Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e851-il-100000-n5 Airfoil,e851-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,50.7368 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-e851-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.4615,0.09223,0.08724,-0.0395,1.0000,0.0110 -8.750,-0.4671,0.08819,0.08329,-0.0404,1.0000,0.0107 -8.500,-0.4744,0.08415,0.07933,-0.0412,1.0000,0.0104 -8.250,-0.4842,0.08012,0.07539,-0.0419,1.0000,0.0102 -8.000,-0.4976,0.07604,0.07141,-0.0424,1.0000,0.0100 -7.750,-0.5165,0.07206,0.06752,-0.0428,1.0000,0.0098 -7.500,-0.5337,0.06756,0.06304,-0.0445,1.0000,0.0096 -7.250,-0.5470,0.06331,0.05871,-0.0449,1.0000,0.0094 -7.000,-0.5562,0.05900,0.05427,-0.0449,1.0000,0.0092 -6.750,-0.5597,0.05473,0.04982,-0.0447,1.0000,0.0089 -6.500,-0.5570,0.05064,0.04545,-0.0445,1.0000,0.0086 -6.250,-0.5361,0.04555,0.03990,-0.0478,0.9964,0.0084 -6.000,-0.5119,0.04104,0.03487,-0.0505,0.9931,0.0082 -5.750,-0.4877,0.03726,0.03057,-0.0522,0.9897,0.0081 -5.500,-0.4619,0.03344,0.02618,-0.0537,0.9868,0.0082 -5.250,-0.4343,0.03003,0.02220,-0.0548,0.9844,0.0083 -5.000,-0.4053,0.02715,0.01885,-0.0557,0.9825,0.0087 -4.750,-0.3763,0.02541,0.01685,-0.0568,0.9804,0.0107 -4.500,-0.3495,0.02426,0.01545,-0.0569,0.9775,0.0141 -4.250,-0.3209,0.02306,0.01385,-0.0570,0.9749,0.0173 -4.000,-0.2932,0.02098,0.01166,-0.0573,0.9728,0.0207 -3.750,-0.2625,0.01982,0.01042,-0.0582,0.9706,0.0384 -3.500,-0.2308,0.01838,0.00915,-0.0596,0.9689,0.0912 -3.250,-0.2055,0.01647,0.00845,-0.0608,0.9666,0.3445 -3.000,-0.1806,0.01617,0.00860,-0.0603,0.9630,0.5081 -2.750,-0.1525,0.01621,0.00862,-0.0603,0.9598,0.5669 -2.500,-0.1229,0.01631,0.00865,-0.0605,0.9571,0.6105 -2.250,-0.0975,0.01639,0.00871,-0.0599,0.9537,0.6448 -2.000,-0.0717,0.01640,0.00854,-0.0595,0.9497,0.6654 -1.750,-0.0422,0.01641,0.00844,-0.0600,0.9466,0.6787 -1.500,-0.0105,0.01644,0.00836,-0.0610,0.9440,0.6914 -1.250,0.0157,0.01645,0.00831,-0.0609,0.9401,0.7039 -1.000,0.0426,0.01648,0.00828,-0.0610,0.9360,0.7167 -0.750,0.0732,0.01651,0.00828,-0.0618,0.9329,0.7301 -0.500,0.1057,0.01654,0.00824,-0.0629,0.9305,0.7443 -0.250,0.1287,0.01658,0.00830,-0.0621,0.9252,0.7591 0.000,0.1574,0.01661,0.00835,-0.0624,0.9213,0.7759 0.250,0.1892,0.01662,0.00841,-0.0634,0.9183,0.7948 0.500,0.2131,0.01665,0.00851,-0.0627,0.9132,0.8164 0.750,0.2400,0.01665,0.00861,-0.0625,0.9085,0.8433 1.000,0.2725,0.01659,0.00867,-0.0634,0.9053,0.8793 1.250,0.3086,0.01654,0.00876,-0.0654,0.9006,0.9516 1.500,0.3410,0.01661,0.00884,-0.0668,0.8951,1.0000 1.750,0.3790,0.01666,0.00893,-0.0691,0.8917,1.0000 2.000,0.4048,0.01681,0.00922,-0.0690,0.8840,1.0000 2.250,0.4424,0.01680,0.00930,-0.0711,0.8795,1.0000 2.500,0.4709,0.01687,0.00946,-0.0713,0.8713,1.0000 2.750,0.5126,0.01665,0.00940,-0.0738,0.8658,1.0000 3.000,0.5446,0.01650,0.00940,-0.0742,0.8551,1.0000 3.250,0.5855,0.01601,0.00921,-0.0759,0.8418,1.0000 3.500,0.6243,0.01519,0.00859,-0.0764,0.8177,1.0000 3.750,0.6589,0.01449,0.00807,-0.0761,0.7853,1.0000 4.000,0.6820,0.01418,0.00790,-0.0741,0.7384,1.0000 4.250,0.7230,0.01425,0.00685,-0.0739,0.4756,1.0000 4.500,0.7270,0.01629,0.00760,-0.0699,0.2491,1.0000 4.750,0.7389,0.01817,0.00855,-0.0677,0.1033,1.0000 5.000,0.7562,0.01957,0.00972,-0.0659,0.0622,1.0000 5.250,0.7735,0.02100,0.01107,-0.0640,0.0370,1.0000 5.500,0.7914,0.02245,0.01256,-0.0622,0.0227,1.0000 5.750,0.8104,0.02410,0.01451,-0.0604,0.0163,1.0000 6.000,0.8311,0.02697,0.01752,-0.0590,0.0138,1.0000 6.250,0.8581,0.02923,0.02003,-0.0584,0.0123,1.0000 6.500,0.8831,0.03092,0.02203,-0.0577,0.0095,1.0000 6.750,0.9048,0.03258,0.02396,-0.0568,0.0075,1.0000 7.000,0.9243,0.03495,0.02666,-0.0555,0.0067,1.0000 7.250,0.9414,0.03812,0.03028,-0.0537,0.0065,1.0000 7.500,0.9545,0.04151,0.03413,-0.0515,0.0064,1.0000 7.750,0.9631,0.04512,0.03820,-0.0488,0.0063,1.0000 8.000,0.9681,0.04882,0.04234,-0.0459,0.0063,1.0000 8.250,0.9690,0.05266,0.04658,-0.0428,0.0063,1.0000 8.500,0.9661,0.05657,0.05085,-0.0397,0.0064,1.0000 8.750,0.9593,0.06052,0.05512,-0.0365,0.0065,1.0000 9.000,0.9469,0.06424,0.05908,-0.0330,0.0066,1.0000 9.250,0.9321,0.06818,0.06323,-0.0302,0.0067,1.0000 9.500,0.9154,0.07244,0.06767,-0.0284,0.0068,1.0000 9.750,0.8977,0.07718,0.07258,-0.0280,0.0069,1.0000 10.000,0.8789,0.08281,0.07835,-0.0293,0.0071,1.0000 10.250,0.8606,0.08973,0.08537,-0.0326,0.0073,1.0000