Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh25-il-50000-n5 Airfoil,mh25-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,32.897 Max Cl/Cd alpha,5.5 Url,http://airfoiltools.com/polar/csv?polar=xf-mh25-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.4768,0.09996,0.09299,-0.0380,1.0000,0.0385 -9.250,-0.4824,0.09629,0.08939,-0.0386,1.0000,0.0375 -9.000,-0.4906,0.09237,0.08556,-0.0395,1.0000,0.0367 -8.750,-0.5014,0.08836,0.08161,-0.0407,1.0000,0.0358 -8.500,-0.5172,0.08446,0.07778,-0.0410,1.0000,0.0352 -8.250,-0.5349,0.08144,0.07481,-0.0394,1.0000,0.0345 -8.000,-0.5534,0.07838,0.07176,-0.0370,1.0000,0.0340 -7.750,-0.5712,0.07454,0.06787,-0.0349,1.0000,0.0327 -7.500,-0.5870,0.07067,0.06385,-0.0323,1.0000,0.0318 -7.000,-0.6012,0.06457,0.05718,-0.0264,1.0000,0.0303 -6.750,-0.6029,0.06125,0.05374,-0.0237,1.0000,0.0300 -6.500,-0.6039,0.05790,0.05017,-0.0209,1.0000,0.0298 -6.250,-0.6023,0.05468,0.04672,-0.0181,1.0000,0.0295 -6.000,-0.5985,0.05153,0.04328,-0.0154,1.0000,0.0293 -5.750,-0.5928,0.04832,0.03971,-0.0125,1.0000,0.0292 -5.500,-0.5842,0.04532,0.03634,-0.0099,1.0000,0.0291 -5.250,-0.5730,0.04244,0.03302,-0.0073,1.0000,0.0291 -5.000,-0.5591,0.03980,0.02994,-0.0050,1.0000,0.0292 -4.750,-0.5424,0.03723,0.02688,-0.0028,1.0000,0.0295 -4.500,-0.5229,0.03496,0.02412,-0.0008,1.0000,0.0301 -4.250,-0.5025,0.03255,0.02145,0.0007,1.0000,0.0315 -4.000,-0.4822,0.03097,0.01971,0.0019,1.0000,0.0354 -3.750,-0.4587,0.02956,0.01796,0.0033,1.0000,0.0411 -3.500,-0.4342,0.02797,0.01611,0.0045,1.0000,0.0450 -3.250,-0.4101,0.02674,0.01469,0.0056,1.0000,0.0563 -3.000,-0.3870,0.02549,0.01342,0.0066,1.0000,0.0753 -2.750,-0.3099,0.02122,0.01323,0.0000,1.0000,0.8436 -2.500,-0.1432,0.02278,0.01322,-0.0249,1.0000,1.0000 -2.250,-0.1325,0.02264,0.01282,-0.0223,1.0000,1.0000 -2.000,-0.1216,0.02254,0.01249,-0.0199,1.0000,1.0000 -1.750,-0.1103,0.02247,0.01221,-0.0174,1.0000,1.0000 -1.500,-0.0988,0.02244,0.01199,-0.0150,1.0000,1.0000 -1.250,-0.0871,0.02243,0.01180,-0.0126,1.0000,1.0000 -1.000,-0.0753,0.02245,0.01166,-0.0102,1.0000,1.0000 -0.750,-0.0634,0.02250,0.01153,-0.0079,1.0000,1.0000 -0.500,-0.0515,0.02258,0.01148,-0.0056,1.0000,1.0000 -0.250,-0.0394,0.02269,0.01147,-0.0033,1.0000,1.0000 0.000,-0.0274,0.02283,0.01151,-0.0011,1.0000,1.0000 0.250,-0.0019,0.02311,0.01168,-0.0017,0.9960,1.0000 0.500,0.0369,0.02353,0.01198,-0.0048,0.9871,1.0000 0.750,0.0754,0.02397,0.01234,-0.0079,0.9780,1.0000 1.000,0.1153,0.02443,0.01276,-0.0111,0.9690,1.0000 1.250,0.1519,0.02477,0.01308,-0.0136,0.9583,1.0000 1.500,0.1877,0.02507,0.01339,-0.0159,0.9470,1.0000 1.750,0.2236,0.02533,0.01368,-0.0181,0.9353,1.0000 2.000,0.2594,0.02554,0.01396,-0.0202,0.9229,1.0000 2.250,0.2946,0.02570,0.01421,-0.0221,0.9098,1.0000 2.500,0.3288,0.02577,0.01438,-0.0236,0.8958,1.0000 2.750,0.3626,0.02577,0.01449,-0.0249,0.8809,1.0000 3.000,0.3970,0.02569,0.01454,-0.0261,0.8654,1.0000 3.250,0.4303,0.02551,0.01460,-0.0270,0.8487,1.0000 3.500,0.4565,0.02531,0.01457,-0.0264,0.8288,1.0000 3.750,0.4931,0.02491,0.01438,-0.0274,0.8109,1.0000 4.000,0.5203,0.02455,0.01421,-0.0267,0.7888,1.0000 4.250,0.5545,0.02397,0.01395,-0.0268,0.7666,1.0000 4.500,0.5889,0.02342,0.01364,-0.0268,0.7396,1.0000 4.750,0.6264,0.02286,0.01331,-0.0273,0.7054,1.0000 5.000,0.6687,0.02226,0.01289,-0.0283,0.6604,1.0000 5.250,0.7045,0.02203,0.01277,-0.0284,0.6016,1.0000 5.500,0.7313,0.02223,0.01283,-0.0271,0.5361,1.0000 5.750,0.7477,0.02276,0.01317,-0.0244,0.4732,1.0000 6.000,0.7592,0.02348,0.01367,-0.0210,0.4140,1.0000 6.250,0.7680,0.02431,0.01429,-0.0175,0.3584,1.0000 6.500,0.7756,0.02525,0.01501,-0.0140,0.3060,1.0000 6.750,0.7835,0.02626,0.01585,-0.0107,0.2572,1.0000 7.000,0.7913,0.02740,0.01680,-0.0075,0.2127,1.0000 7.250,0.7998,0.02865,0.01787,-0.0046,0.1729,1.0000 7.500,0.8096,0.03001,0.01909,-0.0019,0.1400,1.0000 7.750,0.8207,0.03148,0.02047,0.0005,0.1140,1.0000 8.000,0.8346,0.03307,0.02223,0.0026,0.0952,1.0000 8.250,0.8451,0.03454,0.02369,0.0050,0.0798,1.0000 8.500,0.8647,0.03651,0.02586,0.0064,0.0693,1.0000 8.750,0.8856,0.03875,0.02829,0.0075,0.0614,1.0000 9.000,0.8947,0.04047,0.03003,0.0098,0.0537,1.0000 9.250,0.9134,0.04315,0.03320,0.0113,0.0485,1.0000 9.500,0.9270,0.04601,0.03642,0.0132,0.0452,1.0000 9.750,0.9354,0.04884,0.03949,0.0154,0.0429,1.0000 10.000,0.9371,0.05194,0.04280,0.0182,0.0406,1.0000 10.250,0.9275,0.05463,0.04598,0.0226,0.0387,1.0000 10.500,0.9169,0.05739,0.04908,0.0265,0.0373,1.0000 10.750,0.9037,0.06030,0.05228,0.0300,0.0360,1.0000 11.000,0.8893,0.06354,0.05578,0.0327,0.0354,1.0000 11.250,0.8724,0.06711,0.05957,0.0346,0.0349,1.0000 11.500,0.8528,0.07129,0.06397,0.0356,0.0351,1.0000 11.750,0.8314,0.07606,0.06892,0.0352,0.0354,1.0000 12.000,0.8081,0.08185,0.07486,0.0333,0.0360,1.0000 12.250,0.7846,0.08880,0.08192,0.0297,0.0371,1.0000 12.500,0.7664,0.09598,0.08913,0.0257,0.0386,1.0000