Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-lwk79100-il-200000 Airfoil,lwk79100-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,47.7298 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-lwk79100-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.000,-0.7779,0.09684,0.09322,0.0054,1.0000,0.0379 -11.750,-0.7991,0.08724,0.08365,-0.0001,1.0000,0.0369 -11.500,-0.8327,0.07593,0.07227,-0.0087,1.0000,0.0358 -11.250,-0.8653,0.06711,0.06330,-0.0157,1.0000,0.0351 -11.000,-0.8960,0.06030,0.05631,-0.0203,1.0000,0.0345 -10.750,-0.9247,0.05514,0.05093,-0.0217,1.0000,0.0339 -10.500,-0.9487,0.05080,0.04630,-0.0203,1.0000,0.0335 -10.250,-0.9625,0.04608,0.04119,-0.0191,1.0000,0.0333 -10.000,-0.9649,0.04211,0.03683,-0.0178,1.0000,0.0335 -9.750,-0.9598,0.03875,0.03310,-0.0165,1.0000,0.0341 -9.500,-0.9497,0.03590,0.02988,-0.0153,1.0000,0.0352 -9.250,-0.9358,0.03372,0.02732,-0.0142,1.0000,0.0369 -9.000,-0.9188,0.03230,0.02550,-0.0130,1.0000,0.0382 -8.750,-0.9038,0.02830,0.02124,-0.0121,1.0000,0.0401 -8.500,-0.8830,0.02671,0.01957,-0.0115,1.0000,0.0420 -8.250,-0.8612,0.02545,0.01817,-0.0107,1.0000,0.0449 -8.000,-0.8385,0.02447,0.01694,-0.0099,1.0000,0.0477 -7.750,-0.8174,0.02229,0.01468,-0.0091,1.0000,0.0508 -7.500,-0.7945,0.02130,0.01367,-0.0085,1.0000,0.0546 -7.250,-0.7706,0.02044,0.01267,-0.0078,1.0000,0.0585 -7.000,-0.7488,0.01893,0.01116,-0.0070,1.0000,0.0625 -6.750,-0.7254,0.01812,0.01035,-0.0063,1.0000,0.0680 -6.500,-0.7025,0.01713,0.00931,-0.0055,1.0000,0.0737 -6.250,-0.6797,0.01626,0.00846,-0.0047,1.0000,0.0813 -6.000,-0.6570,0.01537,0.00762,-0.0039,1.0000,0.0921 -5.750,-0.6340,0.01454,0.00685,-0.0032,1.0000,0.1091 -5.500,-0.6115,0.01364,0.00612,-0.0024,1.0000,0.1373 -5.250,-0.5888,0.01282,0.00553,-0.0018,1.0000,0.1783 -5.000,-0.5655,0.01212,0.00504,-0.0012,1.0000,0.2252 -4.750,-0.5425,0.01145,0.00464,-0.0006,1.0000,0.2772 -4.500,-0.5194,0.01088,0.00434,0.0001,1.0000,0.3378 -4.250,-0.4959,0.01043,0.00412,0.0009,1.0000,0.3956 -4.000,-0.4720,0.01012,0.00399,0.0017,1.0000,0.4470 -3.750,-0.4480,0.00991,0.00394,0.0026,1.0000,0.4905 -3.500,-0.4236,0.00980,0.00392,0.0034,1.0000,0.5244 -3.250,-0.3993,0.00974,0.00390,0.0043,1.0000,0.5524 -3.000,-0.3757,0.00969,0.00392,0.0052,1.0000,0.5753 -2.750,-0.3510,0.00969,0.00396,0.0055,0.9973,0.5963 -2.500,-0.3021,0.00970,0.00399,0.0012,0.9696,0.6180 -2.250,-0.2566,0.00971,0.00397,-0.0022,0.9375,0.6376 -2.000,-0.2158,0.00972,0.00392,-0.0046,0.9048,0.6550 -1.750,-0.1833,0.00975,0.00387,-0.0050,0.8757,0.6703 -1.500,-0.1558,0.00979,0.00384,-0.0044,0.8521,0.6839 -1.250,-0.1297,0.00983,0.00382,-0.0036,0.8334,0.6967 -1.000,-0.1039,0.00987,0.00381,-0.0028,0.8169,0.7096 -0.750,-0.0779,0.00990,0.00380,-0.0021,0.8024,0.7226 -0.500,-0.0520,0.00993,0.00381,-0.0014,0.7893,0.7361 -0.250,-0.0261,0.00994,0.00381,-0.0006,0.7762,0.7501 0.000,0.0000,0.00994,0.00382,0.0000,0.7634,0.7634 0.250,0.0261,0.00994,0.00381,0.0006,0.7501,0.7762 0.500,0.0520,0.00993,0.00381,0.0014,0.7361,0.7893 0.750,0.0779,0.00990,0.00380,0.0021,0.7226,0.8024 1.000,0.1039,0.00987,0.00381,0.0028,0.7097,0.8169 1.250,0.1298,0.00983,0.00382,0.0036,0.6967,0.8334 1.500,0.1558,0.00979,0.00384,0.0044,0.6839,0.8521 1.750,0.1833,0.00975,0.00387,0.0050,0.6703,0.8758 2.000,0.2158,0.00972,0.00392,0.0046,0.6550,0.9048 2.250,0.2566,0.00971,0.00397,0.0022,0.6376,0.9375 2.500,0.3021,0.00970,0.00399,-0.0012,0.6179,0.9697 2.750,0.3511,0.00969,0.00396,-0.0055,0.5964,0.9974 3.000,0.3756,0.00969,0.00392,-0.0051,0.5755,1.0000 3.250,0.3992,0.00974,0.00390,-0.0042,0.5525,1.0000 3.500,0.4236,0.00980,0.00392,-0.0034,0.5245,1.0000 3.750,0.4479,0.00991,0.00394,-0.0026,0.4906,1.0000 4.000,0.4720,0.01012,0.00399,-0.0017,0.4470,1.0000 4.250,0.4958,0.01043,0.00412,-0.0009,0.3955,1.0000 4.500,0.5193,0.01088,0.00434,-0.0001,0.3378,1.0000 4.750,0.5425,0.01145,0.00464,0.0006,0.2773,1.0000 5.000,0.5655,0.01212,0.00504,0.0012,0.2252,1.0000 5.250,0.5887,0.01282,0.00553,0.0018,0.1783,1.0000 5.500,0.6115,0.01364,0.00612,0.0024,0.1373,1.0000 5.750,0.6340,0.01454,0.00685,0.0032,0.1091,1.0000 6.000,0.6570,0.01537,0.00762,0.0039,0.0921,1.0000 6.250,0.6797,0.01626,0.00846,0.0047,0.0812,1.0000 6.500,0.7026,0.01713,0.00931,0.0054,0.0737,1.0000 6.750,0.7255,0.01812,0.01035,0.0063,0.0679,1.0000 7.000,0.7488,0.01894,0.01116,0.0069,0.0624,1.0000 7.250,0.7707,0.02045,0.01267,0.0078,0.0585,1.0000 7.500,0.7946,0.02128,0.01365,0.0085,0.0545,1.0000 7.750,0.8175,0.02229,0.01468,0.0091,0.0508,1.0000 8.000,0.8386,0.02447,0.01695,0.0099,0.0477,1.0000 8.250,0.8614,0.02543,0.01815,0.0107,0.0448,1.0000 8.500,0.8831,0.02672,0.01958,0.0114,0.0421,1.0000 8.750,0.9040,0.02832,0.02126,0.0121,0.0400,1.0000 9.000,0.9189,0.03239,0.02559,0.0129,0.0383,1.0000 9.250,0.9359,0.03380,0.02741,0.0141,0.0369,1.0000 9.500,0.9501,0.03586,0.02984,0.0153,0.0351,1.0000 9.750,0.9600,0.03878,0.03313,0.0165,0.0341,1.0000 10.000,0.9648,0.04221,0.03693,0.0177,0.0336,1.0000 10.250,0.9632,0.04605,0.04115,0.0190,0.0332,1.0000 10.500,0.9494,0.05078,0.04628,0.0202,0.0335,1.0000 10.750,0.9252,0.05516,0.05095,0.0216,0.0338,1.0000 11.000,0.8966,0.06032,0.05633,0.0201,0.0344,1.0000 11.250,0.8662,0.06709,0.06328,0.0156,0.0350,1.0000 11.500,0.8336,0.07597,0.07231,0.0086,0.0358,1.0000 11.750,0.7966,0.08815,0.08457,-0.0009,0.0369,1.0000 12.000,0.7763,0.09764,0.09403,-0.0062,0.0379,1.0000