Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca16015-il-50000-n5 Airfoil,naca16015-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,21.7105 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-naca16015-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.000,-0.6371,0.10993,0.10246,-0.0545,1.0000,0.0575 -12.750,-0.6654,0.10178,0.09433,-0.0578,1.0000,0.0566 -12.500,-0.6978,0.09470,0.08721,-0.0596,1.0000,0.0556 -12.250,-0.7324,0.08873,0.08117,-0.0595,1.0000,0.0547 -12.000,-0.7666,0.08385,0.07617,-0.0575,1.0000,0.0541 -11.750,-0.7984,0.07984,0.07203,-0.0542,1.0000,0.0538 -11.500,-0.8278,0.07650,0.06854,-0.0497,1.0000,0.0536 -11.250,-0.8549,0.07367,0.06554,-0.0445,1.0000,0.0536 -11.000,-0.8799,0.07123,0.06294,-0.0386,1.0000,0.0538 -10.750,-0.9035,0.06911,0.06066,-0.0322,1.0000,0.0541 -10.500,-0.9252,0.06714,0.05851,-0.0255,1.0000,0.0545 -10.250,-0.9418,0.06490,0.05605,-0.0195,1.0000,0.0554 -10.000,-0.9557,0.06257,0.05345,-0.0137,1.0000,0.0564 -9.750,-0.9671,0.06012,0.05068,-0.0080,1.0000,0.0576 -9.500,-0.9754,0.05759,0.04775,-0.0026,1.0000,0.0589 -9.250,-0.9793,0.05499,0.04469,0.0024,1.0000,0.0601 -9.000,-0.9789,0.05249,0.04166,0.0069,1.0000,0.0613 -8.750,-0.9674,0.05037,0.03955,0.0089,1.0000,0.0638 -8.500,-0.9575,0.04872,0.03769,0.0115,1.0000,0.0669 -8.250,-0.9439,0.04675,0.03538,0.0138,1.0000,0.0700 -8.000,-0.9246,0.04472,0.03287,0.0153,1.0000,0.0730 -7.750,-0.9030,0.04301,0.03108,0.0159,1.0000,0.0773 -7.500,-0.8790,0.04156,0.02947,0.0163,1.0000,0.0821 -7.250,-0.8417,0.03998,0.02752,0.0147,1.0000,0.0872 -7.000,-0.8091,0.03869,0.02628,0.0134,1.0000,0.0944 -6.750,-0.7695,0.03759,0.02498,0.0112,1.0000,0.1032 -6.500,-0.7337,0.03652,0.02386,0.0095,1.0000,0.1126 -6.250,-0.7120,0.03557,0.02291,0.0104,1.0000,0.1241 -6.000,-0.6969,0.03465,0.02200,0.0123,1.0000,0.1404 -5.750,-0.6852,0.03367,0.02112,0.0149,1.0000,0.1622 -5.500,-0.6779,0.03253,0.02025,0.0182,1.0000,0.1958 -5.250,-0.6764,0.03118,0.01940,0.0224,1.0000,0.2611 -5.000,-0.5834,0.03274,0.02350,0.0157,1.0000,0.7235 -4.750,-0.5775,0.03344,0.02403,0.0211,1.0000,0.7734 -4.500,-0.5463,0.03518,0.02548,0.0226,1.0000,0.8141 -4.250,-0.5025,0.03714,0.02711,0.0216,1.0000,0.8506 -4.000,-0.4340,0.03928,0.02887,0.0157,1.0000,0.8843 -3.750,-0.3940,0.04000,0.02929,0.0135,1.0000,0.9060 -3.500,-0.3560,0.04014,0.02920,0.0109,1.0000,0.9186 -3.000,-0.2920,0.03996,0.02863,0.0074,1.0000,0.9381 -2.750,-0.2647,0.03985,0.02835,0.0063,1.0000,0.9475 -2.500,-0.2334,0.03964,0.02800,0.0045,1.0000,0.9548 -2.250,-0.2075,0.03953,0.02776,0.0037,1.0000,0.9633 -2.000,-0.1769,0.03932,0.02744,0.0018,1.0000,0.9699 -1.750,-0.1487,0.03918,0.02720,0.0004,1.0000,0.9768 -1.500,-0.1199,0.03905,0.02698,-0.0011,1.0000,0.9834 -1.250,-0.0900,0.03888,0.02675,-0.0030,1.0000,0.9890 -1.000,-0.0601,0.03881,0.02661,-0.0048,1.0000,0.9949 -0.750,-0.0297,0.03871,0.02647,-0.0068,1.0000,1.0000 -0.500,-0.0198,0.03865,0.02639,-0.0045,1.0000,1.0000 -0.250,-0.0099,0.03861,0.02634,-0.0023,1.0000,1.0000 0.000,0.0000,0.03859,0.02632,0.0000,1.0000,1.0000 0.250,0.0099,0.03860,0.02633,0.0023,1.0000,1.0000 0.500,0.0198,0.03864,0.02639,0.0045,1.0000,1.0000 0.750,0.0297,0.03871,0.02647,0.0068,1.0000,1.0000 1.000,0.0600,0.03880,0.02660,0.0048,0.9949,1.0000 1.250,0.0899,0.03887,0.02674,0.0030,0.9891,1.0000 1.500,0.1198,0.03904,0.02697,0.0012,0.9834,1.0000 1.750,0.1486,0.03916,0.02718,-0.0004,0.9768,1.0000 2.000,0.1768,0.03931,0.02743,-0.0018,0.9700,1.0000 2.250,0.2074,0.03951,0.02774,-0.0036,0.9633,1.0000 2.500,0.2333,0.03962,0.02797,-0.0044,0.9549,1.0000 2.750,0.2647,0.03983,0.02833,-0.0063,0.9476,1.0000 3.000,0.2919,0.03994,0.02860,-0.0073,0.9382,1.0000 3.500,0.3561,0.04012,0.02918,-0.0109,0.9188,1.0000 3.750,0.3936,0.03997,0.02927,-0.0134,0.9060,1.0000 4.000,0.4339,0.03926,0.02884,-0.0157,0.8844,1.0000 4.250,0.5022,0.03713,0.02709,-0.0215,0.8507,1.0000 4.500,0.5464,0.03515,0.02546,-0.0226,0.8142,1.0000 4.750,0.5776,0.03341,0.02400,-0.0211,0.7735,1.0000 5.000,0.5835,0.03272,0.02348,-0.0157,0.7235,1.0000 5.250,0.6765,0.03116,0.01939,-0.0225,0.2610,1.0000 5.500,0.6780,0.03252,0.02023,-0.0182,0.1958,1.0000 5.750,0.6853,0.03365,0.02110,-0.0149,0.1622,1.0000 6.000,0.6970,0.03464,0.02199,-0.0123,0.1403,1.0000 6.250,0.7122,0.03556,0.02289,-0.0104,0.1241,1.0000 6.500,0.7339,0.03651,0.02385,-0.0096,0.1126,1.0000 6.750,0.7696,0.03757,0.02496,-0.0113,0.1032,1.0000 7.000,0.8092,0.03868,0.02626,-0.0134,0.0944,1.0000 7.250,0.8417,0.03996,0.02750,-0.0147,0.0872,1.0000 7.500,0.8790,0.04154,0.02945,-0.0163,0.0821,1.0000 7.750,0.9029,0.04299,0.03106,-0.0159,0.0773,1.0000 8.000,0.9245,0.04471,0.03285,-0.0153,0.0730,1.0000 8.250,0.9438,0.04674,0.03537,-0.0138,0.0700,1.0000 8.500,0.9574,0.04869,0.03766,-0.0115,0.0669,1.0000 8.750,0.9674,0.05036,0.03954,-0.0089,0.0638,1.0000 9.000,0.9789,0.05247,0.04164,-0.0069,0.0613,1.0000 9.250,0.9793,0.05497,0.04467,-0.0024,0.0601,1.0000 9.500,0.9754,0.05757,0.04774,0.0026,0.0589,1.0000 9.750,0.9672,0.06011,0.05067,0.0080,0.0577,1.0000 10.000,0.9558,0.06256,0.05344,0.0137,0.0565,1.0000 10.250,0.9420,0.06490,0.05605,0.0195,0.0554,1.0000 10.500,0.9254,0.06713,0.05850,0.0255,0.0546,1.0000 10.750,0.9038,0.06911,0.06065,0.0322,0.0540,1.0000 11.000,0.8802,0.07123,0.06293,0.0386,0.0537,1.0000 11.250,0.8552,0.07365,0.06552,0.0445,0.0536,1.0000 11.500,0.8281,0.07650,0.06853,0.0497,0.0536,1.0000 11.750,0.7988,0.07982,0.07201,0.0542,0.0537,1.0000 12.000,0.7670,0.08383,0.07615,0.0575,0.0541,1.0000 12.250,0.7329,0.08870,0.08114,0.0594,0.0547,1.0000 12.500,0.6982,0.09467,0.08719,0.0596,0.0556,1.0000 12.750,0.6659,0.10176,0.09430,0.0578,0.0566,1.0000 13.000,0.6377,0.10991,0.10244,0.0545,0.0575,1.0000