Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca22112-jf-100000-n5 Airfoil,naca22112-jf Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,36.8216 Max Cl/Cd alpha,6.75 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca22112-jf-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.250,-0.4437,0.13770,0.13259,-0.0010,1.0000,0.0634 -13.000,-0.4465,0.13469,0.12958,-0.0023,1.0000,0.0656 -12.250,-0.6184,0.12124,0.11581,-0.0008,1.0000,0.0406 -12.000,-0.6135,0.11767,0.11225,-0.0012,1.0000,0.0403 -11.750,-0.5995,0.11774,0.11235,0.0011,1.0000,0.0439 -11.500,-0.6103,0.10905,0.10368,-0.0038,1.0000,0.0390 -11.000,-0.6867,0.08036,0.07476,-0.0267,1.0000,0.0342 -10.750,-0.6995,0.07554,0.06986,-0.0290,1.0000,0.0340 -10.500,-0.7148,0.07118,0.06539,-0.0302,1.0000,0.0338 -10.250,-0.7306,0.06739,0.06148,-0.0297,1.0000,0.0337 -10.000,-0.7445,0.06393,0.05786,-0.0281,1.0000,0.0336 -9.750,-0.7534,0.06035,0.05406,-0.0266,1.0000,0.0335 -9.500,-0.7585,0.05684,0.05030,-0.0248,1.0000,0.0334 -9.250,-0.7601,0.05342,0.04659,-0.0229,1.0000,0.0334 -9.000,-0.7585,0.05015,0.04298,-0.0208,1.0000,0.0334 -8.750,-0.7541,0.04703,0.03950,-0.0187,1.0000,0.0336 -8.500,-0.7502,0.04405,0.03593,-0.0159,1.0000,0.0342 -8.250,-0.7352,0.04191,0.03375,-0.0148,1.0000,0.0350 -8.000,-0.7197,0.04013,0.03186,-0.0135,1.0000,0.0359 -7.750,-0.7048,0.03815,0.02965,-0.0118,1.0000,0.0367 -7.500,-0.6891,0.03607,0.02730,-0.0100,1.0000,0.0371 -7.250,-0.6720,0.03412,0.02506,-0.0083,1.0000,0.0376 -7.000,-0.6537,0.03233,0.02301,-0.0066,1.0000,0.0382 -6.750,-0.6345,0.03074,0.02115,-0.0050,1.0000,0.0392 -6.500,-0.6151,0.02950,0.01954,-0.0032,1.0000,0.0407 -6.250,-0.5942,0.02799,0.01807,-0.0022,1.0000,0.0420 -6.000,-0.5727,0.02679,0.01683,-0.0010,1.0000,0.0431 -5.750,-0.5510,0.02563,0.01563,0.0002,1.0000,0.0441 -5.500,-0.5294,0.02458,0.01452,0.0015,1.0000,0.0454 -5.250,-0.5083,0.02374,0.01358,0.0029,1.0000,0.0475 -5.000,-0.4880,0.02278,0.01264,0.0043,1.0000,0.0494 -4.750,-0.4687,0.02190,0.01185,0.0058,1.0000,0.0512 -4.500,-0.4500,0.02114,0.01113,0.0074,1.0000,0.0529 -4.250,-0.4317,0.02051,0.01050,0.0091,1.0000,0.0552 -4.000,-0.4134,0.02001,0.00997,0.0108,1.0000,0.0580 -3.750,-0.3916,0.01924,0.00926,0.0115,0.9979,0.0612 -3.500,-0.3531,0.01859,0.00856,0.0091,0.9894,0.0659 -3.250,-0.3145,0.01793,0.00787,0.0067,0.9804,0.0730 -3.000,-0.2750,0.01736,0.00726,0.0043,0.9710,0.0830 -2.750,-0.2400,0.01634,0.00660,0.0025,0.9599,0.1285 -2.500,-0.2165,0.01420,0.00633,0.0025,0.9481,0.5070 -2.250,-0.1855,0.01363,0.00635,0.0026,0.9356,0.6428 -2.000,-0.1517,0.01341,0.00645,0.0026,0.9227,0.7296 -1.750,-0.1174,0.01338,0.00656,0.0027,0.9080,0.7921 -1.500,-0.0817,0.01353,0.00679,0.0028,0.8918,0.8449 -1.250,-0.0454,0.01365,0.00686,0.0024,0.8731,0.8760 -1.000,-0.0101,0.01367,0.00677,0.0017,0.8514,0.8922 -0.750,0.0273,0.01369,0.00667,0.0006,0.8280,0.9047 -0.500,0.0635,0.01372,0.00656,-0.0003,0.8014,0.9166 -0.250,0.0978,0.01376,0.00644,-0.0008,0.7716,0.9285 0.000,0.1304,0.01382,0.00631,-0.0011,0.7371,0.9407 0.250,0.1696,0.01390,0.00619,-0.0029,0.6976,0.9485 0.500,0.2048,0.01401,0.00607,-0.0040,0.6593,0.9583 0.750,0.2422,0.01413,0.00598,-0.0057,0.6220,0.9669 1.000,0.2795,0.01425,0.00591,-0.0075,0.5862,0.9750 1.250,0.3157,0.01440,0.00587,-0.0092,0.5507,0.9836 1.500,0.3542,0.01453,0.00581,-0.0114,0.5143,0.9908 1.750,0.3921,0.01470,0.00578,-0.0137,0.4774,0.9977 2.000,0.4195,0.01487,0.00578,-0.0139,0.4448,1.0000 2.250,0.4414,0.01506,0.00582,-0.0129,0.4152,1.0000 2.500,0.4631,0.01529,0.00588,-0.0120,0.3862,1.0000 2.750,0.4846,0.01555,0.00599,-0.0110,0.3579,1.0000 3.000,0.5061,0.01583,0.00613,-0.0100,0.3310,1.0000 3.250,0.5272,0.01615,0.00630,-0.0089,0.3076,1.0000 3.500,0.5486,0.01647,0.00653,-0.0079,0.2867,1.0000 3.750,0.5697,0.01682,0.00677,-0.0068,0.2686,1.0000 4.000,0.5907,0.01720,0.00705,-0.0057,0.2531,1.0000 4.250,0.6117,0.01759,0.00735,-0.0046,0.2403,1.0000 4.500,0.6326,0.01800,0.00770,-0.0035,0.2297,1.0000 4.750,0.6539,0.01840,0.00807,-0.0024,0.2202,1.0000 5.000,0.6745,0.01887,0.00844,-0.0012,0.2124,1.0000 5.250,0.6961,0.01928,0.00889,-0.0002,0.2044,1.0000 5.500,0.7168,0.01977,0.00931,0.0010,0.1981,1.0000 5.750,0.7384,0.02024,0.00981,0.0020,0.1922,1.0000 6.000,0.7597,0.02073,0.01032,0.0031,0.1864,1.0000 6.250,0.7804,0.02131,0.01081,0.0042,0.1816,1.0000 6.500,0.8022,0.02181,0.01142,0.0052,0.1763,1.0000 6.750,0.8237,0.02237,0.01200,0.0061,0.1717,1.0000 7.000,0.8450,0.02299,0.01258,0.0071,0.1677,1.0000 7.250,0.8667,0.02361,0.01330,0.0080,0.1634,1.0000 7.500,0.8883,0.02422,0.01401,0.0089,0.1589,1.0000 7.750,0.9098,0.02487,0.01468,0.0098,0.1550,1.0000 8.000,0.9314,0.02563,0.01539,0.0106,0.1516,1.0000 8.250,0.9524,0.02634,0.01632,0.0115,0.1475,1.0000 8.500,0.9733,0.02707,0.01718,0.0123,0.1435,1.0000 8.750,0.9943,0.02780,0.01793,0.0132,0.1401,1.0000 9.000,1.0153,0.02866,0.01878,0.0139,0.1369,1.0000 9.250,1.0344,0.02955,0.01995,0.0149,0.1330,1.0000 9.500,1.0535,0.03040,0.02097,0.0159,0.1292,1.0000 9.750,1.0731,0.03119,0.02181,0.0168,0.1260,1.0000 10.000,1.0928,0.03211,0.02271,0.0175,0.1231,1.0000 10.250,1.1079,0.03323,0.02420,0.0189,0.1193,1.0000 10.500,1.1238,0.03425,0.02540,0.0201,0.1158,1.0000 10.750,1.1407,0.03506,0.02628,0.0211,0.1126,1.0000 11.000,1.1577,0.03598,0.02720,0.0221,0.1099,1.0000 11.250,1.1665,0.03747,0.02907,0.0238,0.1064,1.0000 11.500,1.1767,0.03868,0.03051,0.0254,0.1031,1.0000 11.750,1.1888,0.03958,0.03147,0.0267,0.1003,1.0000 12.000,1.2022,0.04045,0.03230,0.0279,0.0980,1.0000 12.250,1.1980,0.04245,0.03469,0.0306,0.0952,1.0000 12.500,1.1954,0.04430,0.03679,0.0327,0.0926,1.0000 12.750,1.1962,0.04594,0.03858,0.0341,0.0902,1.0000 13.000,1.2010,0.04728,0.03996,0.0351,0.0881,1.0000 13.250,1.2021,0.04919,0.04194,0.0358,0.0862,1.0000 13.500,1.1846,0.05327,0.04638,0.0357,0.0843,1.0000 13.750,1.1658,0.05798,0.05137,0.0343,0.0827,1.0000 14.000,1.1436,0.06368,0.05732,0.0318,0.0814,1.0000 14.250,1.1086,0.07202,0.06591,0.0270,0.0806,1.0000