Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-p51htip-il-100000 Airfoil,p51htip-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,35.3701 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-p51htip-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.4602,0.09906,0.09424,-0.0455,1.0000,0.1205 -10.000,-0.4776,0.09511,0.09040,-0.0493,1.0000,0.1257 -9.750,-0.5193,0.09128,0.08675,-0.0530,1.0000,0.1268 -9.500,-0.5479,0.08978,0.08533,-0.0498,1.0000,0.1267 -9.250,-0.5806,0.08865,0.08427,-0.0455,1.0000,0.1267 -9.000,-0.6123,0.08759,0.08327,-0.0407,1.0000,0.1266 -8.750,-0.6465,0.08645,0.08214,-0.0358,1.0000,0.1267 -8.500,-0.6802,0.08501,0.08064,-0.0316,1.0000,0.1270 -8.250,-0.6469,0.08031,0.07611,-0.0304,1.0000,0.1338 -8.000,-0.6675,0.07818,0.07396,-0.0271,1.0000,0.1359 -7.750,-0.6930,0.07593,0.07164,-0.0239,1.0000,0.1390 -7.500,-0.7463,0.07614,0.07131,-0.0187,1.0000,0.1422 -7.250,-0.7129,0.07029,0.06592,-0.0182,1.0000,0.1497 -7.000,-0.7452,0.06866,0.06384,-0.0146,1.0000,0.1575 -6.750,-0.7268,0.06510,0.06055,-0.0129,1.0000,0.1666 -6.500,-0.7293,0.06237,0.05777,-0.0104,1.0000,0.1780 -6.250,-0.7295,0.05994,0.05526,-0.0077,1.0000,0.1937 -6.000,-0.7281,0.05757,0.05282,-0.0052,1.0000,0.2103 -5.000,-0.6610,0.03747,0.02931,0.0016,1.0000,0.0818 -4.750,-0.6411,0.03462,0.02612,0.0031,1.0000,0.0778 -4.500,-0.6208,0.03268,0.02381,0.0045,1.0000,0.0780 -4.250,-0.5988,0.03075,0.02150,0.0059,1.0000,0.0769 -4.000,-0.5760,0.02912,0.01953,0.0072,1.0000,0.0758 -3.750,-0.5532,0.02775,0.01793,0.0083,1.0000,0.0762 -3.500,-0.5313,0.02675,0.01681,0.0093,1.0000,0.0800 -3.250,-0.5057,0.02594,0.01584,0.0098,0.9990,0.0832 -3.000,-0.4794,0.02489,0.01476,0.0100,0.9977,0.0858 -2.750,-0.4542,0.02403,0.01402,0.0101,0.9960,0.0918 -2.500,-0.4280,0.02349,0.01349,0.0101,0.9940,0.1007 -2.250,-0.4062,0.02292,0.01293,0.0108,0.9925,0.1110 -2.000,-0.0917,0.02680,0.01971,-0.0289,0.9905,1.0000 -1.750,-0.0729,0.02673,0.01951,-0.0289,0.9878,1.0000 -1.500,-0.0520,0.02676,0.01943,-0.0292,0.9853,1.0000 -1.250,-0.0348,0.02675,0.01931,-0.0287,0.9825,1.0000 -1.000,-0.0206,0.02673,0.01921,-0.0276,0.9796,1.0000 -0.750,-0.0028,0.02680,0.01920,-0.0272,0.9765,1.0000 -0.500,0.0198,0.02699,0.01932,-0.0277,0.9734,1.0000 -0.250,0.0341,0.02706,0.01934,-0.0266,0.9700,1.0000 0.000,0.0480,0.02714,0.01938,-0.0253,0.9659,1.0000 0.250,0.0693,0.02737,0.01957,-0.0255,0.9619,1.0000 0.500,0.0889,0.02762,0.01979,-0.0253,0.9575,1.0000 0.750,0.1003,0.02772,0.01987,-0.0236,0.9523,1.0000 1.000,0.1266,0.02809,0.02023,-0.0246,0.9472,1.0000 1.250,0.1381,0.02826,0.02040,-0.0228,0.9411,1.0000 1.500,0.1592,0.02856,0.02070,-0.0228,0.9347,1.0000 1.750,0.1771,0.02886,0.02102,-0.0221,0.9275,1.0000 2.000,0.1990,0.02919,0.02137,-0.0222,0.9201,1.0000 2.250,0.2138,0.02945,0.02167,-0.0208,0.9113,1.0000 2.500,0.2496,0.02999,0.02226,-0.0232,0.9035,1.0000 2.750,0.2567,0.03011,0.02242,-0.0204,0.8927,1.0000 3.000,0.2767,0.03043,0.02280,-0.0197,0.8825,1.0000 3.250,0.3186,0.03096,0.02343,-0.0228,0.8738,1.0000 3.500,0.3289,0.03108,0.02360,-0.0203,0.8612,1.0000 3.750,0.3465,0.03128,0.02390,-0.0189,0.8487,1.0000 4.000,0.3704,0.03151,0.02423,-0.0185,0.8364,1.0000 4.250,0.4025,0.03169,0.02454,-0.0193,0.8240,1.0000 4.500,0.4452,0.03169,0.02476,-0.0215,0.8115,1.0000 4.750,0.6929,0.01959,0.01027,-0.0355,0.1673,1.0000 5.000,0.6881,0.02089,0.01109,-0.0301,0.1184,1.0000 5.250,0.6878,0.02169,0.01179,-0.0253,0.1037,1.0000 5.500,0.6865,0.02242,0.01251,-0.0204,0.0968,1.0000 5.750,0.6868,0.02304,0.01316,-0.0157,0.0915,1.0000 6.000,0.6897,0.02402,0.01400,-0.0115,0.0868,1.0000 6.250,0.7019,0.02473,0.01477,-0.0087,0.0813,1.0000 6.500,0.7254,0.02594,0.01589,-0.0079,0.0760,1.0000 6.750,0.7788,0.02863,0.01852,-0.0120,0.0724,1.0000 7.000,0.8049,0.03007,0.02019,-0.0113,0.0702,1.0000 7.250,0.8270,0.03156,0.02187,-0.0101,0.0673,1.0000 7.500,0.8513,0.03366,0.02424,-0.0092,0.0668,1.0000 7.750,0.8720,0.03607,0.02698,-0.0076,0.0676,1.0000 8.000,0.8900,0.03887,0.03015,-0.0057,0.0692,1.0000 8.250,0.9058,0.04208,0.03367,-0.0038,0.0709,1.0000 8.500,0.9193,0.04552,0.03737,-0.0018,0.0720,1.0000 8.750,0.9368,0.05003,0.04206,-0.0009,0.0735,1.0000 10.500,0.7530,0.09093,0.08615,0.0160,0.1986,1.0000 10.750,0.6895,0.10023,0.09531,0.0073,0.1935,1.0000 11.000,0.6982,0.10356,0.09864,0.0083,0.1827,1.0000