Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fxm2-il-100000 Airfoil,fxm2-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,45.9334 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-fxm2-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.250,-0.2698,0.09562,0.09102,-0.0153,1.0000,0.0488 -7.000,-0.2705,0.09360,0.08908,-0.0146,1.0000,0.0498 -6.750,-0.2739,0.09175,0.08732,-0.0136,1.0000,0.0509 -6.500,-0.2752,0.08975,0.08541,-0.0138,1.0000,0.0519 -6.250,-0.2747,0.08786,0.08361,-0.0159,1.0000,0.0530 -6.000,-0.2693,0.08628,0.08207,-0.0231,1.0000,0.0538 -5.750,-0.2617,0.08307,0.07891,-0.0262,1.0000,0.0543 -5.500,-0.2615,0.07946,0.07540,-0.0201,1.0000,0.0552 -5.250,-0.2572,0.07676,0.07278,-0.0182,1.0000,0.0565 -5.000,-0.2506,0.07420,0.07028,-0.0184,1.0000,0.0583 -4.750,-0.2403,0.07154,0.06764,-0.0206,1.0000,0.0613 -4.500,-0.2091,0.06820,0.06414,-0.0322,1.0000,0.0648 -4.250,-0.2124,0.06535,0.06146,-0.0269,1.0000,0.0664 -4.000,-0.2040,0.06298,0.05916,-0.0263,1.0000,0.0693 -3.750,-0.1602,0.06002,0.05585,-0.0380,1.0000,0.0757 -3.500,-0.1462,0.05607,0.05212,-0.0370,0.9959,0.0780 -3.250,-0.0805,0.05147,0.04724,-0.0494,0.9865,0.0881 -3.000,-0.0239,0.04752,0.04307,-0.0582,0.9767,0.1004 -2.750,0.0278,0.04349,0.03898,-0.0652,0.9669,0.1154 -2.500,0.0722,0.04005,0.03558,-0.0700,0.9530,0.1359 -1.750,0.2077,0.03120,0.02675,-0.0827,0.9039,0.2923 -1.250,0.2613,0.02654,0.02259,-0.0778,0.8529,0.4685 -1.000,0.2932,0.02455,0.02062,-0.0759,0.8167,0.5434 -0.750,0.4450,0.02086,0.01378,-0.1004,0.7625,0.1390 -0.500,0.4825,0.01994,0.01218,-0.1002,0.7081,0.1239 -0.250,0.5139,0.01955,0.01110,-0.0990,0.6583,0.1121 0.000,0.5411,0.01884,0.01004,-0.0980,0.6134,0.1080 0.250,0.5675,0.01852,0.00936,-0.0968,0.5733,0.1060 0.500,0.5933,0.01839,0.00889,-0.0956,0.5390,0.1090 0.750,0.6187,0.01824,0.00853,-0.0945,0.5057,0.1097 1.000,0.6436,0.01815,0.00823,-0.0933,0.4785,0.1109 1.250,0.6690,0.01821,0.00807,-0.0924,0.4543,0.1140 1.500,0.6950,0.01819,0.00794,-0.0917,0.4322,0.1233 1.750,0.7222,0.01835,0.00785,-0.0912,0.4154,0.1330 2.000,0.7500,0.01855,0.00792,-0.0908,0.3999,0.1621 2.250,0.7667,0.01711,0.00816,-0.0879,0.3872,1.0000 2.500,0.7937,0.01757,0.00831,-0.0873,0.3743,1.0000 2.750,0.8206,0.01805,0.00853,-0.0869,0.3633,1.0000 3.000,0.8475,0.01859,0.00880,-0.0865,0.3538,1.0000 3.250,0.8743,0.01917,0.00917,-0.0861,0.3441,1.0000 3.500,0.9007,0.01976,0.00969,-0.0858,0.3344,1.0000 3.750,0.9274,0.02037,0.01016,-0.0855,0.3265,1.0000 4.000,0.9537,0.02089,0.01063,-0.0851,0.3185,1.0000 4.250,0.9799,0.02143,0.01113,-0.0847,0.3111,1.0000 4.500,1.0064,0.02191,0.01148,-0.0843,0.3046,1.0000 4.750,1.0320,0.02248,0.01205,-0.0839,0.2974,1.0000 5.000,1.0589,0.02307,0.01244,-0.0837,0.2917,1.0000 5.250,1.0839,0.02380,0.01327,-0.0832,0.2852,1.0000 5.500,1.1106,0.02455,0.01392,-0.0830,0.2800,1.0000 5.750,1.1348,0.02536,0.01488,-0.0825,0.2740,1.0000 6.000,1.1606,0.02607,0.01552,-0.0821,0.2681,1.0000 6.250,1.1838,0.02680,0.01643,-0.0814,0.2613,1.0000 6.500,1.2098,0.02740,0.01693,-0.0811,0.2559,1.0000 6.750,1.2322,0.02814,0.01789,-0.0803,0.2491,1.0000 7.000,1.2579,0.02870,0.01832,-0.0800,0.2437,1.0000 7.250,1.2804,0.02947,0.01922,-0.0792,0.2369,1.0000 7.500,1.3046,0.03030,0.02004,-0.0788,0.2311,1.0000 7.750,1.3272,0.03120,0.02100,-0.0781,0.2245,1.0000 8.000,1.3485,0.03236,0.02229,-0.0774,0.2182,1.0000 8.250,1.3707,0.03331,0.02330,-0.0767,0.2121,1.0000 8.500,1.3898,0.03460,0.02480,-0.0757,0.2065,1.0000 8.750,1.4101,0.03567,0.02605,-0.0748,0.2011,1.0000 9.000,1.4330,0.03668,0.02705,-0.0743,0.1971,1.0000 9.250,1.4469,0.03835,0.02911,-0.0728,0.1919,1.0000 9.500,1.4680,0.03931,0.03012,-0.0721,0.1882,1.0000 9.750,1.4937,0.04019,0.03091,-0.0719,0.1854,1.0000 10.000,1.4986,0.04297,0.03426,-0.0698,0.1818,1.0000 10.250,1.5083,0.04531,0.03692,-0.0682,0.1788,1.0000 10.500,1.5213,0.04726,0.03907,-0.0670,0.1762,1.0000 10.750,1.5367,0.04895,0.04088,-0.0660,0.1741,1.0000 11.000,1.5555,0.05056,0.04255,-0.0654,0.1722,1.0000 11.250,1.5621,0.05356,0.04577,-0.0640,0.1706,1.0000 11.500,1.5390,0.05848,0.05123,-0.0607,0.1693,1.0000 11.750,1.4975,0.06443,0.05763,-0.0568,0.1686,1.0000 12.000,1.4182,0.07357,0.06711,-0.0540,0.1688,1.0000