01592,0.00978,-0.0687,0.7880,0.7617 -1.000,0.1847,0.01585,0.00966,-0.0687,0.7846,0.7650 -0.750,0.2135,0.01582,0.00959,-0.0688,0.7820,0.7685 -0.500,0.2369,0.01597,0.00974,-0.0685,0.7769,0.7732 -0.250,0.2649,0.01594,0.00966,-0.0692,0.7725,0.7786 0.000,0.2921,0.01591,0.00963,-0.0690,0.7692,0.7817 0.250,0.3210,0.01590,0.00959,-0.0692,0.7666,0.7854 0.500,0.3451,0.01607,0.00978,-0.0691,0.7620,0.7901 0.750,0.3717,0.01614,0.00985,-0.0694,0.7574,0.7954 1.000,0.3982,0.01616,0.00989,-0.0691,0.7540,0.7988 1.250,0.4271,0.01616,0.00988,-0.0694,0.7514,0.8030 1.500,0.4533,0.01632,0.01006,-0.0696,0.7476,0.8081 1.750,0.4765,0.01650,0.01030,-0.0692,0.7424,0.8129 2.000,0.5023,0.01658,0.01042,-0.0689,0.7389,0.8171 2.250,0.5318,0.01658,0.01044,-0.0693,0.7362,0.8222 2.500,0.5606,0.01667,0.01055,-0.0699,0.7329,0.8275 2.750,0.5789,0.01699,0.01098,-0.0685,0.7271,0.8320 3.000,0.6057,0.01704,0.01108,-0.0684,0.7231,0.8376 3.250,0.6375,0.01695,0.01101,-0.0692,0.7201,0.8434 3.500,0.6579,0.01714,0.01131,-0.0679,0.7145,0.8483 3.750,0.6824,0.01722,0.01146,-0.0675,0.7089,0.8544 4.000,0.7133,0.01706,0.01134,-0.0679,0.7050,0.8601 4.250,0.7359,0.01710,0.01148,-0.0668,0.6993,0.8660 4.500,0.7626,0.01697,0.01141,-0.0665,0.6919,0.8734 4.750,0.7926,0.01650,0.01098,-0.0662,0.6853,0.8785 5.000,0.8233,0.01563,0.01008,-0.0655,0.6715,0.8848 5.250,0.8450,0.01493,0.00939,-0.0635,0.6527,0.8923 5.500,0.8665,0.01448,0.00899,-0.0616,0.6371,0.9005 5.750,0.8886,0.01418,0.00873,-0.0601,0.6239,0.9088 6.000,0.9079,0.01396,0.00858,-0.0582,0.6082,0.9189 6.250,0.9220,0.01375,0.00847,-0.0553,0.5895,0.9298 6.500,0.9364,0.01353,0.00830,-0.0524,0.5648,0.9429 6.750,0.9496,0.01341,0.00818,-0.0495,0.5264,0.9592 7.000,0.9596,0.01400,0.00823,-0.0468,0.4117,0.9807 7.250,0.9453,0.01572,0.00920,-0.0415,0.2948,1.0000 7.500,0.9290,0.01808,0.01083,-0.0368,0.1821,1.0000 7.750,0.9173,0.02059,0.01268,-0.0331,0.0983,1.0000 8.000,0.9200,0.02235,0.01426,-0.0310,0.0746,1.0000 8.250,0.9281,0.02379,0.01567,-0.0294,0.0651,1.0000 8.500,0.9328,0.02548,0.01730,-0.0276,0.0598,1.0000 8.750,0.9451,0.02670,0.01858,-0.0264,0.0555,1.0000 9.000,0.9555,0.02806,0.01993,-0.0252,0.0521,1.0000 9.250,0.9639,0.02971,0.02153,-0.0237,0.0492,1.0000 9.500,0.9793,0.03085,0.02276,-0.0228,0.0469,1.0000 9.750,0.9955,0.03203,0.02396,-0.0219,0.0451,1.0000 10.000,1.0135,0.03321,0.02512,-0.0211,0.0434,1.0000 10.250,1.0415,0.03452,0.02633,-0.0210,0.0415,1.0000 10.500,1.0685,0.03575,0.02767,-0.0208,0.0400,1.0000 10.750,1.0927,0.03695,0.02900,-0.0206,0.0387,1.0000 11.000,1.1194,0.03834,0.03051,-0.0206,0.0375,1.0000 11.250,1.1482,0.03998,0.03227,-0.0208,0.0366,1.0000 11.500,1.1764,0.04186,0.03430,-0.0211,0.0359,1.0000 11.750,1.2026,0.04412,0.03674,-0.0212,0.0355,1.0000 12.000,1.2233,0.04663,0.03948,-0.0209,0.0353,1.0000 12.250,1.2393,0.04920,0.04221,-0.0204,0.0348,1.0000 12.500,1.2537,0.05231,0.04552,-0.0200,0.0343,1.0000 12.750,1.2610,0.05590,0.04935,-0.0189,0.0340,1.0000 13.000,1.2573,0.05866,0.05238,-0.0168,0.0342,1.0000 13.250,1.2409,0.06165,0.05576,-0.0139,0.0348,1.0000 13.500,1.1861,0.06866,0.06353,-0.0101,0.0369,1.0000 13.750,1.1632,0.07416,0.06934,-0.0091,0.0380,1.0000 14.000,1.1431,0.07958,0.07500,-0.0089,0.0390,1.0000 14.250,1.1248,0.08516,0.08076,-0.0093,0.0397,1.0000 14.500,0.9564,0.08962,0.08587,-0.0069,0.0388,1.0000 14.750,0.9181,0.09562,0.09210,-0.0093,0.0394,1.0000 15.000,0.8845,0.10238,0.09904,-0.0128,0.0399,1.0000 15.250,0.8898,0.10594,0.10262,-0.0134,0.0414,1.0000