Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-v13006-il-100000-n5 Airfoil,v13006-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,35.3166 Max Cl/Cd alpha,4 Url,http://www.airfoiltools.com/polar/csv?polar=xf-v13006-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.6288,0.10037,0.09539,0.0163,1.0000,0.0499 -8.250,-0.6296,0.09610,0.09117,0.0116,1.0000,0.0515 -8.000,-0.6316,0.09099,0.08608,0.0020,1.0000,0.0526 -7.750,-0.6285,0.08608,0.08104,-0.0052,1.0000,0.0531 -7.500,-0.6234,0.08168,0.07645,-0.0091,1.0000,0.0533 -7.250,-0.6161,0.07579,0.07058,-0.0103,1.0000,0.0539 -7.000,-0.6063,0.07117,0.06604,-0.0097,1.0000,0.0549 -6.750,-0.5952,0.06729,0.06213,-0.0101,1.0000,0.0560 -6.500,-0.5827,0.06335,0.05810,-0.0113,1.0000,0.0572 -6.250,-0.5623,0.05646,0.05076,-0.0140,1.0000,0.0382 -6.000,-0.5489,0.05203,0.04621,-0.0145,1.0000,0.0350 -5.500,-0.5056,0.04258,0.03565,-0.0149,1.0000,0.0278 -5.250,-0.4873,0.03865,0.03146,-0.0148,1.0000,0.0274 -5.000,-0.4665,0.03536,0.02778,-0.0144,1.0000,0.0272 -4.750,-0.4433,0.03288,0.02479,-0.0138,1.0000,0.0282 -4.500,-0.4226,0.02957,0.02121,-0.0135,1.0000,0.0296 -4.250,-0.3988,0.02729,0.01861,-0.0129,1.0000,0.0302 -4.000,-0.3737,0.02513,0.01608,-0.0122,1.0000,0.0302 -3.750,-0.3484,0.02325,0.01390,-0.0115,1.0000,0.0304 -3.500,-0.3229,0.02160,0.01199,-0.0107,1.0000,0.0310 -3.250,-0.2973,0.02016,0.01039,-0.0100,1.0000,0.0319 -3.000,-0.2719,0.01898,0.00910,-0.0093,1.0000,0.0339 -2.750,-0.2467,0.01805,0.00808,-0.0086,1.0000,0.0374 -2.500,-0.2217,0.01707,0.00700,-0.0078,1.0000,0.0392 -2.250,-0.1980,0.01597,0.00592,-0.0069,1.0000,0.0413 -2.000,-0.1743,0.01513,0.00508,-0.0060,1.0000,0.0451 -1.750,-0.1497,0.01460,0.00448,-0.0053,1.0000,0.0533 -1.500,-0.1252,0.01396,0.00386,-0.0046,1.0000,0.0663 -1.250,-0.1012,0.01285,0.00335,-0.0041,1.0000,0.1757 -1.000,-0.0395,0.01023,0.00331,-0.0093,1.0000,1.0000 -0.750,-0.0183,0.01020,0.00313,-0.0081,1.0000,1.0000 -0.500,0.0029,0.01019,0.00300,-0.0069,1.0000,1.0000 -0.250,0.0242,0.01020,0.00291,-0.0057,1.0000,1.0000 0.000,0.0457,0.01023,0.00288,-0.0046,1.0000,1.0000 0.250,0.0674,0.01028,0.00288,-0.0036,1.0000,1.0000 0.500,0.0915,0.01035,0.00292,-0.0032,0.9983,1.0000 0.750,0.1376,0.01042,0.00298,-0.0071,0.9780,1.0000 1.000,0.1826,0.01045,0.00302,-0.0106,0.9459,1.0000 1.250,0.2245,0.01047,0.00303,-0.0131,0.9026,1.0000 1.500,0.2601,0.01052,0.00304,-0.0141,0.8534,1.0000 1.750,0.2891,0.01062,0.00305,-0.0137,0.7996,1.0000 2.000,0.3147,0.01080,0.00309,-0.0125,0.7422,1.0000 2.250,0.3390,0.01105,0.00318,-0.0112,0.6831,1.0000 2.500,0.3631,0.01137,0.00329,-0.0099,0.6222,1.0000 2.750,0.3875,0.01174,0.00346,-0.0089,0.5619,1.0000 3.000,0.4119,0.01213,0.00368,-0.0080,0.5056,1.0000 3.250,0.4364,0.01256,0.00398,-0.0072,0.4523,1.0000 3.500,0.4600,0.01313,0.00425,-0.0064,0.3849,1.0000 3.750,0.4833,0.01378,0.00452,-0.0057,0.3089,1.0000 4.000,0.5075,0.01437,0.00488,-0.0052,0.2537,1.0000 4.250,0.5310,0.01516,0.00528,-0.0048,0.1643,1.0000 4.500,0.5531,0.01657,0.00603,-0.0043,0.0578,1.0000 4.750,0.5770,0.01766,0.00703,-0.0037,0.0423,1.0000 5.000,0.6013,0.01862,0.00811,-0.0030,0.0378,1.0000 5.250,0.6255,0.01954,0.00921,-0.0024,0.0353,1.0000 5.500,0.6492,0.02057,0.01042,-0.0017,0.0334,1.0000 5.750,0.6724,0.02173,0.01169,-0.0009,0.0320,1.0000 6.000,0.6954,0.02305,0.01311,-0.0001,0.0309,1.0000 6.250,0.7178,0.02463,0.01476,0.0005,0.0292,1.0000 6.500,0.7399,0.02670,0.01700,0.0012,0.0276,1.0000 6.750,0.7634,0.02823,0.01880,0.0019,0.0267,1.0000 7.000,0.7860,0.03024,0.02112,0.0027,0.0263,1.0000 7.250,0.8073,0.03254,0.02380,0.0034,0.0259,1.0000 7.500,0.8269,0.03518,0.02686,0.0042,0.0257,1.0000 7.750,0.8441,0.03819,0.03035,0.0050,0.0256,1.0000 8.000,0.8585,0.04163,0.03431,0.0057,0.0255,1.0000 8.250,0.8693,0.04551,0.03868,0.0063,0.0256,1.0000 8.500,0.8758,0.04984,0.04347,0.0066,0.0257,1.0000 8.750,0.8776,0.05453,0.04858,0.0066,0.0258,1.0000 9.000,0.8739,0.05956,0.05397,0.0059,0.0258,1.0000 9.250,0.8642,0.06497,0.05967,0.0042,0.0259,1.0000 9.500,0.8480,0.07069,0.06556,0.0013,0.0262,1.0000 9.750,0.8307,0.07851,0.07348,-0.0061,0.0266,1.0000 10.000,0.8175,0.08788,0.08285,-0.0140,0.0270,1.0000 10.250,0.8085,0.09573,0.09065,-0.0189,0.0274,1.0000 10.500,0.8020,0.10244,0.09733,-0.0224,0.0276,1.0000 10.750,0.7973,0.10859,0.10345,-0.0252,0.0278,1.0000 11.000,0.7936,0.11457,0.10940,-0.0279,0.0279,1.0000