Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-lwk79100-il-100000-n5 Airfoil,lwk79100-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,35.5063 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-lwk79100-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.500,-0.8119,0.09724,0.09206,0.0066,1.0000,0.0298 -12.250,-0.8396,0.08635,0.08111,-0.0010,1.0000,0.0294 -12.000,-0.8675,0.07681,0.07145,-0.0082,1.0000,0.0292 -11.750,-0.8917,0.06927,0.06374,-0.0137,1.0000,0.0290 -11.500,-0.9135,0.06309,0.05738,-0.0178,1.0000,0.0288 -11.250,-0.9334,0.05800,0.05207,-0.0204,1.0000,0.0288 -11.000,-0.9521,0.05385,0.04765,-0.0210,1.0000,0.0290 -10.750,-0.9661,0.05034,0.04385,-0.0198,1.0000,0.0292 -10.500,-0.9723,0.04681,0.03991,-0.0188,1.0000,0.0296 -10.250,-0.9706,0.04353,0.03632,-0.0178,1.0000,0.0302 -10.000,-0.9606,0.04129,0.03397,-0.0170,1.0000,0.0312 -9.750,-0.9482,0.03956,0.03211,-0.0163,1.0000,0.0328 -9.500,-0.9353,0.03756,0.02985,-0.0154,1.0000,0.0347 -9.250,-0.9206,0.03531,0.02724,-0.0145,1.0000,0.0366 -9.000,-0.9035,0.03318,0.02472,-0.0135,1.0000,0.0381 -8.750,-0.8859,0.03133,0.02284,-0.0128,1.0000,0.0404 -8.500,-0.8664,0.03002,0.02143,-0.0122,1.0000,0.0431 -8.250,-0.8459,0.02852,0.01972,-0.0114,1.0000,0.0459 -8.000,-0.8247,0.02707,0.01805,-0.0105,1.0000,0.0486 -7.750,-0.8046,0.02577,0.01679,-0.0099,1.0000,0.0522 -7.500,-0.7830,0.02465,0.01554,-0.0091,1.0000,0.0562 -7.250,-0.7611,0.02351,0.01426,-0.0083,1.0000,0.0600 -7.000,-0.7402,0.02244,0.01322,-0.0075,1.0000,0.0654 -6.750,-0.7176,0.02154,0.01218,-0.0068,1.0000,0.0718 -6.500,-0.6964,0.02050,0.01121,-0.0060,1.0000,0.0788 -6.250,-0.6741,0.01962,0.01032,-0.0053,1.0000,0.0893 -6.000,-0.6515,0.01877,0.00950,-0.0046,1.0000,0.1034 -5.750,-0.6286,0.01797,0.00875,-0.0040,1.0000,0.1224 -5.500,-0.6058,0.01720,0.00810,-0.0034,1.0000,0.1484 -5.250,-0.5826,0.01649,0.00749,-0.0029,1.0000,0.1803 -5.000,-0.5595,0.01579,0.00696,-0.0023,1.0000,0.2181 -4.750,-0.5366,0.01511,0.00649,-0.0017,1.0000,0.2638 -4.500,-0.5137,0.01449,0.00613,-0.0010,1.0000,0.3168 -4.250,-0.4905,0.01399,0.00583,-0.0003,1.0000,0.3707 -4.000,-0.4670,0.01361,0.00564,0.0006,1.0000,0.4192 -3.750,-0.4432,0.01334,0.00551,0.0014,1.0000,0.4614 -3.500,-0.4192,0.01316,0.00542,0.0023,1.0000,0.4964 -3.250,-0.3950,0.01302,0.00532,0.0032,1.0000,0.5261 -3.000,-0.3709,0.01291,0.00524,0.0040,1.0000,0.5519 -2.750,-0.3475,0.01282,0.00519,0.0049,1.0000,0.5737 -2.500,-0.3107,0.01277,0.00511,0.0030,0.9721,0.5970 -2.250,-0.2708,0.01275,0.00508,0.0007,0.9343,0.6175 -2.000,-0.2313,0.01273,0.00500,-0.0014,0.9004,0.6365 -1.750,-0.1954,0.01272,0.00490,-0.0026,0.8709,0.6537 -1.500,-0.1641,0.01273,0.00482,-0.0029,0.8460,0.6698 -1.250,-0.1356,0.01274,0.00476,-0.0025,0.8247,0.6853 -1.000,-0.1084,0.01275,0.00471,-0.0020,0.8068,0.7001 -0.750,-0.0814,0.01275,0.00468,-0.0014,0.7909,0.7134 -0.500,-0.0543,0.01274,0.00465,-0.0009,0.7765,0.7256 -0.250,-0.0271,0.01273,0.00463,-0.0004,0.7629,0.7377 0.000,0.0000,0.01273,0.00462,0.0000,0.7500,0.7500 0.250,0.0271,0.01273,0.00462,0.0004,0.7377,0.7629 0.500,0.0543,0.01274,0.00465,0.0009,0.7256,0.7765 0.750,0.0814,0.01275,0.00468,0.0014,0.7134,0.7909 1.000,0.1084,0.01275,0.00471,0.0020,0.7001,0.8068 1.250,0.1356,0.01274,0.00476,0.0025,0.6853,0.8248 1.500,0.1641,0.01273,0.00482,0.0029,0.6698,0.8460 1.750,0.1954,0.01272,0.00490,0.0026,0.6538,0.8709 2.000,0.2313,0.01273,0.00500,0.0014,0.6365,0.9004 2.250,0.2708,0.01275,0.00508,-0.0007,0.6175,0.9344 2.500,0.3107,0.01277,0.00511,-0.0030,0.5971,0.9722 2.750,0.3474,0.01282,0.00519,-0.0049,0.5737,1.0000 3.000,0.3708,0.01291,0.00524,-0.0040,0.5519,1.0000 3.250,0.3949,0.01302,0.00532,-0.0032,0.5260,1.0000 3.500,0.4191,0.01316,0.00542,-0.0023,0.4963,1.0000 3.750,0.4431,0.01334,0.00550,-0.0014,0.4613,1.0000 4.000,0.4670,0.01361,0.00564,-0.0006,0.4192,1.0000 4.250,0.4905,0.01399,0.00583,0.0003,0.3708,1.0000 4.500,0.5136,0.01449,0.00613,0.0010,0.3167,1.0000 4.750,0.5365,0.01511,0.00649,0.0017,0.2638,1.0000 5.000,0.5595,0.01579,0.00696,0.0023,0.2181,1.0000 5.250,0.5826,0.01649,0.00749,0.0029,0.1804,1.0000 5.500,0.6058,0.01720,0.00810,0.0034,0.1484,1.0000 5.750,0.6287,0.01797,0.00875,0.0040,0.1224,1.0000 6.000,0.6515,0.01877,0.00950,0.0046,0.1033,1.0000 6.250,0.6741,0.01962,0.01032,0.0053,0.0893,1.0000 6.500,0.6964,0.02050,0.01121,0.0060,0.0788,1.0000 6.750,0.7177,0.02154,0.01219,0.0068,0.0717,1.0000 7.000,0.7403,0.02244,0.01322,0.0075,0.0653,1.0000 7.250,0.7612,0.02352,0.01426,0.0082,0.0600,1.0000 7.500,0.7832,0.02465,0.01554,0.0091,0.0562,1.0000 7.750,0.8048,0.02577,0.01679,0.0098,0.0521,1.0000 8.000,0.8248,0.02708,0.01806,0.0105,0.0486,1.0000 8.250,0.8461,0.02852,0.01973,0.0113,0.0459,1.0000 8.500,0.8666,0.03003,0.02144,0.0121,0.0431,1.0000 8.750,0.8861,0.03134,0.02284,0.0128,0.0403,1.0000 9.000,0.9038,0.03319,0.02473,0.0135,0.0381,1.0000 9.250,0.9208,0.03533,0.02727,0.0144,0.0366,1.0000 9.500,0.9355,0.03757,0.02987,0.0153,0.0347,1.0000 9.750,0.9485,0.03960,0.03216,0.0162,0.0328,1.0000 10.000,0.9609,0.04133,0.03402,0.0170,0.0313,1.0000 10.250,0.9709,0.04355,0.03634,0.0177,0.0302,1.0000 10.500,0.9729,0.04682,0.03991,0.0187,0.0296,1.0000 10.750,0.9663,0.05040,0.04391,0.0197,0.0292,1.0000 11.000,0.9525,0.05387,0.04768,0.0209,0.0290,1.0000 11.250,0.9343,0.05801,0.05207,0.0203,0.0289,1.0000 11.500,0.9145,0.06309,0.05737,0.0177,0.0289,1.0000 11.750,0.8913,0.06948,0.06396,0.0134,0.0289,1.0000 12.000,0.8682,0.07687,0.07151,0.0080,0.0292,1.0000 12.250,0.8400,0.08650,0.08126,0.0007,0.0294,1.0000 12.500,0.8136,0.09706,0.09188,-0.0066,0.0298,1.0000