Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e332-il-500000 Airfoil,e332-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,95.6068 Max Cl/Cd alpha,8.5 Url,http://airfoiltools.com/polar/csv?polar=xf-e332-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.4068,0.08830,0.08619,-0.0158,1.0000,0.0138 -8.500,-0.4094,0.08383,0.08176,-0.0189,1.0000,0.0142 -8.250,-0.4126,0.07982,0.07778,-0.0218,1.0000,0.0140 -8.000,-0.4227,0.07538,0.07335,-0.0249,1.0000,0.0142 -7.750,-0.4327,0.07202,0.06999,-0.0248,1.0000,0.0142 -7.500,-0.4385,0.06758,0.06547,-0.0256,1.0000,0.0145 -7.250,-0.4385,0.06405,0.06188,-0.0251,1.0000,0.0146 -7.000,-0.4322,0.05988,0.05759,-0.0253,0.9925,0.0148 -6.750,-0.3919,0.05350,0.05088,-0.0328,0.9152,0.0149 -6.500,-0.3904,0.04821,0.04521,-0.0322,0.8475,0.0152 -6.250,-0.3834,0.04597,0.04272,-0.0304,0.8070,0.0155 -6.000,-0.3732,0.04396,0.04051,-0.0289,0.7773,0.0158 -5.750,-0.3610,0.04174,0.03807,-0.0273,0.7530,0.0162 -5.500,-0.3474,0.03944,0.03555,-0.0257,0.7322,0.0167 -5.250,-0.3322,0.03702,0.03288,-0.0239,0.7132,0.0175 -5.000,-0.3095,0.03494,0.03034,-0.0212,0.6968,0.0196 -4.750,-0.2921,0.03333,0.02833,-0.0190,0.6809,0.0198 -4.500,-0.2825,0.02866,0.02347,-0.0172,0.6674,0.0207 -4.250,-0.2631,0.02716,0.02184,-0.0162,0.6527,0.0215 -4.000,-0.2421,0.02576,0.02023,-0.0150,0.6389,0.0226 -3.750,-0.2155,0.02590,0.01998,-0.0132,0.6254,0.0260 -3.500,-0.1988,0.02220,0.01595,-0.0115,0.6139,0.0276 -3.250,-0.1754,0.02086,0.01452,-0.0107,0.6013,0.0291 -3.000,-0.1447,0.01622,0.00913,-0.0080,0.5919,0.0139 -2.750,-0.1165,0.01452,0.00703,-0.0069,0.5810,0.0113 -2.500,-0.0902,0.01365,0.00605,-0.0062,0.5698,0.0110 -2.250,-0.0654,0.01282,0.00512,-0.0054,0.5591,0.0110 -2.000,-0.0411,0.01225,0.00446,-0.0044,0.5491,0.0111 -1.750,-0.0185,0.01153,0.00368,-0.0032,0.5391,0.0118 -1.500,0.0062,0.01120,0.00329,-0.0024,0.5299,0.0131 -1.000,0.0546,0.01043,0.00256,-0.0005,0.5121,0.0513 -0.750,0.0657,0.00898,0.00233,0.0022,0.5050,0.4086 -0.500,0.0635,0.00763,0.00274,0.0094,0.4984,0.8951 -0.250,0.1099,0.00872,0.00373,0.0076,0.4892,0.9380 0.000,0.1797,0.00937,0.00418,-0.0004,0.4784,0.9492 0.250,0.2545,0.00998,0.00463,-0.0096,0.4674,0.9624 0.500,0.3165,0.01014,0.00462,-0.0165,0.4584,0.9690 0.750,0.3449,0.01020,0.00461,-0.0166,0.4510,0.9731 1.000,0.3742,0.01022,0.00453,-0.0171,0.4446,0.9755 1.250,0.4084,0.01014,0.00441,-0.0185,0.4374,0.9768 1.500,0.4405,0.01014,0.00432,-0.0196,0.4309,0.9784 1.750,0.4718,0.01011,0.00426,-0.0204,0.4245,0.9801 2.000,0.5012,0.01013,0.00422,-0.0209,0.4184,0.9821 2.250,0.5288,0.01017,0.00422,-0.0210,0.4127,0.9841 2.500,0.5548,0.01023,0.00426,-0.0208,0.4069,0.9862 2.750,0.5864,0.01023,0.00419,-0.0218,0.4012,0.9872 3.000,0.6178,0.01018,0.00415,-0.0227,0.3955,0.9883 3.250,0.6484,0.01019,0.00412,-0.0235,0.3900,0.9896 3.500,0.6773,0.01025,0.00415,-0.0239,0.3847,0.9909 3.750,0.7066,0.01025,0.00417,-0.0244,0.3791,0.9923 4.000,0.7348,0.01032,0.00420,-0.0247,0.3739,0.9936 4.250,0.7622,0.01039,0.00428,-0.0248,0.3687,0.9948 4.500,0.7922,0.01040,0.00432,-0.0255,0.3631,0.9958 4.750,0.8213,0.01048,0.00435,-0.0260,0.3578,0.9968 5.000,0.8498,0.01051,0.00443,-0.0264,0.3524,0.9976 5.250,0.8788,0.01055,0.00449,-0.0269,0.3467,0.9987 5.500,0.9078,0.01067,0.00458,-0.0274,0.3411,0.9997 5.750,0.9339,0.01071,0.00469,-0.0273,0.3354,1.0000 6.000,0.9571,0.01084,0.00483,-0.0266,0.3299,1.0000 6.250,0.9805,0.01097,0.00499,-0.0259,0.3243,1.0000 6.500,1.0039,0.01107,0.00513,-0.0252,0.3183,1.0000 6.750,1.0265,0.01124,0.00531,-0.0245,0.3124,1.0000 7.000,1.0499,0.01133,0.00547,-0.0238,0.3059,1.0000 7.500,1.0950,0.01163,0.00583,-0.0222,0.2922,1.0000 7.750,1.1166,0.01184,0.00605,-0.0213,0.2851,1.0000 8.000,1.1391,0.01196,0.00624,-0.0205,0.2766,1.0000 8.250,1.1603,0.01218,0.00648,-0.0195,0.2690,1.0000 8.500,1.1817,0.01236,0.00671,-0.0185,0.2601,1.0000 8.750,1.2025,0.01258,0.00698,-0.0175,0.2500,1.0000 9.000,1.2223,0.01286,0.00727,-0.0163,0.2401,1.0000 9.250,1.2411,0.01317,0.00759,-0.0150,0.2283,1.0000 9.750,1.2757,0.01394,0.00835,-0.0119,0.2014,1.0000 10.000,1.2909,0.01440,0.00882,-0.0100,0.1860,1.0000 10.250,1.3043,0.01493,0.00932,-0.0078,0.1705,1.0000 10.500,1.3156,0.01551,0.00987,-0.0053,0.1557,1.0000 10.750,1.3243,0.01614,0.01047,-0.0024,0.1413,1.0000 11.000,1.3301,0.01679,0.01109,0.0010,0.1278,1.0000 11.250,1.3326,0.01746,0.01173,0.0049,0.1153,1.0000 11.500,1.3326,0.01810,0.01236,0.0093,0.1054,1.0000 11.750,1.3303,0.01879,0.01304,0.0140,0.0963,1.0000 12.000,1.3242,0.01951,0.01376,0.0192,0.0884,1.0000 12.250,1.3238,0.02032,0.01460,0.0230,0.0813,1.0000 12.500,1.3226,0.02147,0.01575,0.0261,0.0736,1.0000 12.750,1.3223,0.02285,0.01716,0.0284,0.0672,1.0000 13.000,1.3225,0.02447,0.01883,0.0300,0.0611,1.0000 13.250,1.3192,0.02665,0.02103,0.0311,0.0556,1.0000 13.500,1.3196,0.02879,0.02325,0.0316,0.0510,1.0000 13.750,1.3155,0.03152,0.02603,0.0317,0.0470,1.0000 14.000,1.3115,0.03443,0.02902,0.0316,0.0431,1.0000 14.250,1.3071,0.03749,0.03215,0.0313,0.0399,1.0000 14.500,1.2961,0.04137,0.03608,0.0307,0.0370,1.0000 14.750,1.2899,0.04478,0.03960,0.0301,0.0345,1.0000 15.000,1.2820,0.04846,0.04334,0.0293,0.0319,1.0000 15.250,1.2708,0.05258,0.04753,0.0284,0.0305,1.0000 15.500,1.2548,0.05737,0.05238,0.0272,0.0283,1.0000 15.750,1.2493,0.06103,0.05618,0.0262,0.0270,1.0000 16.000,1.2406,0.06523,0.06046,0.0249,0.0254,1.0000 16.250,1.2299,0.06979,0.06507,0.0234,0.0238,1.0000 16.500,1.2151,0.07505,0.07040,0.0216,0.0228,1.0000 16.750,1.2067,0.07955,0.07499,0.0200,0.0213,1.0000 17.000,1.1988,0.08403,0.07957,0.0183,0.0205,1.0000 17.250,1.1933,0.08822,0.08385,0.0167,0.0195,1.0000 17.500,1.1837,0.09317,0.08886,0.0147,0.0185,1.0000 17.750,1.1722,0.09846,0.09423,0.0126,0.0179,1.0000