Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e297-il-200000-n5 Airfoil,e297-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,39.5758 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-e297-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.750,-0.7035,0.10102,0.09765,-0.0079,1.0000,0.0060 -12.500,-0.7336,0.08659,0.08314,-0.0164,1.0000,0.0058 -12.250,-0.7545,0.07657,0.07300,-0.0236,1.0000,0.0057 -12.000,-0.7757,0.06843,0.06470,-0.0294,1.0000,0.0056 -11.750,-0.7968,0.06178,0.05786,-0.0333,1.0000,0.0056 -11.500,-0.8140,0.05667,0.05256,-0.0354,1.0000,0.0055 -11.250,-0.8308,0.05218,0.04785,-0.0361,1.0000,0.0055 -11.000,-0.8481,0.04796,0.04337,-0.0357,1.0000,0.0055 -10.750,-0.8600,0.04457,0.03972,-0.0344,1.0000,0.0055 -10.500,-0.8691,0.04153,0.03641,-0.0325,1.0000,0.0055 -10.250,-0.8746,0.03884,0.03344,-0.0301,1.0000,0.0055 -10.000,-0.8773,0.03625,0.03055,-0.0274,1.0000,0.0056 -9.750,-0.8746,0.03391,0.02792,-0.0249,1.0000,0.0057 -9.500,-0.8670,0.03153,0.02522,-0.0229,1.0000,0.0059 -9.250,-0.8554,0.02953,0.02297,-0.0213,1.0000,0.0060 -9.000,-0.8420,0.02768,0.02083,-0.0197,1.0000,0.0062 -8.750,-0.8271,0.02608,0.01902,-0.0182,1.0000,0.0065 -8.500,-0.8141,0.02435,0.01713,-0.0165,1.0000,0.0069 -8.250,-0.8012,0.02294,0.01560,-0.0148,1.0000,0.0074 -8.000,-0.7866,0.02198,0.01457,-0.0131,1.0000,0.0084 -7.750,-0.7663,0.02113,0.01363,-0.0126,0.9930,0.0098 -7.500,-0.7386,0.02005,0.01241,-0.0135,0.9809,0.0126 -7.250,-0.7117,0.01893,0.01121,-0.0143,0.9708,0.0166 -7.000,-0.6847,0.01798,0.01020,-0.0149,0.9620,0.0232 -6.750,-0.6568,0.01719,0.00928,-0.0156,0.9547,0.0311 -6.500,-0.6316,0.01648,0.00853,-0.0157,0.9468,0.0413 -6.250,-0.6066,0.01574,0.00783,-0.0157,0.9403,0.0577 -6.000,-0.5834,0.01516,0.00726,-0.0153,0.9329,0.0777 -5.750,-0.5596,0.01456,0.00675,-0.0150,0.9272,0.1063 -5.500,-0.5383,0.01395,0.00630,-0.0143,0.9204,0.1467 -5.250,-0.5174,0.01330,0.00587,-0.0135,0.9148,0.2001 -5.000,-0.4972,0.01268,0.00549,-0.0126,0.9090,0.2601 -4.750,-0.4772,0.01209,0.00510,-0.0116,0.9033,0.3256 -4.500,-0.4569,0.01154,0.00480,-0.0104,0.8987,0.3934 -4.250,-0.4363,0.01107,0.00457,-0.0093,0.8931,0.4596 -4.000,-0.4149,0.01068,0.00441,-0.0082,0.8885,0.5230 -3.750,-0.3921,0.01042,0.00433,-0.0071,0.8844,0.5791 -3.500,-0.3679,0.01029,0.00433,-0.0063,0.8796,0.6241 -3.250,-0.3427,0.01027,0.00433,-0.0055,0.8754,0.6576 -3.000,-0.3169,0.01029,0.00435,-0.0048,0.8719,0.6838 -2.750,-0.2909,0.01034,0.00437,-0.0044,0.8670,0.7051 -2.500,-0.2648,0.01039,0.00438,-0.0039,0.8626,0.7227 -2.250,-0.2384,0.01045,0.00437,-0.0034,0.8590,0.7373 -2.000,-0.2121,0.01050,0.00439,-0.0030,0.8541,0.7500 -1.750,-0.1857,0.01055,0.00439,-0.0026,0.8495,0.7610 -1.500,-0.1591,0.01060,0.00441,-0.0021,0.8456,0.7701 -1.250,-0.1327,0.01064,0.00441,-0.0018,0.8404,0.7791 -1.000,-0.1062,0.01067,0.00442,-0.0014,0.8353,0.7876 -0.750,-0.0795,0.01069,0.00441,-0.0010,0.8312,0.7943 -0.500,-0.0531,0.01071,0.00443,-0.0008,0.8251,0.8018 -0.250,-0.0265,0.01072,0.00442,-0.0004,0.8198,0.8076 0.000,0.0000,0.01072,0.00443,0.0000,0.8141,0.8141 0.250,0.0265,0.01072,0.00442,0.0004,0.8076,0.8198 0.500,0.0531,0.01071,0.00443,0.0008,0.8018,0.8251 0.750,0.0795,0.01069,0.00441,0.0010,0.7943,0.8312 1.000,0.1063,0.01067,0.00441,0.0014,0.7876,0.8354 1.250,0.1327,0.01064,0.00441,0.0018,0.7792,0.8404 1.500,0.1591,0.01060,0.00441,0.0021,0.7701,0.8456 1.750,0.1857,0.01055,0.00439,0.0026,0.7610,0.8495 2.000,0.2121,0.01050,0.00438,0.0030,0.7500,0.8541 2.250,0.2385,0.01045,0.00437,0.0034,0.7373,0.8590 2.500,0.2648,0.01039,0.00438,0.0039,0.7228,0.8627 2.750,0.2909,0.01034,0.00437,0.0044,0.7051,0.8670 3.000,0.3170,0.01029,0.00435,0.0048,0.6838,0.8719 3.250,0.3428,0.01027,0.00433,0.0055,0.6575,0.8754 3.500,0.3680,0.01029,0.00433,0.0062,0.6239,0.8796 3.750,0.3922,0.01042,0.00433,0.0071,0.5787,0.8845 4.000,0.4151,0.01067,0.00441,0.0081,0.5232,0.8886 4.250,0.4365,0.01107,0.00457,0.0093,0.4597,0.8932 4.500,0.4571,0.01155,0.00480,0.0104,0.3928,0.8987 4.750,0.4774,0.01209,0.00510,0.0115,0.3249,0.9034 5.000,0.4975,0.01268,0.00549,0.0125,0.2596,0.9089 5.250,0.5178,0.01331,0.00587,0.0134,0.1996,0.9148 5.500,0.5388,0.01395,0.00630,0.0142,0.1463,0.9204 5.750,0.5601,0.01457,0.00675,0.0149,0.1058,0.9272 6.000,0.5839,0.01516,0.00727,0.0152,0.0776,0.9329 6.250,0.6072,0.01575,0.00784,0.0156,0.0575,0.9403 6.500,0.6323,0.01649,0.00853,0.0155,0.0413,0.9468 6.750,0.6574,0.01720,0.00928,0.0155,0.0309,0.9547 7.000,0.6854,0.01798,0.01020,0.0148,0.0230,0.9621 7.250,0.7125,0.01893,0.01121,0.0141,0.0166,0.9709 7.500,0.7395,0.02003,0.01240,0.0134,0.0128,0.9812 8.000,0.7875,0.02193,0.01450,0.0130,0.0082,1.0000 8.250,0.8019,0.02296,0.01562,0.0146,0.0073,1.0000 8.500,0.8131,0.02469,0.01749,0.0166,0.0067,1.0000 8.750,0.8283,0.02612,0.01906,0.0180,0.0065,1.0000 9.000,0.8433,0.02777,0.02093,0.0195,0.0062,1.0000 9.250,0.8568,0.02963,0.02309,0.0210,0.0059,1.0000 9.500,0.8684,0.03164,0.02535,0.0226,0.0058,1.0000 9.750,0.8763,0.03397,0.02799,0.0246,0.0057,1.0000 10.000,0.8787,0.03641,0.03073,0.0271,0.0056,1.0000 10.250,0.8774,0.03879,0.03338,0.0297,0.0056,1.0000 10.500,0.8709,0.04161,0.03650,0.0321,0.0055,1.0000 10.750,0.8598,0.04491,0.04009,0.0342,0.0055,1.0000 11.000,0.8484,0.04824,0.04367,0.0354,0.0055,1.0000 11.250,0.8323,0.05232,0.04799,0.0357,0.0055,1.0000 11.500,0.8145,0.05696,0.05287,0.0349,0.0055,1.0000 11.750,0.7984,0.06193,0.05801,0.0329,0.0056,1.0000 12.000,0.7770,0.06865,0.06492,0.0289,0.0057,1.0000 12.250,0.7571,0.07654,0.07297,0.0233,0.0057,1.0000 12.500,0.7339,0.08726,0.08383,0.0156,0.0058,1.0000 12.750,0.7061,0.10102,0.09765,0.0075,0.0060,1.0000