Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca001034a08cli02-il-1000000-n5 Airfoil,naca001034a08cli02-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,78.672 Max Cl/Cd alpha,2 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca001034a08cli02-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.5285,0.08041,0.07886,-0.0403,1.0000,0.0014 -9.250,-0.5383,0.07437,0.07286,-0.0447,1.0000,0.0013 -9.000,-0.5513,0.06632,0.06477,-0.0542,0.9968,0.0013 -8.750,-0.5565,0.05926,0.05757,-0.0598,0.9905,0.0013 -8.500,-0.5571,0.05243,0.05055,-0.0632,0.9853,0.0013 -8.250,-0.5572,0.04604,0.04391,-0.0640,0.9785,0.0013 -8.000,-0.5569,0.03940,0.03694,-0.0631,0.9713,0.0012 -7.750,-0.5592,0.03111,0.02811,-0.0602,0.9639,0.0013 -7.500,-0.5621,0.02196,0.01816,-0.0553,0.9558,0.0015 -7.250,-0.5449,0.01890,0.01471,-0.0536,0.9516,0.0017 -7.000,-0.5231,0.01756,0.01317,-0.0528,0.9471,0.0018 -6.750,-0.4997,0.01662,0.01208,-0.0522,0.9432,0.0019 -6.500,-0.4796,0.01444,0.00955,-0.0509,0.9396,0.0021 -6.250,-0.4587,0.01288,0.00771,-0.0497,0.9353,0.0022 -6.000,-0.4360,0.01191,0.00659,-0.0489,0.9312,0.0024 -5.750,-0.4121,0.01121,0.00578,-0.0483,0.9277,0.0026 -5.500,-0.3866,0.01085,0.00538,-0.0480,0.9240,0.0030 -5.250,-0.3605,0.01059,0.00510,-0.0479,0.9202,0.0035 -5.000,-0.3348,0.01023,0.00469,-0.0477,0.9165,0.0041 -4.750,-0.3098,0.00973,0.00410,-0.0472,0.9131,0.0048 -4.500,-0.2831,0.00954,0.00388,-0.0472,0.9091,0.0055 -4.250,-0.2583,0.00901,0.00324,-0.0467,0.9049,0.0067 -4.000,-0.2322,0.00867,0.00279,-0.0465,0.9012,0.0077 -3.750,-0.2054,0.00847,0.00258,-0.0465,0.8972,0.0096 -3.500,-0.1786,0.00826,0.00233,-0.0464,0.8926,0.0114 -3.250,-0.1514,0.00814,0.00218,-0.0464,0.8884,0.0122 -3.000,-0.1244,0.00795,0.00194,-0.0464,0.8837,0.0133 -2.750,-0.0973,0.00779,0.00170,-0.0463,0.8784,0.0151 -2.500,-0.0702,0.00764,0.00154,-0.0463,0.8734,0.0215 -2.250,-0.0447,0.00723,0.00135,-0.0460,0.8672,0.0915 -2.000,-0.0221,0.00649,0.00113,-0.0455,0.8609,0.2564 -1.750,0.0007,0.00581,0.00099,-0.0450,0.8535,0.4154 -1.500,0.0248,0.00538,0.00089,-0.0445,0.8464,0.5224 -1.250,0.0484,0.00497,0.00084,-0.0439,0.8386,0.6334 -1.000,0.0741,0.00479,0.00082,-0.0435,0.8311,0.6890 -0.750,0.1012,0.00475,0.00077,-0.0435,0.8230,0.7099 -0.500,0.1281,0.00469,0.00076,-0.0434,0.8141,0.7348 -0.250,0.1550,0.00465,0.00075,-0.0433,0.8047,0.7556 0.000,0.1820,0.00463,0.00074,-0.0432,0.7943,0.7721 0.250,0.2090,0.00463,0.00074,-0.0431,0.7825,0.7869 0.500,0.2359,0.00463,0.00074,-0.0430,0.7697,0.8009 0.750,0.2626,0.00465,0.00076,-0.0428,0.7554,0.8148 1.000,0.2889,0.00468,0.00079,-0.0426,0.7382,0.8295 1.250,0.3146,0.00474,0.00083,-0.0422,0.7160,0.8453 1.500,0.3402,0.00480,0.00090,-0.0418,0.6936,0.8623 1.750,0.3657,0.00488,0.00097,-0.0414,0.6736,0.8811 2.000,0.3910,0.00497,0.00106,-0.0409,0.6494,0.9009 2.250,0.4109,0.00544,0.00121,-0.0393,0.5610,0.9216 2.500,0.4317,0.00597,0.00141,-0.0381,0.4698,0.9395 2.750,0.4551,0.00646,0.00162,-0.0374,0.3930,0.9530 3.000,0.4745,0.00744,0.00198,-0.0363,0.2408,0.9645 3.250,0.4982,0.00833,0.00235,-0.0361,0.1118,0.9721 3.500,0.5245,0.00893,0.00266,-0.0363,0.0397,0.9783 3.750,0.5540,0.00926,0.00290,-0.0369,0.0183,0.9830 4.000,0.5839,0.00950,0.00313,-0.0377,0.0148,0.9869 4.250,0.6162,0.00976,0.00343,-0.0389,0.0127,0.9891 4.500,0.6473,0.01005,0.00378,-0.0399,0.0119,0.9917 4.750,0.6767,0.01043,0.00428,-0.0406,0.0110,0.9944 5.000,0.7079,0.01074,0.00463,-0.0417,0.0100,0.9960 5.250,0.7402,0.01082,0.00467,-0.0431,0.0087,0.9976 5.500,0.7714,0.01103,0.00483,-0.0444,0.0058,0.9993 5.750,0.7963,0.01135,0.00515,-0.0441,0.0040,1.0000 6.000,0.8165,0.01166,0.00547,-0.0428,0.0031,1.0000 6.250,0.8362,0.01203,0.00584,-0.0413,0.0023,1.0000 6.500,0.8548,0.01253,0.00642,-0.0396,0.0018,1.0000 6.750,0.8714,0.01325,0.00726,-0.0374,0.0015,1.0000 7.000,0.8910,0.01369,0.00779,-0.0360,0.0015,1.0000 7.250,0.9110,0.01413,0.00829,-0.0347,0.0014,1.0000 7.500,0.9308,0.01465,0.00888,-0.0334,0.0012,1.0000 7.750,0.9499,0.01529,0.00961,-0.0320,0.0011,1.0000 8.000,0.9681,0.01609,0.01052,-0.0304,0.0010,1.0000 8.250,0.9855,0.01707,0.01164,-0.0287,0.0009,1.0000 8.500,1.0023,0.01825,0.01299,-0.0269,0.0008,1.0000 8.750,1.0183,0.01971,0.01465,-0.0250,0.0008,1.0000 9.000,1.0330,0.02162,0.01682,-0.0229,0.0008,1.0000 9.250,1.0442,0.02445,0.02003,-0.0203,0.0007,1.0000 9.500,1.0232,0.03451,0.03109,-0.0123,0.0008,1.0000 9.750,0.9924,0.04420,0.04141,-0.0042,0.0008,1.0000 10.000,0.9707,0.04998,0.04751,0.0014,0.0008,1.0000 10.250,0.9483,0.05423,0.05197,0.0064,0.0009,1.0000 10.500,0.9260,0.05844,0.05635,0.0099,0.0009,1.0000 10.750,0.9038,0.06289,0.06095,0.0118,0.0009,1.0000 11.000,0.8809,0.06796,0.06616,0.0119,0.0009,1.0000 11.250,0.8588,0.07379,0.07211,0.0100,0.0009,1.0000 11.500,0.8368,0.08109,0.07952,0.0055,0.0009,1.0000