Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rae2822-il-200000-n5 Airfoil,rae2822-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,49.0992 Max Cl/Cd alpha,3.25 Url,http://airfoiltools.com/polar/csv?polar=xf-rae2822-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.500,-0.7179,0.08429,0.08026,-0.0480,1.0000,0.0142 -13.250,-0.7523,0.07422,0.07000,-0.0543,1.0000,0.0142 -13.000,-0.7788,0.06695,0.06257,-0.0582,1.0000,0.0139 -12.750,-0.8013,0.06101,0.05643,-0.0607,1.0000,0.0139 -12.500,-0.8201,0.05607,0.05127,-0.0623,1.0000,0.0139 -12.250,-0.8361,0.05181,0.04680,-0.0630,1.0000,0.0140 -12.000,-0.8496,0.04811,0.04287,-0.0629,1.0000,0.0141 -11.750,-0.8606,0.04490,0.03943,-0.0622,1.0000,0.0143 -11.500,-0.8692,0.04210,0.03639,-0.0609,1.0000,0.0145 -11.250,-0.8759,0.03965,0.03370,-0.0591,1.0000,0.0148 -11.000,-0.8811,0.03762,0.03145,-0.0567,1.0000,0.0151 -10.750,-0.8867,0.03592,0.02953,-0.0535,1.0000,0.0154 -10.500,-0.8882,0.03446,0.02783,-0.0504,1.0000,0.0158 -10.250,-0.8855,0.03289,0.02623,-0.0479,1.0000,0.0164 -10.000,-0.8798,0.03168,0.02492,-0.0455,1.0000,0.0168 -9.750,-0.8727,0.03060,0.02376,-0.0432,1.0000,0.0174 -9.500,-0.8644,0.02939,0.02243,-0.0408,1.0000,0.0179 -9.250,-0.8551,0.02821,0.02112,-0.0385,1.0000,0.0185 -9.000,-0.8448,0.02705,0.01984,-0.0363,1.0000,0.0191 -8.750,-0.8339,0.02597,0.01860,-0.0340,1.0000,0.0199 -8.500,-0.8220,0.02504,0.01752,-0.0319,1.0000,0.0207 -8.250,-0.7993,0.02377,0.01621,-0.0322,0.9979,0.0221 -8.000,-0.7700,0.02286,0.01525,-0.0337,0.9948,0.0238 -7.750,-0.7423,0.02187,0.01418,-0.0347,0.9915,0.0254 -7.500,-0.7139,0.02093,0.01309,-0.0358,0.9878,0.0272 -7.250,-0.6851,0.01986,0.01199,-0.0373,0.9845,0.0297 -7.000,-0.6564,0.01916,0.01125,-0.0384,0.9809,0.0330 -6.750,-0.6285,0.01844,0.01042,-0.0392,0.9765,0.0361 -6.500,-0.5988,0.01758,0.00954,-0.0406,0.9730,0.0412 -6.250,-0.5664,0.01693,0.00883,-0.0424,0.9705,0.0480 -6.000,-0.5406,0.01633,0.00821,-0.0426,0.9651,0.0561 -5.750,-0.5109,0.01571,0.00761,-0.0438,0.9612,0.0697 -5.500,-0.4790,0.01504,0.00702,-0.0454,0.9583,0.0919 -5.250,-0.4467,0.01428,0.00644,-0.0473,0.9558,0.1340 -5.000,-0.4235,0.01341,0.00587,-0.0475,0.9496,0.2021 -4.750,-0.3969,0.01187,0.00521,-0.0490,0.9457,0.3878 -4.500,-0.3637,0.01160,0.00519,-0.0504,0.9432,0.4750 -4.250,-0.3318,0.01156,0.00514,-0.0513,0.9399,0.5075 -4.000,-0.3034,0.01156,0.00509,-0.0515,0.9345,0.5296 -3.750,-0.2708,0.01157,0.00505,-0.0525,0.9311,0.5478 -3.500,-0.2371,0.01160,0.00507,-0.0536,0.9285,0.5650 -3.250,-0.2080,0.01172,0.00518,-0.0537,0.9239,0.5824 -3.000,-0.1786,0.01172,0.00513,-0.0540,0.9188,0.5925 -2.750,-0.1457,0.01162,0.00498,-0.0551,0.9154,0.5957 -2.500,-0.1114,0.01151,0.00481,-0.0566,0.9128,0.5993 -2.250,-0.0845,0.01145,0.00468,-0.0565,0.9064,0.6033 -2.000,-0.0532,0.01136,0.00455,-0.0573,0.9020,0.6065 -1.750,-0.0200,0.01126,0.00444,-0.0584,0.8988,0.6093 -1.500,0.0079,0.01122,0.00438,-0.0585,0.8930,0.6129 -1.250,0.0382,0.01116,0.00429,-0.0590,0.8878,0.6168 -1.000,0.0708,0.01107,0.00418,-0.0601,0.8841,0.6205 -0.750,0.0985,0.01104,0.00418,-0.0601,0.8781,0.6234 -0.500,0.1281,0.01099,0.00415,-0.0605,0.8726,0.6269 -0.250,0.1602,0.01093,0.00409,-0.0613,0.8687,0.6311 0.000,0.1871,0.01093,0.00410,-0.0612,0.8617,0.6353 0.250,0.2170,0.01088,0.00411,-0.0616,0.8564,0.6383 0.500,0.2463,0.01086,0.00413,-0.0619,0.8508,0.6420 0.750,0.2744,0.01085,0.00417,-0.0619,0.8438,0.6463 1.000,0.3052,0.01081,0.00415,-0.0625,0.8382,0.6508 1.250,0.3316,0.01081,0.00423,-0.0621,0.8291,0.6545 1.500,0.3606,0.01078,0.00425,-0.0622,0.8206,0.6588 1.750,0.3896,0.01073,0.00425,-0.0623,0.8099,0.6635 2.000,0.4170,0.01068,0.00425,-0.0619,0.7954,0.6675 2.250,0.4428,0.01061,0.00421,-0.0610,0.7717,0.6720 2.500,0.4688,0.01057,0.00409,-0.0601,0.7357,0.6773 2.750,0.4935,0.01061,0.00408,-0.0591,0.6978,0.6820 3.000,0.5179,0.01072,0.00412,-0.0581,0.6549,0.6867 3.250,0.5396,0.01099,0.00415,-0.0566,0.5831,0.6920 3.500,0.5532,0.01175,0.00433,-0.0537,0.4535,0.6971 3.750,0.5643,0.01283,0.00478,-0.0509,0.3149,0.7024 4.000,0.5795,0.01385,0.00527,-0.0490,0.2019,0.7087 4.250,0.5973,0.01469,0.00576,-0.0475,0.1243,0.7141 4.500,0.6180,0.01531,0.00625,-0.0465,0.0866,0.7203 4.750,0.6399,0.01585,0.00672,-0.0456,0.0666,0.7265 5.000,0.6620,0.01632,0.00723,-0.0446,0.0560,0.7330 5.250,0.6841,0.01686,0.00779,-0.0437,0.0487,0.7404 5.500,0.7058,0.01734,0.00836,-0.0427,0.0429,0.7474 5.750,0.7265,0.01798,0.00906,-0.0415,0.0392,0.7553 6.000,0.7478,0.01851,0.00971,-0.0404,0.0358,0.7629 6.250,0.7688,0.01910,0.01034,-0.0394,0.0325,0.7713 6.500,0.7880,0.01990,0.01123,-0.0380,0.0303,0.7805 6.750,0.8084,0.02061,0.01209,-0.0367,0.0285,0.7899 7.000,0.8289,0.02135,0.01294,-0.0356,0.0267,0.8004 7.250,0.8489,0.02202,0.01368,-0.0344,0.0250,0.8116 7.500,0.8680,0.02305,0.01479,-0.0332,0.0234,0.8234 7.750,0.8887,0.02397,0.01590,-0.0320,0.0223,0.8370 8.000,0.9090,0.02502,0.01715,-0.0307,0.0212,0.8527 8.250,0.9285,0.02608,0.01839,-0.0294,0.0202,0.8717 8.500,0.9461,0.02701,0.01949,-0.0278,0.0194,0.8980 8.750,0.9660,0.02789,0.02049,-0.0269,0.0185,0.9821 9.000,0.9867,0.02954,0.02232,-0.0263,0.0176,1.0000 9.250,1.0061,0.03125,0.02432,-0.0254,0.0167,1.0000 9.500,1.0229,0.03332,0.02671,-0.0242,0.0161,1.0000 9.750,1.0365,0.03549,0.02917,-0.0227,0.0156,1.0000 10.000,1.0470,0.03767,0.03163,-0.0209,0.0151,1.0000 10.250,1.0540,0.03995,0.03419,-0.0188,0.0148,1.0000 10.500,1.0561,0.04216,0.03664,-0.0161,0.0145,1.0000 10.750,1.0551,0.04436,0.03906,-0.0132,0.0143,1.0000 11.000,1.0506,0.04681,0.04173,-0.0103,0.0141,1.0000 11.250,1.0435,0.04940,0.04454,-0.0077,0.0140,1.0000 11.500,1.0336,0.05232,0.04766,-0.0055,0.0139,1.0000 11.750,1.0252,0.05506,0.05053,-0.0041,0.0136,1.0000 12.000,1.0068,0.05930,0.05503,-0.0031,0.0136,1.0000 12.250,0.9885,0.06380,0.05968,-0.0032,0.0135,1.0000