Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n5h10-il-100000 Airfoil,n5h10-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,48.4379 Max Cl/Cd alpha,5.5 Url,http://airfoiltools.com/polar/csv?polar=xf-n5h10-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.4097,0.10541,0.10134,-0.0111,1.0000,0.0853 -9.750,-0.4216,0.10184,0.09782,-0.0155,1.0000,0.0869 -9.500,-0.4359,0.09800,0.09404,-0.0206,1.0000,0.0875 -9.250,-0.4048,0.09238,0.08839,-0.0166,1.0000,0.0925 -9.000,-0.4023,0.08832,0.08435,-0.0183,1.0000,0.0965 -8.750,-0.4114,0.08397,0.08005,-0.0224,1.0000,0.0999 -8.500,-0.4311,0.07935,0.07550,-0.0290,1.0000,0.1012 -8.250,-0.5021,0.08375,0.07965,-0.0226,1.0000,0.0940 -8.000,-0.5068,0.08021,0.07612,-0.0249,1.0000,0.0976 -7.750,-0.5232,0.07731,0.07310,-0.0296,1.0000,0.1013 -7.500,-0.5284,0.07320,0.06895,-0.0305,1.0000,0.1032 -7.250,-0.5135,0.06974,0.06562,-0.0283,1.0000,0.1073 -7.000,-0.5294,0.06848,0.06438,-0.0245,1.0000,0.1093 -6.750,-0.5273,0.06472,0.06027,-0.0284,0.9873,0.1178 -6.500,-0.4997,0.06055,0.05612,-0.0306,0.9806,0.1271 -6.250,-0.4770,0.05624,0.05167,-0.0336,0.9725,0.1386 -6.000,-0.4596,0.05336,0.04834,-0.0365,0.9627,0.1609 -5.750,-0.4313,0.04926,0.04438,-0.0382,0.9571,0.1799 -5.500,-0.4114,0.04663,0.04166,-0.0386,0.9490,0.2092 -5.250,-0.3462,0.02735,0.02282,-0.0418,0.9269,0.2574 -5.000,-0.3758,0.04186,0.03686,-0.0373,0.9337,0.2819 -4.750,-0.3246,0.03288,0.02538,-0.0393,0.9265,0.0986 -4.500,-0.3027,0.03039,0.02247,-0.0380,0.9182,0.0946 -4.250,-0.2714,0.02867,0.01992,-0.0370,0.9123,0.0872 -4.000,-0.2467,0.02674,0.01771,-0.0362,0.9051,0.0865 -3.750,-0.2177,0.02499,0.01572,-0.0363,0.8996,0.0905 -3.500,-0.1899,0.02377,0.01436,-0.0362,0.8933,0.0930 -3.250,-0.1598,0.02272,0.01319,-0.0363,0.8874,0.0959 -3.000,-0.1320,0.02214,0.01245,-0.0361,0.8818,0.1025 -2.750,-0.1059,0.02118,0.01164,-0.0360,0.8759,0.1085 -2.500,0.1400,0.01674,0.00992,-0.0705,0.8897,1.0000 -2.250,0.1623,0.01696,0.00992,-0.0698,0.8833,1.0000 -2.000,0.1856,0.01715,0.00996,-0.0697,0.8762,1.0000 -1.750,0.2068,0.01741,0.01007,-0.0687,0.8702,1.0000 -1.500,0.2308,0.01764,0.01018,-0.0688,0.8636,1.0000 -1.250,0.2533,0.01791,0.01034,-0.0682,0.8582,1.0000 -1.000,0.2766,0.01822,0.01057,-0.0681,0.8529,1.0000 -0.750,0.2996,0.01852,0.01081,-0.0678,0.8470,1.0000 -0.500,0.3211,0.01885,0.01106,-0.0669,0.8425,1.0000 -0.250,0.3456,0.01923,0.01142,-0.0673,0.8371,1.0000 0.000,0.3683,0.01960,0.01177,-0.0671,0.8323,1.0000 0.250,0.3899,0.01998,0.01211,-0.0661,0.8281,1.0000 0.500,0.4127,0.02044,0.01260,-0.0663,0.8219,1.0000 0.750,0.4341,0.02083,0.01298,-0.0655,0.8167,1.0000 1.000,0.4549,0.02128,0.01346,-0.0648,0.8103,1.0000 1.250,0.4752,0.02164,0.01383,-0.0637,0.8034,1.0000 1.500,0.4954,0.02210,0.01434,-0.0628,0.7971,1.0000 1.750,0.5155,0.02251,0.01480,-0.0618,0.7901,1.0000 2.000,0.5351,0.02291,0.01524,-0.0605,0.7834,1.0000 2.250,0.5546,0.02327,0.01566,-0.0592,0.7755,1.0000 2.500,0.5740,0.02371,0.01620,-0.0580,0.7689,1.0000 2.750,0.5931,0.02422,0.01680,-0.0570,0.7620,1.0000 3.000,0.6132,0.02456,0.01722,-0.0555,0.7561,1.0000 3.250,0.6316,0.02475,0.01751,-0.0537,0.7461,1.0000 3.500,0.6497,0.02449,0.01733,-0.0507,0.7329,1.0000 3.750,0.6685,0.02356,0.01647,-0.0466,0.7175,1.0000 4.000,0.6873,0.02215,0.01508,-0.0418,0.7015,1.0000 4.250,0.7052,0.02105,0.01405,-0.0378,0.6831,1.0000 4.500,0.7258,0.02024,0.01331,-0.0348,0.6710,1.0000 4.750,0.7466,0.01952,0.01273,-0.0320,0.6582,1.0000 5.000,0.7656,0.01864,0.01198,-0.0288,0.6355,1.0000 5.250,0.7850,0.01748,0.01087,-0.0252,0.6061,1.0000 5.500,0.8031,0.01658,0.01000,-0.0217,0.5569,1.0000 5.750,0.8040,0.01735,0.00946,-0.0161,0.3048,1.0000 6.000,0.7933,0.02078,0.01152,-0.0116,0.1354,1.0000 6.250,0.7994,0.02224,0.01284,-0.0084,0.1095,1.0000 6.500,0.8075,0.02340,0.01394,-0.0053,0.0973,1.0000 6.750,0.8164,0.02463,0.01510,-0.0022,0.0902,1.0000 7.000,0.8288,0.02568,0.01612,0.0004,0.0826,1.0000 7.250,0.8450,0.02708,0.01746,0.0025,0.0763,1.0000 7.500,0.8658,0.02849,0.01895,0.0042,0.0721,1.0000 7.750,0.8877,0.03036,0.02074,0.0052,0.0673,1.0000 8.000,0.9075,0.03210,0.02273,0.0069,0.0636,1.0000 8.250,0.9285,0.03432,0.02522,0.0085,0.0620,1.0000 8.500,0.9461,0.03684,0.02807,0.0104,0.0609,1.0000 8.750,0.9599,0.03918,0.03069,0.0126,0.0592,1.0000 9.000,0.9745,0.04136,0.03295,0.0141,0.0567,1.0000 9.250,0.9834,0.04446,0.03646,0.0167,0.0568,1.0000 9.500,0.9810,0.04848,0.04119,0.0205,0.0594,1.0000 9.750,0.9795,0.05272,0.04586,0.0234,0.0619,1.0000 10.000,0.9798,0.05720,0.05058,0.0255,0.0644,1.0000 10.250,0.9574,0.06173,0.05575,0.0298,0.0720,1.0000 10.500,0.9303,0.06733,0.06175,0.0330,0.0845,1.0000 10.750,0.8458,0.05812,0.05272,0.0382,0.0717,1.0000 11.000,0.8150,0.06275,0.05752,0.0391,0.0730,1.0000 11.250,0.7849,0.06799,0.06290,0.0388,0.0739,1.0000 11.500,0.7542,0.07399,0.06901,0.0374,0.0746,1.0000 11.750,0.7235,0.08090,0.07600,0.0349,0.0756,1.0000 12.000,0.6545,0.09620,0.09140,0.0253,0.0854,1.0000