Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n5h10-il-200000-n5 Airfoil,n5h10-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,56.1905 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-n5h10-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.4955,0.09001,0.08648,-0.0160,0.8476,0.0147 -9.000,-0.4990,0.08556,0.08204,-0.0186,0.8419,0.0143 -8.750,-0.5073,0.08078,0.07726,-0.0218,0.8363,0.0142 -8.500,-0.5169,0.07639,0.07286,-0.0242,0.8297,0.0139 -8.250,-0.5289,0.07226,0.06868,-0.0247,0.8242,0.0137 -8.000,-0.5351,0.06753,0.06387,-0.0257,0.8187,0.0136 -7.750,-0.5386,0.06261,0.05882,-0.0262,0.8137,0.0134 -7.250,-0.5373,0.05254,0.04834,-0.0254,0.8046,0.0133 -7.000,-0.5323,0.04775,0.04327,-0.0242,0.7999,0.0135 -6.750,-0.5249,0.04330,0.03848,-0.0225,0.7959,0.0138 -6.500,-0.5135,0.03917,0.03401,-0.0209,0.7910,0.0149 -6.250,-0.5028,0.03425,0.02857,-0.0185,0.7864,0.0158 -6.000,-0.4904,0.02933,0.02295,-0.0158,0.7826,0.0165 -5.750,-0.4717,0.02607,0.01906,-0.0140,0.7785,0.0173 -5.500,-0.4511,0.02391,0.01658,-0.0130,0.7737,0.0185 -5.250,-0.4275,0.02355,0.01614,-0.0126,0.7693,0.0202 -5.000,-0.4032,0.02232,0.01463,-0.0119,0.7652,0.0224 -4.750,-0.3775,0.02072,0.01269,-0.0112,0.7600,0.0245 -4.500,-0.3513,0.02018,0.01187,-0.0107,0.7556,0.0267 -4.250,-0.3265,0.01858,0.01013,-0.0103,0.7523,0.0298 -4.000,-0.3000,0.01782,0.00928,-0.0101,0.7471,0.0326 -3.750,-0.2737,0.01726,0.00859,-0.0097,0.7425,0.0362 -3.500,-0.2475,0.01666,0.00782,-0.0093,0.7387,0.0379 -3.250,-0.2225,0.01572,0.00688,-0.0089,0.7338,0.0415 -3.000,-0.1971,0.01523,0.00636,-0.0085,0.7291,0.0443 -2.750,-0.1720,0.01475,0.00581,-0.0079,0.7253,0.0463 -2.500,-0.1467,0.01435,0.00533,-0.0074,0.7214,0.0482 -2.250,-0.1210,0.01405,0.00497,-0.0071,0.7165,0.0504 -2.000,-0.0961,0.01366,0.00456,-0.0065,0.7124,0.0544 -1.750,-0.0707,0.01338,0.00421,-0.0060,0.7091,0.0582 -1.500,-0.0446,0.01316,0.00395,-0.0057,0.7041,0.0645 -1.250,-0.0196,0.01282,0.00369,-0.0052,0.7000,0.0874 -1.000,-0.0002,0.01194,0.00346,-0.0040,0.6967,0.2683 -0.750,0.0031,0.01025,0.00389,0.0019,0.6935,0.8453 -0.500,0.0248,0.01046,0.00407,0.0038,0.6892,0.8882 -0.250,0.0597,0.01073,0.00429,0.0033,0.6855,0.9142 0.000,0.1397,0.01145,0.00489,-0.0061,0.6827,0.9463 0.250,0.2044,0.01174,0.00509,-0.0133,0.6786,0.9618 0.500,0.2357,0.01172,0.00501,-0.0142,0.6733,0.9637 0.750,0.2656,0.01167,0.00491,-0.0148,0.6690,0.9650 1.000,0.2920,0.01163,0.00482,-0.0147,0.6653,0.9656 1.250,0.3181,0.01161,0.00481,-0.0146,0.6605,0.9661 1.500,0.3446,0.01158,0.00476,-0.0144,0.6558,0.9668 1.750,0.3710,0.01156,0.00470,-0.0143,0.6523,0.9675 2.000,0.3971,0.01157,0.00476,-0.0142,0.6479,0.9682 2.250,0.4227,0.01157,0.00477,-0.0139,0.6428,0.9688 2.500,0.4482,0.01155,0.00473,-0.0136,0.6380,0.9695 2.750,0.4736,0.01154,0.00479,-0.0133,0.6301,0.9702 3.000,0.4986,0.01151,0.00474,-0.0127,0.6217,0.9710 3.250,0.5230,0.01146,0.00468,-0.0121,0.6079,0.9719 3.500,0.5472,0.01142,0.00467,-0.0114,0.5895,0.9730 3.750,0.5708,0.01140,0.00464,-0.0106,0.5685,0.9744 4.000,0.5961,0.01142,0.00467,-0.0103,0.5476,0.9754 4.250,0.6229,0.01146,0.00476,-0.0103,0.5262,0.9761 4.500,0.6490,0.01155,0.00481,-0.0101,0.4900,0.9769 4.750,0.6715,0.01199,0.00488,-0.0096,0.3956,0.9781 5.000,0.6912,0.01293,0.00538,-0.0090,0.3105,0.9796 5.250,0.7093,0.01408,0.00605,-0.0084,0.1926,0.9815 5.500,0.7282,0.01506,0.00673,-0.0078,0.1348,0.9835 5.750,0.7492,0.01566,0.00726,-0.0072,0.1040,0.9854 6.000,0.7727,0.01635,0.00785,-0.0073,0.0716,0.9869 6.250,0.7966,0.01708,0.00848,-0.0074,0.0506,0.9887 6.500,0.8198,0.01781,0.00922,-0.0075,0.0434,0.9909 6.750,0.8424,0.01846,0.00999,-0.0073,0.0396,0.9932 7.000,0.8637,0.01930,0.01090,-0.0071,0.0354,0.9956 7.250,0.8841,0.02037,0.01207,-0.0069,0.0318,0.9984 7.500,0.9020,0.02113,0.01296,-0.0060,0.0290,1.0000 7.750,0.9076,0.02179,0.01369,-0.0027,0.0263,1.0000 8.000,0.9082,0.02260,0.01458,0.0014,0.0245,1.0000 8.250,0.9039,0.02385,0.01584,0.0061,0.0229,1.0000 8.500,0.9123,0.02449,0.01658,0.0089,0.0217,1.0000 8.750,0.9194,0.02521,0.01740,0.0118,0.0200,1.0000 9.000,0.9264,0.02610,0.01837,0.0146,0.0182,1.0000 9.250,0.9352,0.02715,0.01949,0.0168,0.0171,1.0000 9.500,0.9451,0.02829,0.02069,0.0187,0.0161,1.0000 9.750,0.9549,0.02963,0.02208,0.0204,0.0151,1.0000 10.000,0.9671,0.03120,0.02377,0.0220,0.0140,1.0000 10.250,0.9800,0.03248,0.02522,0.0234,0.0131,1.0000 10.500,0.9924,0.03413,0.02710,0.0248,0.0124,1.0000 10.750,1.0028,0.03586,0.02903,0.0262,0.0118,1.0000 11.000,1.0109,0.03776,0.03112,0.0276,0.0113,1.0000 11.250,1.0167,0.03975,0.03330,0.0289,0.0109,1.0000 11.500,1.0204,0.04183,0.03556,0.0302,0.0106,1.0000 11.750,1.0221,0.04393,0.03781,0.0313,0.0103,1.0000 12.000,1.0210,0.04655,0.04063,0.0323,0.0101,1.0000 12.250,1.0163,0.04959,0.04386,0.0332,0.0099,1.0000 12.500,1.0074,0.05299,0.04749,0.0337,0.0096,1.0000 12.750,0.9954,0.05702,0.05182,0.0339,0.0094,1.0000 13.000,0.9829,0.06123,0.05626,0.0336,0.0094,1.0000 13.250,0.9680,0.06594,0.06122,0.0327,0.0093,1.0000 13.500,0.9493,0.07150,0.06704,0.0309,0.0089,1.0000 13.750,0.9333,0.07700,0.07268,0.0287,0.0093,1.0000 14.000,0.9126,0.08386,0.07973,0.0254,0.0093,1.0000 14.250,0.8921,0.09160,0.08765,0.0210,0.0093,1.0000 14.500,0.8738,0.09966,0.09583,0.0163,0.0095,1.0000 14.750,0.8532,0.10917,0.10543,0.0106,0.0097,1.0000