Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-v43015-il-50000-n5 Airfoil,v43015-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,27.1007 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-v43015-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.5223,0.07582,0.06844,-0.0373,1.0000,0.0811 -8.750,-0.5276,0.07307,0.06570,-0.0347,1.0000,0.0801 -8.500,-0.5375,0.07049,0.06309,-0.0316,1.0000,0.0790 -8.250,-0.5495,0.06792,0.06043,-0.0280,1.0000,0.0778 -8.000,-0.5620,0.06538,0.05774,-0.0242,1.0000,0.0761 -7.750,-0.5863,0.06313,0.05495,-0.0184,1.0000,0.0730 -7.500,-0.5837,0.06073,0.05251,-0.0157,1.0000,0.0724 -7.250,-0.5834,0.05848,0.05016,-0.0126,1.0000,0.0718 -7.000,-0.5831,0.05633,0.04786,-0.0094,1.0000,0.0713 -6.750,-0.5817,0.05430,0.04565,-0.0062,1.0000,0.0708 -6.500,-0.5795,0.05242,0.04356,-0.0030,1.0000,0.0709 -6.250,-0.5745,0.05063,0.04151,-0.0002,0.9995,0.0712 -6.000,-0.5439,0.04821,0.03864,-0.0019,0.9892,0.0720 -5.750,-0.5118,0.04595,0.03596,-0.0034,0.9787,0.0723 -5.500,-0.4767,0.04381,0.03348,-0.0053,0.9683,0.0722 -5.250,-0.4408,0.04184,0.03119,-0.0069,0.9572,0.0723 -5.000,-0.4065,0.04017,0.02917,-0.0080,0.9447,0.0728 -4.750,-0.3701,0.03845,0.02733,-0.0097,0.9327,0.0743 -4.500,-0.3260,0.03682,0.02558,-0.0125,0.9224,0.0764 -4.250,-0.2903,0.03546,0.02406,-0.0135,0.9082,0.0776 -4.000,-0.2503,0.03414,0.02261,-0.0151,0.8950,0.0786 -3.750,-0.1990,0.03279,0.02112,-0.0184,0.8851,0.0807 -3.500,-0.1572,0.03160,0.01997,-0.0202,0.8708,0.0836 -3.250,-0.1126,0.03045,0.01890,-0.0224,0.8569,0.0870 -3.000,-0.0675,0.02942,0.01783,-0.0244,0.8434,0.0899 -2.750,-0.0263,0.02835,0.01673,-0.0260,0.8290,0.0940 -2.500,0.0040,0.02748,0.01583,-0.0258,0.8108,0.0993 -2.250,0.0334,0.02667,0.01493,-0.0254,0.7917,0.1045 -2.000,0.0616,0.02582,0.01402,-0.0248,0.7718,0.1116 -1.750,0.0899,0.02500,0.01310,-0.0242,0.7503,0.1221 -1.500,0.1139,0.02424,0.01234,-0.0229,0.7262,0.1393 -1.250,0.1196,0.02201,0.01179,-0.0190,0.7052,0.4703 -1.000,0.1988,0.02202,0.01297,-0.0222,0.6741,0.8460 -0.750,0.2882,0.02313,0.01358,-0.0296,0.6355,0.9137 -0.500,0.3621,0.02361,0.01361,-0.0366,0.5989,0.9504 -0.250,0.4080,0.02368,0.01333,-0.0398,0.5695,0.9665 0.000,0.4457,0.02368,0.01305,-0.0419,0.5429,0.9766 0.250,0.4837,0.02370,0.01278,-0.0442,0.5191,0.9866 0.500,0.5225,0.02373,0.01252,-0.0467,0.4969,0.9961 0.750,0.5484,0.02385,0.01244,-0.0469,0.4784,1.0000 1.000,0.5645,0.02404,0.01248,-0.0451,0.4627,1.0000 1.250,0.5809,0.02425,0.01256,-0.0435,0.4485,1.0000 1.500,0.5981,0.02449,0.01262,-0.0418,0.4361,1.0000 1.750,0.6147,0.02476,0.01277,-0.0401,0.4233,1.0000 2.000,0.6316,0.02506,0.01298,-0.0384,0.4117,1.0000 2.250,0.6493,0.02538,0.01313,-0.0368,0.4015,1.0000 2.500,0.6658,0.02576,0.01347,-0.0350,0.3910,1.0000 2.750,0.6841,0.02613,0.01369,-0.0335,0.3824,1.0000 3.000,0.7005,0.02659,0.01414,-0.0317,0.3731,1.0000 3.250,0.7184,0.02701,0.01444,-0.0301,0.3650,1.0000 3.500,0.7354,0.02751,0.01490,-0.0284,0.3571,1.0000 3.750,0.7522,0.02802,0.01539,-0.0267,0.3494,1.0000 4.000,0.7721,0.02849,0.01570,-0.0253,0.3434,1.0000 4.250,0.7867,0.02915,0.01644,-0.0233,0.3360,1.0000 4.500,0.8036,0.02972,0.01699,-0.0216,0.3295,1.0000 5.000,0.8368,0.03102,0.01828,-0.0181,0.3177,1.0000 5.250,0.8526,0.03169,0.01896,-0.0163,0.3119,1.0000 5.500,0.8723,0.03225,0.01940,-0.0150,0.3069,1.0000 5.750,0.8849,0.03310,0.02036,-0.0128,0.3012,1.0000 6.000,0.8979,0.03394,0.02127,-0.0107,0.2957,1.0000 6.250,0.9151,0.03462,0.02192,-0.0091,0.2910,1.0000 6.500,0.9337,0.03531,0.02254,-0.0078,0.2867,1.0000 6.750,0.9400,0.03648,0.02392,-0.0049,0.2814,1.0000 7.000,0.9520,0.03742,0.02493,-0.0028,0.2767,1.0000 7.250,0.9694,0.03815,0.02563,-0.0013,0.2727,1.0000 7.500,0.9848,0.03905,0.02652,0.0003,0.2690,1.0000 7.750,0.9844,0.04061,0.02831,0.0037,0.2646,1.0000 8.000,0.9903,0.04189,0.02971,0.0063,0.2605,1.0000 8.250,1.0033,0.04289,0.03074,0.0081,0.2570,1.0000 8.500,1.0247,0.04359,0.03136,0.0089,0.2540,1.0000 8.750,1.0157,0.04561,0.03361,0.0129,0.2506,1.0000 9.000,0.9994,0.04798,0.03620,0.0173,0.2471,1.0000 9.250,0.9862,0.05003,0.03837,0.0214,0.2439,1.0000 9.500,0.9848,0.05168,0.04006,0.0241,0.2409,1.0000 9.750,1.0042,0.05246,0.04083,0.0250,0.2382,1.0000 10.000,0.9928,0.05501,0.04347,0.0278,0.2359,1.0000 10.500,0.7432,0.08826,0.07724,0.0219,0.2226,1.0000 10.750,0.7642,0.08837,0.07735,0.0232,0.2209,1.0000