Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n5h10-il-1000000 Airfoil,n5h10-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,74.941 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-n5h10-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.5180,0.08565,0.08349,-0.0150,0.7980,0.0114 -9.000,-0.5222,0.08160,0.07946,-0.0177,0.7943,0.0121 -7.750,-0.7101,0.02238,0.01805,-0.0076,0.7761,0.0093 -7.500,-0.6925,0.02014,0.01544,-0.0061,0.7728,0.0097 -7.250,-0.6742,0.01774,0.01263,-0.0046,0.7692,0.0103 -7.000,-0.6524,0.01631,0.01099,-0.0037,0.7653,0.0110 -6.750,-0.6271,0.01592,0.01054,-0.0034,0.7615,0.0114 -6.500,-0.6019,0.01552,0.01005,-0.0030,0.7578,0.0119 -6.250,-0.5766,0.01486,0.00927,-0.0026,0.7539,0.0126 -6.000,-0.5508,0.01433,0.00864,-0.0022,0.7496,0.0133 -5.750,-0.5250,0.01386,0.00806,-0.0018,0.7454,0.0137 -5.500,-0.5014,0.01262,0.00667,-0.0011,0.7411,0.0150 -5.250,-0.4742,0.01264,0.00671,-0.0010,0.7361,0.0159 -5.000,-0.4474,0.01252,0.00655,-0.0009,0.7314,0.0169 -4.750,-0.4208,0.01224,0.00622,-0.0006,0.7267,0.0180 -4.500,-0.3935,0.01215,0.00608,-0.0005,0.7213,0.0187 -4.250,-0.3698,0.01108,0.00492,0.0002,0.7164,0.0205 -4.000,-0.3429,0.01091,0.00475,0.0004,0.7110,0.0219 -3.750,-0.3159,0.01076,0.00458,0.0005,0.7052,0.0235 -3.500,-0.2891,0.01060,0.00436,0.0007,0.6999,0.0248 -3.250,-0.2613,0.01056,0.00431,0.0007,0.6941,0.0256 -3.000,-0.2388,0.00962,0.00326,0.0017,0.6888,0.0281 -2.750,-0.2125,0.00938,0.00301,0.0020,0.6838,0.0301 -2.500,-0.1860,0.00916,0.00276,0.0022,0.6785,0.0318 -2.250,-0.1597,0.00896,0.00251,0.0025,0.6731,0.0331 -2.000,-0.1328,0.00880,0.00233,0.0027,0.6674,0.0343 -1.750,-0.1060,0.00866,0.00215,0.0029,0.6617,0.0350 -1.500,-0.0802,0.00839,0.00180,0.0033,0.6566,0.0375 -1.250,-0.0535,0.00821,0.00162,0.0036,0.6515,0.0413 -1.000,-0.0266,0.00809,0.00148,0.0038,0.6468,0.0446 -0.750,0.0001,0.00797,0.00137,0.0040,0.6428,0.0541 -0.500,0.0233,0.00745,0.00126,0.0047,0.6391,0.1781 -0.250,0.0389,0.00641,0.00114,0.0067,0.6351,0.4675 0.000,0.0417,0.00516,0.00111,0.0120,0.6313,0.8435 0.250,0.0675,0.00526,0.00122,0.0126,0.6273,0.8670 0.500,0.0938,0.00533,0.00131,0.0131,0.6233,0.8803 0.750,0.1200,0.00541,0.00140,0.0137,0.6196,0.8915 1.000,0.1455,0.00550,0.00147,0.0144,0.6157,0.9018 1.250,0.1716,0.00555,0.00155,0.0150,0.6108,0.9107 1.500,0.1987,0.00557,0.00154,0.0152,0.6039,0.9139 1.750,0.2259,0.00557,0.00155,0.0154,0.5946,0.9184 2.000,0.2515,0.00565,0.00160,0.0160,0.5877,0.9252 2.250,0.2783,0.00564,0.00160,0.0163,0.5806,0.9292 2.500,0.3060,0.00567,0.00160,0.0163,0.5717,0.9305 2.750,0.3342,0.00568,0.00162,0.0161,0.5634,0.9317 3.000,0.3620,0.00572,0.00164,0.0160,0.5550,0.9331 3.250,0.3896,0.00576,0.00166,0.0160,0.5435,0.9344 3.500,0.4173,0.00582,0.00169,0.0159,0.5234,0.9351 3.750,0.4444,0.00593,0.00173,0.0158,0.4979,0.9357 4.000,0.4692,0.00627,0.00184,0.0161,0.4318,0.9364 4.250,0.4885,0.00718,0.00222,0.0170,0.3109,0.9376 4.500,0.5123,0.00763,0.00246,0.0173,0.2557,0.9384 4.750,0.5304,0.00863,0.00293,0.0183,0.1311,0.9398 5.000,0.5533,0.00913,0.00321,0.0188,0.0822,0.9407 5.500,0.6017,0.00991,0.00376,0.0194,0.0356,0.9430 5.750,0.6273,0.01017,0.00407,0.0195,0.0327,0.9442 6.000,0.6530,0.01040,0.00435,0.0196,0.0317,0.9454 6.250,0.6781,0.01067,0.00466,0.0198,0.0300,0.9469 6.500,0.7026,0.01099,0.00503,0.0200,0.0281,0.9485 6.750,0.7255,0.01144,0.00552,0.0205,0.0258,0.9506 7.000,0.7454,0.01211,0.00628,0.0215,0.0235,0.9535 7.250,0.7714,0.01223,0.00642,0.0215,0.0224,0.9557 7.500,0.7972,0.01258,0.00681,0.0213,0.0209,0.9583 7.750,0.8236,0.01292,0.00718,0.0210,0.0192,0.9610 8.000,0.8456,0.01383,0.00815,0.0211,0.0171,0.9654 8.250,0.8729,0.01424,0.00860,0.0205,0.0163,0.9688 8.500,0.9033,0.01450,0.00889,0.0193,0.0150,0.9712 8.750,0.9336,0.01491,0.00931,0.0180,0.0139,0.9737 9.000,0.9624,0.01554,0.00996,0.0168,0.0129,0.9769 9.250,0.9871,0.01673,0.01125,0.0158,0.0118,0.9814 9.500,1.0151,0.01747,0.01206,0.0146,0.0113,0.9848 9.750,1.0431,0.01810,0.01275,0.0134,0.0106,0.9891 10.000,1.0687,0.01876,0.01344,0.0126,0.0100,0.9976 10.250,1.0899,0.01928,0.01398,0.0128,0.0094,1.0000 10.500,1.0916,0.02000,0.01474,0.0163,0.0091,1.0000 10.750,1.0899,0.02158,0.01642,0.0195,0.0087,1.0000 11.000,1.0953,0.02301,0.01796,0.0216,0.0084,1.0000 11.250,1.1075,0.02390,0.01893,0.0228,0.0082,1.0000 11.500,1.1180,0.02502,0.02014,0.0241,0.0080,1.0000 11.750,1.1285,0.02618,0.02138,0.0254,0.0076,1.0000 12.000,1.1379,0.02746,0.02276,0.0265,0.0075,1.0000 12.250,1.1454,0.02899,0.02443,0.0278,0.0073,1.0000 12.500,1.1546,0.03029,0.02581,0.0288,0.0070,1.0000 12.750,1.1648,0.03146,0.02704,0.0294,0.0068,1.0000 13.000,1.1697,0.03328,0.02898,0.0304,0.0067,1.0000 13.250,1.1791,0.03455,0.03030,0.0309,0.0065,1.0000 13.500,1.1828,0.03648,0.03232,0.0315,0.0063,1.0000 13.750,1.1836,0.03880,0.03477,0.0323,0.0062,1.0000 14.000,1.1818,0.04146,0.03758,0.0329,0.0062,1.0000 14.250,1.1739,0.04488,0.04120,0.0334,0.0062,1.0000 14.500,1.1672,0.04821,0.04467,0.0334,0.0060,1.0000 14.750,1.1383,0.05447,0.05122,0.0330,0.0059,1.0000 15.000,1.1115,0.06100,0.05801,0.0316,0.0057,1.0000 15.250,1.0967,0.06634,0.06353,0.0298,0.0057,1.0000 15.500,1.0826,0.07189,0.06923,0.0275,0.0057,1.0000 15.750,1.0689,0.07787,0.07537,0.0247,0.0057,1.0000