Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ea61012-il-100000-n5 Airfoil,ea61012-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,29.1104 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-ea61012-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.000,-0.7863,0.09461,0.08884,-0.0143,1.0000,0.0587 -12.750,-0.8539,0.07852,0.07257,-0.0259,1.0000,0.0580 -12.500,-0.8967,0.07006,0.06389,-0.0307,1.0000,0.0578 -12.250,-0.9289,0.06421,0.05781,-0.0326,1.0000,0.0578 -12.000,-0.9557,0.05967,0.05301,-0.0328,1.0000,0.0580 -11.750,-0.9797,0.05602,0.04908,-0.0313,1.0000,0.0584 -11.500,-0.9993,0.05302,0.04577,-0.0285,1.0000,0.0590 -11.250,-1.0124,0.05004,0.04237,-0.0260,1.0000,0.0597 -11.000,-1.0063,0.04764,0.03983,-0.0249,1.0000,0.0606 -10.750,-0.9943,0.04577,0.03786,-0.0240,1.0000,0.0615 -10.500,-0.9831,0.04383,0.03576,-0.0229,1.0000,0.0623 -10.250,-0.9707,0.04188,0.03360,-0.0218,1.0000,0.0632 -10.000,-0.9573,0.03998,0.03148,-0.0208,1.0000,0.0641 -9.750,-0.9425,0.03816,0.02943,-0.0197,1.0000,0.0652 -9.500,-0.9269,0.03651,0.02751,-0.0187,1.0000,0.0668 -9.250,-0.9105,0.03494,0.02562,-0.0176,1.0000,0.0684 -9.000,-0.8913,0.03340,0.02384,-0.0168,1.0000,0.0695 -8.750,-0.8686,0.03191,0.02232,-0.0165,1.0000,0.0705 -8.500,-0.8461,0.03064,0.02100,-0.0161,1.0000,0.0716 -8.250,-0.8234,0.02946,0.01976,-0.0156,1.0000,0.0728 -8.000,-0.8005,0.02835,0.01857,-0.0151,1.0000,0.0741 -7.750,-0.7774,0.02730,0.01743,-0.0146,1.0000,0.0755 -7.500,-0.7545,0.02638,0.01640,-0.0140,1.0000,0.0775 -7.250,-0.7318,0.02553,0.01545,-0.0134,1.0000,0.0795 -7.000,-0.7097,0.02456,0.01459,-0.0128,1.0000,0.0814 -6.750,-0.6885,0.02376,0.01382,-0.0120,1.0000,0.0833 -6.500,-0.6685,0.02302,0.01311,-0.0110,1.0000,0.0850 -6.250,-0.6513,0.02237,0.01246,-0.0095,1.0000,0.0869 -6.000,-0.6248,0.02168,0.01173,-0.0098,0.9880,0.0892 -5.750,-0.5925,0.02089,0.01094,-0.0113,0.9723,0.0920 -5.500,-0.5603,0.02016,0.01025,-0.0128,0.9592,0.0956 -5.250,-0.5281,0.01958,0.00963,-0.0141,0.9476,0.1011 -5.000,-0.4971,0.01893,0.00902,-0.0152,0.9371,0.1083 -4.750,-0.4662,0.01838,0.00846,-0.0162,0.9281,0.1180 -4.500,-0.4389,0.01777,0.00797,-0.0165,0.9188,0.1329 -4.250,-0.4118,0.01709,0.00748,-0.0168,0.9112,0.1657 -4.000,-0.3896,0.01631,0.00706,-0.0163,0.9022,0.2307 -3.750,-0.3685,0.01542,0.00671,-0.0156,0.8947,0.3369 -3.500,-0.3493,0.01476,0.00651,-0.0142,0.8864,0.4316 -3.250,-0.3282,0.01448,0.00681,-0.0124,0.8800,0.5408 -3.000,-0.3035,0.01453,0.00695,-0.0114,0.8739,0.5965 -2.750,-0.2783,0.01466,0.00711,-0.0104,0.8678,0.6323 -2.500,-0.2527,0.01492,0.00741,-0.0092,0.8626,0.6683 -2.250,-0.2288,0.01529,0.00782,-0.0077,0.8562,0.6994 -2.000,-0.2044,0.01563,0.00815,-0.0062,0.8506,0.7243 -1.750,-0.1786,0.01595,0.00847,-0.0049,0.8465,0.7433 -1.500,-0.1541,0.01611,0.00861,-0.0039,0.8406,0.7570 -1.250,-0.1283,0.01616,0.00862,-0.0033,0.8352,0.7662 -1.000,-0.1012,0.01617,0.00858,-0.0028,0.8305,0.7727 -0.750,-0.0761,0.01619,0.00858,-0.0023,0.8233,0.7796 -0.500,-0.0503,0.01617,0.00851,-0.0017,0.8167,0.7864 -0.250,-0.0251,0.01618,0.00854,-0.0009,0.8086,0.7932 0.000,0.0000,0.01617,0.00850,0.0000,0.8015,0.8015 0.250,0.0251,0.01618,0.00854,0.0009,0.7932,0.8086 0.500,0.0503,0.01617,0.00851,0.0017,0.7864,0.8167 0.750,0.0761,0.01619,0.00858,0.0023,0.7796,0.8233 1.000,0.1012,0.01617,0.00858,0.0028,0.7728,0.8305 1.250,0.1283,0.01616,0.00862,0.0033,0.7662,0.8352 1.500,0.1541,0.01611,0.00862,0.0039,0.7570,0.8406 1.750,0.1786,0.01595,0.00847,0.0049,0.7433,0.8465 2.000,0.2044,0.01563,0.00816,0.0062,0.7244,0.8506 2.250,0.2288,0.01529,0.00782,0.0077,0.6995,0.8562 2.500,0.2527,0.01492,0.00742,0.0092,0.6685,0.8626 2.750,0.2783,0.01466,0.00711,0.0104,0.6323,0.8678 3.000,0.3035,0.01453,0.00695,0.0114,0.5966,0.8739 3.250,0.3282,0.01448,0.00682,0.0124,0.5410,0.8800 3.500,0.3493,0.01476,0.00651,0.0142,0.4312,0.8864 3.750,0.3686,0.01542,0.00671,0.0156,0.3377,0.8947 4.000,0.3896,0.01630,0.00706,0.0163,0.2312,0.9022 4.500,0.4390,0.01777,0.00796,0.0165,0.1329,0.9188 4.750,0.4662,0.01838,0.00846,0.0162,0.1181,0.9281 5.000,0.4972,0.01893,0.00902,0.0152,0.1084,0.9372 5.250,0.5281,0.01958,0.00963,0.0141,0.1012,0.9476 5.500,0.5603,0.02016,0.01025,0.0128,0.0956,0.9592 5.750,0.5925,0.02088,0.01094,0.0113,0.0920,0.9724 6.000,0.6248,0.02168,0.01173,0.0098,0.0892,0.9881 6.250,0.6512,0.02237,0.01246,0.0095,0.0869,1.0000 6.500,0.6685,0.02302,0.01310,0.0110,0.0851,1.0000 6.750,0.6885,0.02376,0.01382,0.0120,0.0833,1.0000 7.000,0.7098,0.02455,0.01458,0.0128,0.0814,1.0000 7.250,0.7318,0.02553,0.01545,0.0134,0.0795,1.0000 7.500,0.7546,0.02638,0.01640,0.0140,0.0774,1.0000 7.750,0.7775,0.02730,0.01742,0.0146,0.0755,1.0000 8.000,0.8006,0.02836,0.01858,0.0151,0.0741,1.0000 8.250,0.8235,0.02946,0.01976,0.0156,0.0728,1.0000 8.500,0.8462,0.03064,0.02100,0.0161,0.0716,1.0000 8.750,0.8687,0.03191,0.02231,0.0165,0.0705,1.0000 9.000,0.8914,0.03340,0.02383,0.0168,0.0695,1.0000 9.250,0.9104,0.03494,0.02562,0.0176,0.0683,1.0000 9.500,0.9269,0.03651,0.02752,0.0187,0.0667,1.0000 9.750,0.9427,0.03817,0.02943,0.0197,0.0652,1.0000 10.000,0.9574,0.03998,0.03149,0.0207,0.0641,1.0000 10.250,0.9709,0.04189,0.03361,0.0218,0.0632,1.0000 10.500,0.9832,0.04384,0.03577,0.0229,0.0624,1.0000 10.750,0.9946,0.04576,0.03785,0.0239,0.0615,1.0000 11.000,1.0067,0.04765,0.03983,0.0248,0.0605,1.0000 11.250,1.0125,0.05005,0.04238,0.0260,0.0597,1.0000 11.500,0.9991,0.05304,0.04580,0.0285,0.0589,1.0000 11.750,0.9793,0.05607,0.04914,0.0313,0.0584,1.0000 12.000,0.9561,0.05970,0.05305,0.0327,0.0580,1.0000 12.250,0.9295,0.06424,0.05784,0.0325,0.0578,1.0000 12.500,0.8964,0.07017,0.06401,0.0306,0.0578,1.0000 12.750,0.8538,0.07864,0.07270,0.0257,0.0580,1.0000 13.000,0.7839,0.09539,0.08963,0.0136,0.0587,1.0000