Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ah85l120-il-1000000 Airfoil,ah85l120-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,55.391 Max Cl/Cd alpha,3.25 Url,http://www.airfoiltools.com/polar/csv?polar=xf-ah85l120-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.250,-0.7329,0.07178,0.07011,-0.0404,0.9523,0.0070 -12.000,-0.9171,0.03812,0.03497,-0.0494,0.9359,0.0056 -11.750,-0.9101,0.03542,0.03203,-0.0504,0.9301,0.0057 -11.250,-0.8779,0.03373,0.03018,-0.0517,0.9206,0.0061 -11.000,-0.8571,0.03347,0.02988,-0.0525,0.9168,0.0064 -10.750,-0.8600,0.02942,0.02541,-0.0504,0.9125,0.0066 -10.500,-0.8443,0.02881,0.02473,-0.0496,0.9092,0.0068 -10.250,-0.8374,0.02576,0.02132,-0.0476,0.9059,0.0068 -10.000,-0.8211,0.02470,0.02010,-0.0465,0.9030,0.0074 -9.750,-0.8043,0.02320,0.01841,-0.0456,0.9003,0.0073 -9.500,-0.7886,0.02259,0.01767,-0.0439,0.8976,0.0078 -9.250,-0.7711,0.02332,0.01836,-0.0422,0.8949,0.0082 -9.000,-0.7517,0.02061,0.01541,-0.0416,0.8931,0.0081 -8.750,-0.7269,0.01778,0.01231,-0.0421,0.8918,0.0088 -8.500,-0.7061,0.01670,0.01113,-0.0413,0.8898,0.0090 -8.250,-0.6872,0.01557,0.00990,-0.0402,0.8875,0.0092 -8.000,-0.6683,0.01510,0.00938,-0.0390,0.8855,0.0095 -7.750,-0.6480,0.01492,0.00921,-0.0379,0.8836,0.0105 -7.500,-0.6317,0.01418,0.00839,-0.0360,0.8814,0.0105 -7.250,-0.6156,0.01356,0.00769,-0.0340,0.8792,0.0108 -7.000,-0.5959,0.01318,0.00726,-0.0327,0.8772,0.0116 -6.750,-0.5753,0.01284,0.00687,-0.0316,0.8753,0.0121 -6.500,-0.5532,0.01260,0.00660,-0.0307,0.8734,0.0125 -6.250,-0.5398,0.01183,0.00572,-0.0281,0.8714,0.0131 -6.000,-0.5227,0.01128,0.00509,-0.0262,0.8693,0.0142 -5.750,-0.5020,0.01096,0.00476,-0.0250,0.8674,0.0158 -5.500,-0.4805,0.01067,0.00444,-0.0239,0.8655,0.0177 -5.250,-0.4597,0.01032,0.00405,-0.0227,0.8635,0.0229 -5.000,-0.4373,0.01008,0.00380,-0.0218,0.8618,0.0273 -4.750,-0.4184,0.00964,0.00350,-0.0203,0.8598,0.0593 -4.500,-0.4014,0.00914,0.00325,-0.0185,0.8578,0.1173 -4.250,-0.3855,0.00856,0.00299,-0.0164,0.8557,0.1901 -4.000,-0.3707,0.00795,0.00274,-0.0142,0.8532,0.2787 -3.750,-0.3554,0.00737,0.00250,-0.0121,0.8508,0.3675 -3.500,-0.3476,0.00650,0.00221,-0.0084,0.8483,0.5140 -3.250,-0.3324,0.00603,0.00203,-0.0059,0.8461,0.5982 -3.000,-0.3142,0.00574,0.00196,-0.0040,0.8438,0.6594 -2.750,-0.2950,0.00553,0.00196,-0.0021,0.8414,0.7179 -2.500,-0.2712,0.00550,0.00199,-0.0012,0.8389,0.7473 -2.250,-0.2449,0.00550,0.00197,-0.0009,0.8366,0.7601 -2.000,-0.2182,0.00553,0.00199,-0.0007,0.8346,0.7711 -1.750,-0.1907,0.00555,0.00200,-0.0006,0.8328,0.7780 -1.500,-0.1636,0.00562,0.00203,-0.0005,0.8308,0.7852 -1.250,-0.1370,0.00565,0.00208,-0.0003,0.8286,0.7919 -1.000,-0.1101,0.00569,0.00212,-0.0001,0.8260,0.7977 -0.750,-0.0834,0.00572,0.00214,0.0001,0.8234,0.8036 -0.500,-0.0551,0.00577,0.00220,0.0000,0.8209,0.8085 -0.250,-0.0272,0.00580,0.00221,-0.0001,0.8185,0.8126 0.000,0.0000,0.00584,0.00222,0.0000,0.8158,0.8159 0.250,0.0272,0.00579,0.00221,0.0001,0.8124,0.8186 0.500,0.0552,0.00576,0.00219,0.0000,0.8083,0.8209 0.750,0.0834,0.00572,0.00213,-0.0001,0.8034,0.8234 1.000,0.1102,0.00569,0.00212,0.0001,0.7978,0.8260 1.250,0.1370,0.00565,0.00207,0.0003,0.7918,0.8286 1.500,0.1637,0.00563,0.00204,0.0005,0.7855,0.8308 1.750,0.1908,0.00555,0.00200,0.0006,0.7781,0.8328 2.000,0.2182,0.00553,0.00199,0.0007,0.7711,0.8346 2.250,0.2450,0.00551,0.00198,0.0009,0.7605,0.8367 2.500,0.2714,0.00550,0.00200,0.0012,0.7483,0.8389 2.750,0.2963,0.00552,0.00199,0.0018,0.7253,0.8414 3.000,0.3157,0.00570,0.00196,0.0037,0.6682,0.8438 3.250,0.3329,0.00601,0.00203,0.0058,0.6017,0.8460 3.500,0.3477,0.00649,0.00221,0.0083,0.5143,0.8482 3.750,0.3598,0.00716,0.00245,0.0113,0.4024,0.8506 4.000,0.3728,0.00785,0.00272,0.0139,0.2955,0.8531 4.250,0.3864,0.00852,0.00298,0.0163,0.1976,0.8556 4.500,0.4024,0.00908,0.00323,0.0183,0.1243,0.8578 4.750,0.4186,0.00963,0.00351,0.0202,0.0615,0.8598 5.000,0.4377,0.01005,0.00378,0.0217,0.0301,0.8617 5.250,0.4584,0.01040,0.00413,0.0230,0.0205,0.8636 5.500,0.4806,0.01066,0.00442,0.0239,0.0180,0.8655 5.750,0.5023,0.01094,0.00474,0.0250,0.0162,0.8674 6.000,0.5229,0.01127,0.00507,0.0262,0.0140,0.8693 6.250,0.5352,0.01211,0.00605,0.0291,0.0126,0.8716 6.500,0.5570,0.01234,0.00629,0.0300,0.0123,0.8732 6.750,0.5781,0.01263,0.00664,0.0310,0.0118,0.8751 7.000,0.5984,0.01299,0.00705,0.0323,0.0107,0.8771 7.250,0.6143,0.01365,0.00779,0.0343,0.0110,0.8793 7.500,0.6318,0.01414,0.00834,0.0360,0.0104,0.8815 7.750,0.6490,0.01473,0.00900,0.0377,0.0103,0.8835 8.000,0.6662,0.01544,0.00975,0.0394,0.0095,0.8856 8.250,0.6846,0.01597,0.01029,0.0406,0.0088,0.8875 8.500,0.7051,0.01698,0.01142,0.0414,0.0087,0.8898 8.750,0.7315,0.01960,0.01425,0.0408,0.0084,0.8911 9.000,0.7533,0.02206,0.01694,0.0412,0.0083,0.8928 9.250,0.7705,0.02145,0.01637,0.0427,0.0079,0.8953 9.500,0.7866,0.02447,0.01970,0.0438,0.0081,0.8975 9.750,0.8033,0.02440,0.01973,0.0455,0.0076,0.9002 10.000,0.8154,0.02670,0.02231,0.0472,0.0075,0.9030 10.250,0.8278,0.02828,0.02412,0.0488,0.0071,0.9061 10.500,0.8238,0.03252,0.02880,0.0521,0.0071,0.9102 10.750,0.8421,0.03251,0.02882,0.0524,0.0066,0.9134 11.000,0.8131,0.04026,0.03722,0.0556,0.0072,0.9192 11.250,0.8055,0.04451,0.04178,0.0560,0.0068,0.9247 11.500,0.7909,0.04963,0.04720,0.0555,0.0068,0.9309 11.750,0.7550,0.05816,0.05608,0.0519,0.0075,0.9380 12.000,0.6282,0.04097,0.03881,0.0654,0.0078,0.9301 12.250,0.7288,0.07268,0.07102,0.0392,0.0073,0.9532 12.750,0.5869,0.05852,0.05676,0.0562,0.0072,0.9401 13.000,0.5657,0.06682,0.06516,0.0510,0.0074,0.9425 13.250,0.6457,0.12613,0.12462,0.0052,0.0090,1.0000 13.500,0.6348,0.13516,0.13363,0.0013,0.0093,1.0000 13.750,0.6449,0.13601,0.13449,0.0005,0.0088,1.0000 14.000,0.6433,0.14210,0.14057,-0.0023,0.0089,1.0000 14.250,0.3907,0.11792,0.11629,0.0319,0.0123,0.9348