Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ames01-il-100000 Airfoil,ames01-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,35.0047 Max Cl/Cd alpha,10 Url,http://airfoiltools.com/polar/csv?polar=xf-ames01-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.4401,0.09033,0.08590,-0.0089,1.0000,0.1356 -8.750,-0.4731,0.08491,0.08056,-0.0152,1.0000,0.1405 -8.500,-0.5197,0.07852,0.07419,-0.0231,1.0000,0.1412 -8.250,-0.5787,0.08546,0.08094,-0.0081,1.0000,0.1343 -8.000,-0.6169,0.07953,0.07483,-0.0186,1.0000,0.1409 -7.750,-0.5968,0.07514,0.07057,-0.0163,1.0000,0.1451 -7.500,-0.5930,0.07166,0.06702,-0.0177,1.0000,0.1538 -7.250,-0.5892,0.06735,0.06268,-0.0185,1.0000,0.1610 -7.000,-0.5916,0.06355,0.05869,-0.0201,1.0000,0.1738 -6.750,-0.5874,0.06075,0.05574,-0.0200,1.0000,0.1881 -6.250,-0.5672,0.05549,0.05057,-0.0166,1.0000,0.2196 -6.000,-0.5594,0.05331,0.04844,-0.0139,1.0000,0.2362 -5.750,-0.5580,0.04005,0.03297,-0.0146,1.0000,0.1131 -5.500,-0.5421,0.03594,0.02818,-0.0117,1.0000,0.0950 -5.250,-0.5269,0.03325,0.02522,-0.0097,1.0000,0.0937 -5.000,-0.5101,0.03126,0.02285,-0.0077,1.0000,0.0944 -4.750,-0.4916,0.02927,0.02051,-0.0059,1.0000,0.0945 -4.500,-0.4714,0.02748,0.01840,-0.0044,1.0000,0.0947 -4.250,-0.4507,0.02650,0.01702,-0.0027,1.0000,0.0967 -4.000,-0.4288,0.02439,0.01492,-0.0020,1.0000,0.1004 -3.750,-0.4059,0.02321,0.01365,-0.0010,1.0000,0.1032 -3.500,-0.3825,0.02222,0.01253,-0.0001,1.0000,0.1069 -3.250,-0.3591,0.02140,0.01158,0.0009,1.0000,0.1125 -3.000,-0.3355,0.02040,0.01070,0.0015,1.0000,0.1186 -2.750,-0.3117,0.01977,0.01003,0.0023,1.0000,0.1253 -2.500,-0.2889,0.01898,0.00940,0.0029,1.0000,0.1357 -2.250,-0.2663,0.01834,0.00886,0.0037,1.0000,0.1475 -2.000,-0.2435,0.01775,0.00839,0.0044,1.0000,0.1679 -1.750,-0.2207,0.01516,0.00801,0.0048,1.0000,0.5620 -1.500,-0.0949,0.01537,0.00904,-0.0096,1.0000,1.0000 -1.250,-0.0898,0.01539,0.00892,-0.0065,1.0000,1.0000 -1.000,-0.0814,0.01547,0.00887,-0.0037,1.0000,1.0000 -0.750,-0.0427,0.01565,0.00889,-0.0067,0.9945,1.0000 -0.500,0.0250,0.01582,0.00889,-0.0149,0.9820,1.0000 -0.250,0.0873,0.01592,0.00888,-0.0220,0.9720,1.0000 0.000,0.1490,0.01591,0.00880,-0.0287,0.9610,1.0000 0.250,0.2083,0.01582,0.00868,-0.0348,0.9487,1.0000 0.500,0.2587,0.01569,0.00854,-0.0387,0.9341,1.0000 0.750,0.2967,0.01556,0.00840,-0.0399,0.9168,1.0000 1.000,0.3207,0.01545,0.00830,-0.0383,0.8960,1.0000 1.250,0.3425,0.01524,0.00808,-0.0358,0.8756,1.0000 1.500,0.3603,0.01497,0.00781,-0.0325,0.8525,1.0000 1.750,0.3771,0.01455,0.00738,-0.0287,0.8278,1.0000 2.000,0.3935,0.01411,0.00692,-0.0249,0.7943,1.0000 2.250,0.4102,0.01365,0.00639,-0.0211,0.7422,1.0000 2.500,0.4250,0.01331,0.00564,-0.0163,0.6374,1.0000 2.750,0.4417,0.01396,0.00537,-0.0131,0.5070,1.0000 3.000,0.4637,0.01472,0.00560,-0.0119,0.4499,1.0000 3.250,0.4873,0.01534,0.00592,-0.0111,0.4199,1.0000 3.500,0.5114,0.01593,0.00628,-0.0104,0.3993,1.0000 3.750,0.5360,0.01648,0.00668,-0.0098,0.3827,1.0000 4.000,0.5607,0.01707,0.00712,-0.0093,0.3698,1.0000 4.250,0.5859,0.01762,0.00762,-0.0088,0.3580,1.0000 4.500,0.6111,0.01819,0.00817,-0.0083,0.3473,1.0000 4.750,0.6362,0.01885,0.00872,-0.0079,0.3380,1.0000 5.000,0.6616,0.01944,0.00936,-0.0075,0.3290,1.0000 5.250,0.6871,0.02015,0.01005,-0.0071,0.3209,1.0000 5.500,0.7124,0.02080,0.01072,-0.0067,0.3124,1.0000 5.750,0.7378,0.02157,0.01155,-0.0064,0.3049,1.0000 6.000,0.7631,0.02227,0.01230,-0.0061,0.2970,1.0000 6.250,0.7882,0.02310,0.01321,-0.0057,0.2895,1.0000 6.500,0.8132,0.02384,0.01401,-0.0054,0.2815,1.0000 6.750,0.8379,0.02473,0.01504,-0.0050,0.2739,1.0000 7.000,0.8627,0.02549,0.01585,-0.0047,0.2657,1.0000 7.250,0.8865,0.02643,0.01698,-0.0043,0.2574,1.0000 7.500,0.9112,0.02718,0.01772,-0.0039,0.2491,1.0000 7.750,0.9339,0.02808,0.01888,-0.0033,0.2395,1.0000 8.000,0.9579,0.02887,0.01964,-0.0029,0.2308,1.0000 8.250,0.9804,0.02950,0.02045,-0.0023,0.2203,1.0000 8.500,1.0020,0.03036,0.02152,-0.0016,0.2099,1.0000 8.750,1.0251,0.03083,0.02196,-0.0011,0.1997,1.0000 9.000,1.0474,0.03106,0.02223,-0.0004,0.1882,1.0000 9.250,1.0672,0.03138,0.02274,0.0006,0.1755,1.0000 9.500,1.0868,0.03164,0.02314,0.0016,0.1627,1.0000 9.750,1.1057,0.03182,0.02339,0.0028,0.1496,1.0000 10.000,1.1233,0.03209,0.02372,0.0040,0.1363,1.0000 10.250,1.1394,0.03269,0.02437,0.0054,0.1234,1.0000 10.500,1.1540,0.03366,0.02540,0.0068,0.1116,1.0000 10.750,1.1675,0.03485,0.02662,0.0083,0.1016,1.0000 11.000,1.1831,0.03620,0.02778,0.0095,0.0933,1.0000 11.250,1.1909,0.03821,0.03023,0.0115,0.0867,1.0000 11.500,1.2052,0.04002,0.03186,0.0126,0.0809,1.0000 11.750,1.2077,0.04234,0.03463,0.0149,0.0768,1.0000 12.000,1.2146,0.04444,0.03687,0.0166,0.0732,1.0000 12.250,1.2290,0.04736,0.03968,0.0173,0.0699,1.0000 12.500,1.2194,0.05021,0.04294,0.0202,0.0687,1.0000 12.750,1.2049,0.05334,0.04642,0.0229,0.0677,1.0000 13.000,1.1876,0.05701,0.05041,0.0247,0.0669,1.0000 13.250,1.1668,0.06136,0.05507,0.0254,0.0664,1.0000 13.500,1.1410,0.06675,0.06074,0.0246,0.0664,1.0000 13.750,1.1086,0.07378,0.06804,0.0219,0.0669,1.0000 14.000,1.0703,0.08298,0.07747,0.0165,0.0680,1.0000 14.250,1.0283,0.09451,0.08916,0.0091,0.0692,1.0000 14.500,0.8172,0.15803,0.15248,-0.0285,0.0927,1.0000 14.750,0.8212,0.16329,0.15775,-0.0298,0.0931,1.0000