Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-lwk80100-il-500000 Airfoil,lwk80100-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,49.0147 Max Cl/Cd alpha,3.25 Url,http://airfoiltools.com/polar/csv?polar=xf-lwk80100-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.750,-0.7135,0.09312,0.09094,-0.0086,1.0000,0.0155 -11.500,-0.7303,0.08654,0.08440,-0.0128,1.0000,0.0145 -11.250,-0.7737,0.06822,0.06593,-0.0274,1.0000,0.0138 -11.000,-0.8100,0.05945,0.05697,-0.0323,1.0000,0.0133 -10.750,-0.9390,0.04052,0.03699,-0.0288,1.0000,0.0114 -10.500,-0.8805,0.04648,0.04343,-0.0311,1.0000,0.0129 -10.250,-0.8997,0.04245,0.03912,-0.0274,1.0000,0.0130 -10.000,-0.9352,0.03404,0.02991,-0.0217,1.0000,0.0121 -9.750,-0.9319,0.03105,0.02659,-0.0191,1.0000,0.0123 -9.500,-0.9214,0.02907,0.02439,-0.0172,1.0000,0.0126 -9.250,-0.9093,0.02703,0.02210,-0.0153,1.0000,0.0128 -9.000,-0.8944,0.02539,0.02026,-0.0136,1.0000,0.0134 -8.750,-0.8767,0.02430,0.01901,-0.0123,1.0000,0.0143 -8.500,-0.8599,0.02263,0.01712,-0.0107,1.0000,0.0146 -8.250,-0.8418,0.02116,0.01546,-0.0093,1.0000,0.0149 -8.000,-0.8216,0.02046,0.01461,-0.0081,1.0000,0.0154 -7.750,-0.8088,0.01796,0.01189,-0.0058,1.0000,0.0162 -7.500,-0.7896,0.01681,0.01069,-0.0048,0.9915,0.0173 -7.250,-0.7561,0.01592,0.00974,-0.0066,0.9834,0.0184 -7.000,-0.7210,0.01521,0.00896,-0.0086,0.9765,0.0206 -6.750,-0.6863,0.01412,0.00776,-0.0106,0.9701,0.0237 -6.500,-0.6502,0.01345,0.00706,-0.0129,0.9635,0.0275 -6.250,-0.6130,0.01281,0.00633,-0.0154,0.9574,0.0317 -6.000,-0.5786,0.01219,0.00570,-0.0173,0.9494,0.0383 -5.750,-0.5446,0.01168,0.00514,-0.0190,0.9423,0.0450 -5.500,-0.5152,0.01139,0.00481,-0.0196,0.9341,0.0524 -5.250,-0.4871,0.01096,0.00438,-0.0200,0.9272,0.0626 -5.000,-0.4635,0.01061,0.00405,-0.0194,0.9195,0.0755 -4.750,-0.4377,0.01029,0.00375,-0.0192,0.9135,0.0938 -4.500,-0.4161,0.00989,0.00347,-0.0181,0.9071,0.1235 -4.250,-0.3949,0.00941,0.00320,-0.0171,0.9015,0.1785 -4.000,-0.3764,0.00878,0.00294,-0.0157,0.8960,0.2686 -3.750,-0.3603,0.00809,0.00268,-0.0137,0.8902,0.3798 -3.500,-0.3465,0.00732,0.00244,-0.0112,0.8853,0.5131 -3.250,-0.3328,0.00681,0.00241,-0.0082,0.8802,0.6381 -3.000,-0.3102,0.00675,0.00245,-0.0069,0.8759,0.6865 -2.750,-0.2854,0.00677,0.00249,-0.0061,0.8722,0.7151 -2.500,-0.2597,0.00682,0.00252,-0.0055,0.8689,0.7326 -2.250,-0.2346,0.00686,0.00255,-0.0048,0.8648,0.7474 -2.000,-0.2088,0.00692,0.00259,-0.0042,0.8611,0.7604 -1.750,-0.1825,0.00698,0.00261,-0.0038,0.8578,0.7704 -1.500,-0.1561,0.00706,0.00268,-0.0033,0.8547,0.7803 -1.250,-0.1307,0.00713,0.00277,-0.0026,0.8509,0.7910 -1.000,-0.1052,0.00721,0.00286,-0.0019,0.8471,0.8018 -0.750,-0.0789,0.00729,0.00292,-0.0014,0.8437,0.8108 -0.500,-0.0519,0.00735,0.00300,-0.0011,0.8405,0.8180 -0.250,-0.0268,0.00738,0.00304,-0.0004,0.8356,0.8253 0.000,0.0000,0.00738,0.00304,0.0000,0.8308,0.8307 0.250,0.0269,0.00739,0.00304,0.0004,0.8254,0.8356 0.500,0.0519,0.00734,0.00299,0.0011,0.8177,0.8404 0.750,0.0789,0.00729,0.00292,0.0014,0.8107,0.8437 1.000,0.1052,0.00721,0.00286,0.0019,0.8018,0.8471 1.250,0.1309,0.00714,0.00278,0.0026,0.7916,0.8509 1.500,0.1560,0.00705,0.00267,0.0034,0.7794,0.8548 1.750,0.1825,0.00698,0.00260,0.0038,0.7700,0.8579 2.000,0.2087,0.00691,0.00258,0.0043,0.7593,0.8611 2.250,0.2346,0.00686,0.00255,0.0048,0.7469,0.8648 2.500,0.2597,0.00682,0.00252,0.0055,0.7318,0.8689 2.750,0.2855,0.00677,0.00249,0.0061,0.7160,0.8722 3.000,0.3108,0.00675,0.00247,0.0068,0.6915,0.8758 3.250,0.3333,0.00680,0.00242,0.0081,0.6419,0.8802 3.500,0.3475,0.00728,0.00243,0.0110,0.5216,0.8853 3.750,0.3606,0.00807,0.00268,0.0137,0.3819,0.8902 4.000,0.3762,0.00880,0.00295,0.0157,0.2660,0.8961 4.250,0.3951,0.00940,0.00320,0.0171,0.1798,0.9015 4.500,0.4164,0.00988,0.00346,0.0181,0.1251,0.9071 4.750,0.4381,0.01026,0.00373,0.0191,0.0963,0.9135 5.000,0.4636,0.01060,0.00405,0.0194,0.0775,0.9196 5.250,0.4873,0.01094,0.00436,0.0200,0.0644,0.9273 5.500,0.5155,0.01136,0.00478,0.0196,0.0526,0.9341 5.750,0.5449,0.01164,0.00509,0.0190,0.0444,0.9422 6.000,0.5791,0.01211,0.00562,0.0172,0.0378,0.9493 6.250,0.6126,0.01290,0.00642,0.0154,0.0305,0.9575 6.500,0.6509,0.01333,0.00692,0.0129,0.0261,0.9633 6.750,0.6842,0.01463,0.00830,0.0110,0.0217,0.9706 7.000,0.7217,0.01510,0.00884,0.0085,0.0195,0.9764 7.250,0.7564,0.01587,0.00967,0.0065,0.0180,0.9834 7.500,0.7892,0.01692,0.01077,0.0048,0.0165,0.9918 7.750,0.8054,0.01880,0.01279,0.0064,0.0157,1.0000 8.000,0.8218,0.02041,0.01457,0.0081,0.0152,1.0000 8.250,0.8410,0.02147,0.01581,0.0095,0.0149,1.0000 8.500,0.8591,0.02292,0.01745,0.0110,0.0143,1.0000 8.750,0.8752,0.02478,0.01954,0.0126,0.0141,1.0000 9.000,0.8914,0.02625,0.02122,0.0142,0.0135,1.0000 9.250,0.9056,0.02796,0.02315,0.0159,0.0130,1.0000 9.500,0.9166,0.03010,0.02554,0.0179,0.0126,1.0000 9.750,0.9224,0.03291,0.02867,0.0203,0.0125,1.0000 10.000,0.9239,0.03596,0.03205,0.0229,0.0124,1.0000 10.250,0.8879,0.04405,0.04083,0.0283,0.0131,1.0000 10.500,0.8550,0.04954,0.04664,0.0323,0.0138,1.0000 10.750,0.8301,0.05444,0.05177,0.0333,0.0138,1.0000 11.000,0.8042,0.06024,0.05776,0.0319,0.0138,1.0000 11.250,0.7740,0.06795,0.06564,0.0274,0.0142,1.0000 11.500,0.5486,0.08516,0.08307,0.0195,0.0197,1.0000 11.750,0.5760,0.08177,0.07970,0.0209,0.0170,1.0000 12.000,0.5662,0.08758,0.08550,0.0186,0.0167,1.0000 12.250,0.5650,0.09082,0.08873,0.0173,0.0162,1.0000 13.250,0.6564,0.14458,0.14224,-0.0147,0.0205,1.0000 13.500,0.4760,0.12429,0.12215,0.0060,0.0220,1.0000 13.750,0.4746,0.12797,0.12583,0.0042,0.0220,1.0000