Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rae5212-il-100000-n5 Airfoil,rae5212-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,40.1997 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-rae5212-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.000,-0.5135,0.09284,0.08728,-0.0459,1.0000,0.0325 -10.750,-0.5277,0.08495,0.07942,-0.0501,1.0000,0.0320 -10.500,-0.5536,0.07603,0.07049,-0.0556,1.0000,0.0315 -10.250,-0.5829,0.06915,0.06354,-0.0593,1.0000,0.0310 -10.000,-0.6128,0.06402,0.05833,-0.0607,1.0000,0.0306 -9.750,-0.6429,0.06045,0.05468,-0.0594,1.0000,0.0305 -9.500,-0.6689,0.05746,0.05157,-0.0565,1.0000,0.0303 -9.250,-0.6872,0.05422,0.04815,-0.0538,1.0000,0.0302 -9.000,-0.6995,0.05115,0.04485,-0.0511,1.0000,0.0303 -8.750,-0.7070,0.04813,0.04158,-0.0485,1.0000,0.0304 -8.500,-0.7101,0.04524,0.03840,-0.0460,1.0000,0.0306 -8.250,-0.7092,0.04256,0.03540,-0.0436,1.0000,0.0311 -8.000,-0.7052,0.04006,0.03254,-0.0413,1.0000,0.0320 -7.750,-0.6990,0.03748,0.02947,-0.0391,1.0000,0.0331 -7.500,-0.6887,0.03525,0.02688,-0.0372,1.0000,0.0339 -7.250,-0.6749,0.03364,0.02515,-0.0356,1.0000,0.0346 -7.000,-0.6558,0.03203,0.02336,-0.0350,0.9990,0.0354 -6.750,-0.6257,0.03030,0.02140,-0.0362,0.9954,0.0365 -6.500,-0.5958,0.02875,0.01959,-0.0372,0.9918,0.0383 -6.250,-0.5657,0.02737,0.01794,-0.0380,0.9880,0.0406 -6.000,-0.5349,0.02625,0.01682,-0.0393,0.9846,0.0427 -5.750,-0.5058,0.02517,0.01566,-0.0399,0.9805,0.0447 -5.500,-0.4755,0.02427,0.01459,-0.0406,0.9761,0.0478 -5.250,-0.4447,0.02330,0.01372,-0.0418,0.9727,0.0511 -5.000,-0.4183,0.02251,0.01290,-0.0419,0.9675,0.0545 -4.750,-0.3892,0.02174,0.01210,-0.0426,0.9628,0.0590 -4.500,-0.3569,0.02106,0.01142,-0.0439,0.9592,0.0656 -4.250,-0.3329,0.02039,0.01075,-0.0436,0.9527,0.0725 -4.000,-0.3029,0.01974,0.01013,-0.0445,0.9482,0.0850 -3.750,-0.2710,0.01904,0.00953,-0.0459,0.9446,0.1102 -3.500,-0.2492,0.01804,0.00896,-0.0456,0.9376,0.1853 -3.250,-0.2270,0.01649,0.00889,-0.0456,0.9330,0.4688 -3.000,-0.1990,0.01665,0.00920,-0.0452,0.9280,0.5610 -2.750,-0.1728,0.01687,0.00937,-0.0446,0.9215,0.6021 -2.500,-0.1425,0.01727,0.00979,-0.0442,0.9173,0.6398 -2.250,-0.1192,0.01768,0.01024,-0.0424,0.9112,0.6720 -2.000,-0.0925,0.01784,0.01038,-0.0416,0.9056,0.6905 -1.750,-0.0578,0.01776,0.01016,-0.0430,0.9021,0.6987 -1.500,-0.0296,0.01770,0.01003,-0.0431,0.8965,0.7036 -1.250,-0.0007,0.01763,0.00990,-0.0433,0.8908,0.7089 -1.000,0.0347,0.01752,0.00969,-0.0449,0.8871,0.7149 -0.750,0.0718,0.01740,0.00952,-0.0466,0.8845,0.7194 -0.500,0.0928,0.01742,0.00952,-0.0454,0.8758,0.7243 -0.250,0.1276,0.01732,0.00938,-0.0468,0.8717,0.7299 0.000,0.1651,0.01719,0.00923,-0.0486,0.8687,0.7345 0.250,0.1872,0.01723,0.00928,-0.0475,0.8600,0.7392 0.500,0.2225,0.01710,0.00915,-0.0489,0.8551,0.7444 0.750,0.2548,0.01700,0.00905,-0.0497,0.8485,0.7496 1.000,0.2846,0.01689,0.00898,-0.0498,0.8406,0.7542 1.250,0.3234,0.01665,0.00876,-0.0515,0.8355,0.7594 1.500,0.3500,0.01655,0.00869,-0.0511,0.8237,0.7652 1.750,0.3809,0.01630,0.00849,-0.0510,0.8117,0.7699 2.000,0.4146,0.01600,0.00823,-0.0515,0.7989,0.7754 2.250,0.4449,0.01566,0.00789,-0.0512,0.7785,0.7814 2.500,0.4760,0.01523,0.00745,-0.0506,0.7503,0.7865 2.750,0.5040,0.01498,0.00715,-0.0498,0.7175,0.7926 3.000,0.5305,0.01486,0.00699,-0.0489,0.6851,0.7989 3.250,0.5556,0.01481,0.00694,-0.0479,0.6503,0.8057 3.500,0.5808,0.01483,0.00685,-0.0469,0.5989,0.8133 3.750,0.6038,0.01502,0.00671,-0.0454,0.5199,0.8202 4.250,0.6359,0.01632,0.00712,-0.0408,0.3428,0.8394 4.500,0.6511,0.01709,0.00752,-0.0387,0.2697,0.8518 4.750,0.6685,0.01780,0.00796,-0.0371,0.2135,0.8672 5.000,0.6885,0.01846,0.00845,-0.0360,0.1754,0.8880 5.250,0.7155,0.01908,0.00900,-0.0362,0.1513,0.9223 5.500,0.7436,0.01972,0.00957,-0.0369,0.1378,1.0000 6.000,0.7865,0.02107,0.01080,-0.0354,0.1227,1.0000 6.250,0.8075,0.02177,0.01143,-0.0346,0.1169,1.0000 6.500,0.8287,0.02251,0.01213,-0.0338,0.1124,1.0000 6.750,0.8508,0.02321,0.01287,-0.0330,0.1084,1.0000 7.000,0.8728,0.02396,0.01360,-0.0323,0.1049,1.0000 7.250,0.8944,0.02482,0.01440,-0.0316,0.1017,1.0000 7.500,0.9176,0.02567,0.01528,-0.0311,0.0988,1.0000 7.750,0.9411,0.02648,0.01618,-0.0307,0.0958,1.0000 8.000,0.9649,0.02739,0.01713,-0.0303,0.0934,1.0000 8.250,0.9885,0.02833,0.01810,-0.0299,0.0911,1.0000 8.500,1.0122,0.02938,0.01912,-0.0296,0.0888,1.0000 8.750,1.0365,0.03054,0.02034,-0.0294,0.0866,1.0000 9.000,1.0592,0.03163,0.02162,-0.0289,0.0845,1.0000 9.250,1.0819,0.03284,0.02301,-0.0284,0.0826,1.0000 9.500,1.1039,0.03411,0.02443,-0.0278,0.0808,1.0000 9.750,1.1248,0.03537,0.02579,-0.0272,0.0791,1.0000 10.000,1.1453,0.03663,0.02711,-0.0266,0.0774,1.0000 10.250,1.1678,0.03829,0.02876,-0.0265,0.0756,1.0000 10.500,1.1817,0.03987,0.03067,-0.0248,0.0742,1.0000 10.750,1.1943,0.04169,0.03283,-0.0232,0.0729,1.0000 11.000,1.2044,0.04354,0.03498,-0.0213,0.0714,1.0000 11.250,1.2129,0.04536,0.03706,-0.0193,0.0699,1.0000 11.500,1.2195,0.04705,0.03897,-0.0172,0.0684,1.0000 11.750,1.2250,0.04868,0.04075,-0.0149,0.0671,1.0000 12.000,1.2304,0.05035,0.04255,-0.0128,0.0660,1.0000 12.250,1.2385,0.05211,0.04437,-0.0113,0.0649,1.0000 12.500,1.2368,0.05455,0.04699,-0.0090,0.0639,1.0000 12.750,1.2182,0.05740,0.05021,-0.0055,0.0632,1.0000 13.000,1.1971,0.06084,0.05400,-0.0028,0.0625,1.0000 13.250,1.1736,0.06487,0.05834,-0.0012,0.0618,1.0000 13.500,1.1467,0.06975,0.06351,-0.0007,0.0614,1.0000 13.750,1.1138,0.07591,0.06995,-0.0017,0.0612,1.0000 14.000,1.0709,0.08444,0.07874,-0.0053,0.0613,1.0000 14.250,1.0041,0.09933,0.09389,-0.0146,0.0622,1.0000