Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-bacj-il-500000 Airfoil,bacj-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,51.7927 Max Cl/Cd alpha,2 Url,http://airfoiltools.com/polar/csv?polar=xf-bacj-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.250,-0.6814,0.10236,0.09977,-0.0405,1.0000,0.0264 -13.000,-0.6795,0.10052,0.09796,-0.0407,1.0000,0.0267 -12.750,-0.8004,0.06821,0.06536,-0.0610,1.0000,0.0240 -12.500,-0.8583,0.05826,0.05515,-0.0651,1.0000,0.0232 -12.250,-0.8943,0.05308,0.04978,-0.0648,1.0000,0.0233 -12.000,-0.9900,0.04432,0.04041,-0.0596,1.0000,0.0223 -11.750,-0.9542,0.04641,0.04278,-0.0592,1.0000,0.0233 -11.500,-1.0120,0.04282,0.03888,-0.0511,1.0000,0.0227 -11.250,-1.0484,0.03874,0.03437,-0.0447,1.0000,0.0224 -11.000,-1.0446,0.03774,0.03331,-0.0420,1.0000,0.0227 -10.750,-1.0397,0.03663,0.03212,-0.0395,1.0000,0.0230 -10.500,-1.0367,0.03273,0.02775,-0.0383,0.9987,0.0227 -10.250,-1.0163,0.03097,0.02581,-0.0388,0.9971,0.0230 -10.000,-0.9949,0.02908,0.02370,-0.0393,0.9955,0.0233 -9.750,-0.9723,0.02761,0.02205,-0.0396,0.9935,0.0235 -9.500,-0.9478,0.02626,0.02053,-0.0401,0.9919,0.0241 -9.250,-0.9225,0.02506,0.01917,-0.0406,0.9908,0.0245 -9.000,-0.9017,0.02379,0.01774,-0.0400,0.9888,0.0249 -8.750,-0.8767,0.02311,0.01694,-0.0402,0.9871,0.0255 -8.500,-0.8503,0.02228,0.01597,-0.0405,0.9859,0.0259 -8.250,-0.8262,0.02072,0.01430,-0.0406,0.9850,0.0267 -8.000,-0.8057,0.01985,0.01340,-0.0398,0.9828,0.0273 -7.750,-0.7804,0.01917,0.01270,-0.0399,0.9810,0.0281 -7.500,-0.7528,0.01853,0.01202,-0.0404,0.9796,0.0291 -7.250,-0.7238,0.01797,0.01140,-0.0411,0.9787,0.0299 -7.000,-0.7029,0.01750,0.01088,-0.0401,0.9759,0.0309 -6.750,-0.6764,0.01690,0.01020,-0.0403,0.9741,0.0321 -6.500,-0.6491,0.01611,0.00941,-0.0408,0.9727,0.0337 -6.250,-0.6184,0.01571,0.00900,-0.0418,0.9718,0.0356 -6.000,-0.5995,0.01544,0.00869,-0.0401,0.9685,0.0381 -5.750,-0.5747,0.01485,0.00811,-0.0400,0.9666,0.0411 -5.500,-0.5452,0.01456,0.00781,-0.0406,0.9654,0.0445 -5.250,-0.5153,0.01416,0.00741,-0.0413,0.9644,0.0500 -5.000,-0.4959,0.01391,0.00715,-0.0398,0.9611,0.0555 -4.750,-0.4701,0.01352,0.00682,-0.0396,0.9589,0.0668 -4.500,-0.4421,0.01312,0.00658,-0.0400,0.9574,0.0910 -4.250,-0.4117,0.01279,0.00639,-0.0409,0.9563,0.1217 -4.000,-0.3881,0.01256,0.00626,-0.0403,0.9538,0.1469 -3.750,-0.3672,0.01234,0.00614,-0.0390,0.9506,0.1733 -3.500,-0.3407,0.01207,0.00602,-0.0390,0.9488,0.2092 -3.250,-0.3129,0.01168,0.00588,-0.0393,0.9474,0.2649 -2.750,-0.2792,0.01047,0.00560,-0.0355,0.9403,0.4964 -2.500,-0.2540,0.01021,0.00567,-0.0349,0.9381,0.5886 -2.250,-0.2234,0.01018,0.00573,-0.0353,0.9368,0.6283 -2.000,-0.1915,0.01022,0.00580,-0.0361,0.9358,0.6500 -1.750,-0.1739,0.01033,0.00591,-0.0338,0.9314,0.6647 -1.500,-0.1488,0.01041,0.00601,-0.0331,0.9285,0.6810 -1.250,-0.1175,0.01046,0.00605,-0.0337,0.9266,0.6956 -1.000,-0.0823,0.01042,0.00604,-0.0350,0.9253,0.7031 -0.750,-0.0488,0.01044,0.00604,-0.0362,0.9243,0.7109 -0.500,-0.0283,0.01046,0.00610,-0.0344,0.9186,0.7176 -0.250,0.0072,0.01031,0.00598,-0.0357,0.9154,0.7249 0.000,0.0488,0.01005,0.00573,-0.0382,0.9135,0.7308 0.250,0.0896,0.00983,0.00556,-0.0406,0.9122,0.7364 0.500,0.1332,0.00955,0.00530,-0.0436,0.9113,0.7452 0.750,0.1560,0.00938,0.00520,-0.0420,0.9033,0.7510 1.000,0.2343,0.00815,0.00402,-0.0516,0.8985,0.7551 1.250,0.2648,0.00776,0.00363,-0.0515,0.8857,0.7592 1.500,0.2984,0.00745,0.00331,-0.0521,0.8706,0.7627 1.750,0.3236,0.00726,0.00315,-0.0511,0.8489,0.7662 2.000,0.3698,0.00714,0.00287,-0.0545,0.7813,0.7686 2.250,0.3768,0.00784,0.00285,-0.0495,0.6221,0.7718 2.500,0.3624,0.00886,0.00308,-0.0405,0.4456,0.7758 2.750,0.3659,0.00988,0.00338,-0.0357,0.2771,0.7792 3.000,0.3758,0.01097,0.00372,-0.0325,0.1000,0.7819 3.250,0.3952,0.01152,0.00404,-0.0308,0.0582,0.7847 3.500,0.4176,0.01180,0.00433,-0.0297,0.0511,0.7879 3.750,0.4394,0.01215,0.00465,-0.0284,0.0462,0.7914 4.000,0.4612,0.01249,0.00498,-0.0271,0.0426,0.7947 4.250,0.4843,0.01273,0.00523,-0.0261,0.0402,0.7975 4.500,0.5057,0.01318,0.00568,-0.0249,0.0376,0.8003 4.750,0.5267,0.01374,0.00628,-0.0235,0.0361,0.8036 5.000,0.5498,0.01407,0.00665,-0.0225,0.0345,0.8071 5.250,0.5729,0.01436,0.00692,-0.0216,0.0324,0.8108 5.500,0.5955,0.01513,0.00767,-0.0207,0.0304,0.8140 5.750,0.6214,0.01599,0.00857,-0.0206,0.0300,0.8174 6.000,0.6461,0.01629,0.00896,-0.0199,0.0289,0.8210 6.250,0.6721,0.01687,0.00957,-0.0196,0.0274,0.8247 6.500,0.7013,0.01775,0.01051,-0.0200,0.0271,0.8280 6.750,0.7278,0.01830,0.01108,-0.0200,0.0259,0.8312 7.000,0.7572,0.01936,0.01217,-0.0206,0.0252,0.8346 7.250,0.7903,0.02118,0.01408,-0.0220,0.0248,0.8381 7.500,0.8178,0.02295,0.01606,-0.0221,0.0244,0.8421 7.750,0.8396,0.02337,0.01669,-0.0210,0.0236,0.8463 8.000,0.8647,0.02559,0.01919,-0.0206,0.0237,0.8501 8.250,0.8854,0.02740,0.02125,-0.0195,0.0236,0.8548 8.500,0.9010,0.02989,0.02410,-0.0175,0.0235,0.8595 8.750,0.9158,0.03249,0.02703,-0.0157,0.0236,0.8648 9.000,0.8043,0.03008,0.02641,0.0035,0.0329,0.8586 9.250,0.8057,0.03276,0.02926,0.0061,0.0321,0.8641 9.500,0.8010,0.03547,0.03209,0.0094,0.0318,0.8711 9.750,0.7893,0.03892,0.03575,0.0129,0.0317,0.8784 10.000,0.7843,0.04173,0.03869,0.0149,0.0314,0.8859 10.250,0.7811,0.04471,0.04179,0.0161,0.0311,0.8942 10.500,0.7676,0.04865,0.04589,0.0172,0.0309,0.9033 10.750,0.7461,0.05338,0.05079,0.0176,0.0309,0.9140 11.000,0.7307,0.05868,0.05624,0.0163,0.0307,0.9209 11.250,0.5777,0.08579,0.08362,0.0015,0.0320,0.9059