Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag08-il-100000 Airfoil,ag08-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,45.6167 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-ag08-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.5762,0.11263,0.10781,0.0154,1.0000,0.0737 -8.500,-0.5820,0.11040,0.10567,0.0090,1.0000,0.0745 -8.250,-0.5836,0.10728,0.10261,0.0006,1.0000,0.0748 -8.000,-0.5624,0.10032,0.09561,0.0117,1.0000,0.0781 -7.750,-0.5554,0.09679,0.09211,0.0111,1.0000,0.0810 -7.500,-0.5520,0.09329,0.08865,0.0083,1.0000,0.0843 -7.250,-0.5463,0.08915,0.08453,-0.0079,1.0000,0.0880 -7.000,-0.5383,0.08371,0.07913,-0.0082,1.0000,0.0895 -6.750,-0.5278,0.08032,0.07573,-0.0039,1.0000,0.0925 -6.500,-0.5142,0.07623,0.07163,-0.0083,1.0000,0.0987 -6.250,-0.4993,0.07068,0.06602,-0.0160,1.0000,0.1041 -6.000,-0.4762,0.06633,0.06134,-0.0265,1.0000,0.1159 -5.750,-0.4684,0.06292,0.05821,-0.0194,1.0000,0.1202 -5.500,-0.4470,0.05806,0.05318,-0.0253,1.0000,0.1315 -5.250,-0.4250,0.05399,0.04891,-0.0291,1.0000,0.1444 -5.000,-0.4083,0.05067,0.04567,-0.0276,1.0000,0.1504 -4.750,-0.3596,0.03572,0.02914,-0.0387,1.0000,0.0764 -4.500,-0.3337,0.03118,0.02424,-0.0391,1.0000,0.0692 -4.250,-0.3061,0.02765,0.02007,-0.0393,1.0000,0.0715 -4.000,-0.2781,0.02440,0.01619,-0.0391,1.0000,0.0722 -3.750,-0.2496,0.02199,0.01311,-0.0385,1.0000,0.0746 -3.500,-0.2238,0.02015,0.01117,-0.0382,1.0000,0.0852 -3.250,-0.1968,0.01826,0.00909,-0.0376,1.0000,0.0936 -3.000,-0.1705,0.01710,0.00786,-0.0370,1.0000,0.1113 -2.750,-0.1443,0.01581,0.00656,-0.0364,1.0000,0.1319 -2.500,-0.1187,0.01479,0.00572,-0.0358,1.0000,0.1645 -2.250,-0.0934,0.01381,0.00495,-0.0353,1.0000,0.2150 -2.000,-0.0684,0.01266,0.00438,-0.0348,1.0000,0.3139 -1.750,-0.0476,0.01090,0.00402,-0.0332,1.0000,0.6122 -1.500,-0.0149,0.00997,0.00362,-0.0326,1.0000,1.0000 -1.250,0.0104,0.00998,0.00335,-0.0321,1.0000,1.0000 -1.000,0.0355,0.01001,0.00318,-0.0316,1.0000,1.0000 -0.750,0.0606,0.01006,0.00307,-0.0311,1.0000,1.0000 -0.500,0.0854,0.01012,0.00301,-0.0307,1.0000,1.0000 -0.250,0.1102,0.01021,0.00299,-0.0302,1.0000,1.0000 0.000,0.1348,0.01031,0.00301,-0.0298,1.0000,1.0000 0.250,0.1593,0.01045,0.00309,-0.0294,1.0000,1.0000 0.500,0.1837,0.01061,0.00323,-0.0292,1.0000,1.0000 0.750,0.2078,0.01083,0.00343,-0.0290,1.0000,1.0000 1.000,0.2315,0.01109,0.00371,-0.0289,1.0000,1.0000 1.250,0.2547,0.01144,0.00408,-0.0290,1.0000,1.0000 1.500,0.3192,0.01159,0.00431,-0.0367,0.9753,1.0000 1.750,0.3797,0.01155,0.00441,-0.0429,0.9477,1.0000 2.000,0.4279,0.01142,0.00438,-0.0461,0.9127,1.0000 2.250,0.4621,0.01135,0.00434,-0.0460,0.8672,1.0000 2.500,0.4887,0.01139,0.00432,-0.0442,0.8166,1.0000 2.750,0.5119,0.01156,0.00439,-0.0418,0.7608,1.0000 3.000,0.5345,0.01185,0.00450,-0.0396,0.7022,1.0000 3.250,0.5574,0.01225,0.00468,-0.0378,0.6430,1.0000 3.500,0.5807,0.01273,0.00492,-0.0362,0.5862,1.0000 3.750,0.6044,0.01327,0.00526,-0.0350,0.5330,1.0000 4.000,0.6285,0.01385,0.00563,-0.0339,0.4835,1.0000 4.250,0.6527,0.01446,0.00606,-0.0330,0.4377,1.0000 4.500,0.6772,0.01509,0.00655,-0.0322,0.3940,1.0000 4.750,0.7016,0.01575,0.00708,-0.0314,0.3523,1.0000 5.000,0.7259,0.01644,0.00770,-0.0307,0.3115,1.0000 5.250,0.7500,0.01718,0.00833,-0.0300,0.2707,1.0000 5.500,0.7738,0.01800,0.00904,-0.0294,0.2291,1.0000 5.750,0.7972,0.01895,0.00990,-0.0287,0.1862,1.0000 6.000,0.8201,0.02012,0.01094,-0.0279,0.1443,1.0000 6.250,0.8421,0.02163,0.01228,-0.0272,0.1095,1.0000 6.500,0.8649,0.02335,0.01399,-0.0262,0.0850,1.0000 6.750,0.8875,0.02579,0.01637,-0.0253,0.0706,1.0000 7.000,0.9112,0.02751,0.01835,-0.0244,0.0603,1.0000 7.250,0.9341,0.03049,0.02167,-0.0233,0.0549,1.0000 7.500,0.9561,0.03365,0.02533,-0.0221,0.0519,1.0000 7.750,0.9761,0.03665,0.02866,-0.0211,0.0490,1.0000 8.000,0.9900,0.04149,0.03380,-0.0205,0.0460,1.0000 8.250,1.0026,0.04520,0.03823,-0.0192,0.0451,1.0000 8.500,1.0105,0.05040,0.04395,-0.0182,0.0454,1.0000 8.750,1.0149,0.05666,0.05054,-0.0177,0.0461,1.0000 9.000,0.9974,0.06371,0.05873,-0.0178,0.0502,1.0000 9.250,0.9760,0.07159,0.06697,-0.0201,0.0528,1.0000 9.500,0.8752,0.06516,0.06075,-0.0118,0.0517,1.0000 9.750,0.8411,0.07330,0.06898,-0.0167,0.0537,1.0000 10.000,0.8198,0.08127,0.07697,-0.0208,0.0558,1.0000 10.250,0.8065,0.08822,0.08389,-0.0232,0.0570,1.0000 10.500,0.7977,0.09445,0.09011,-0.0245,0.0578,1.0000 10.750,0.8597,0.13307,0.12839,-0.0635,0.1162,1.0000 11.000,0.7308,0.12776,0.12335,-0.0419,0.1231,1.0000 11.250,0.7287,0.13310,0.12867,-0.0428,0.1220,1.0000