Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-cp-060-050-gn-1000000-n1 Airfoil,cp-060-050-gn Reynolds number,1000000 Ncrit,1 Mach,0 Max Cl/Cd,64.1817 Max Cl/Cd alpha,11.5 Url,http://airfoiltools.com/polar/csv?polar=xf-cp-060-050-gn-1000000-n1 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -17.500,-0.5882,0.20612,0.20376,-0.0110,0.9999,0.0187 -17.250,-0.5799,0.20321,0.20085,-0.0130,0.9998,0.0191 -8.750,-0.7614,0.01921,0.01453,-0.1268,0.8812,0.0473 -8.500,-0.7434,0.01809,0.01326,-0.1258,0.8747,0.0476 -8.250,-0.7230,0.01727,0.01232,-0.1250,0.8689,0.0479 -8.000,-0.7015,0.01661,0.01154,-0.1242,0.8634,0.0482 -7.750,-0.6791,0.01601,0.01085,-0.1235,0.8578,0.0484 -7.500,-0.6561,0.01546,0.01022,-0.1228,0.8521,0.0486 -7.250,-0.6328,0.01497,0.00965,-0.1221,0.8468,0.0489 -7.000,-0.6092,0.01451,0.00910,-0.1214,0.8415,0.0492 -6.750,-0.5849,0.01410,0.00862,-0.1208,0.8358,0.0494 -6.500,-0.5594,0.01387,0.00837,-0.1203,0.8308,0.0496 -6.250,-0.5344,0.01362,0.00807,-0.1198,0.8252,0.0498 -6.000,-0.5090,0.01337,0.00777,-0.1192,0.8198,0.0500 -5.750,-0.4834,0.01312,0.00749,-0.1187,0.8140,0.0501 -5.500,-0.4579,0.01287,0.00720,-0.1181,0.8081,0.0503 -5.250,-0.4325,0.01266,0.00694,-0.1175,0.8023,0.0505 -5.000,-0.4067,0.01240,0.00664,-0.1170,0.7967,0.0507 -4.750,-0.3812,0.01219,0.00639,-0.1164,0.7889,0.0509 -4.500,-0.3572,0.01203,0.00615,-0.1154,0.7709,0.0512 -4.250,-0.3359,0.01197,0.00592,-0.1138,0.7354,0.0514 -4.000,-0.3157,0.01197,0.00572,-0.1120,0.6889,0.0517 -3.750,-0.3137,0.01293,0.00576,-0.1067,0.4377,0.0520 -3.500,-0.3052,0.01385,0.00577,-0.1029,0.0658,0.0522 -3.250,-0.2796,0.01369,0.00555,-0.1023,0.0572,0.0525 -3.000,-0.2540,0.01352,0.00533,-0.1016,0.0542,0.0527 -2.750,-0.2282,0.01337,0.00514,-0.1009,0.0528,0.0529 -2.500,-0.2024,0.01321,0.00494,-0.1002,0.0515,0.0530 -2.250,-0.1766,0.01307,0.00476,-0.0995,0.0504,0.0532 -2.000,-0.1508,0.01294,0.00459,-0.0988,0.0495,0.0534 -1.750,-0.1249,0.01283,0.00445,-0.0981,0.0490,0.0535 -1.500,-0.0988,0.01276,0.00435,-0.0973,0.0485,0.0537 -1.250,-0.0728,0.01268,0.00425,-0.0966,0.0482,0.0539 -1.000,-0.0468,0.01262,0.00416,-0.0959,0.0478,0.0541 -0.750,-0.0209,0.01256,0.00408,-0.0951,0.0474,0.0543 -0.500,0.0051,0.01250,0.00400,-0.0943,0.0470,0.0546 -0.250,0.0309,0.01245,0.00393,-0.0935,0.0464,0.0550 0.000,0.0567,0.01240,0.00385,-0.0927,0.0458,0.0553 0.250,0.0825,0.01235,0.00378,-0.0918,0.0455,0.0556 0.500,0.1081,0.01230,0.00370,-0.0910,0.0452,0.0559 0.750,0.1337,0.01225,0.00364,-0.0900,0.0449,0.0561 1.000,0.1592,0.01221,0.00358,-0.0891,0.0448,0.0563 1.250,0.1846,0.01218,0.00352,-0.0882,0.0446,0.0565 1.500,0.2100,0.01216,0.00348,-0.0872,0.0444,0.0567 1.750,0.2353,0.01214,0.00344,-0.0862,0.0442,0.0569 2.000,0.2605,0.01213,0.00342,-0.0852,0.0441,0.0571 2.250,0.2857,0.01213,0.00340,-0.0842,0.0440,0.0572 2.500,0.3108,0.01213,0.00339,-0.0831,0.0439,0.0574 2.750,0.3358,0.01214,0.00339,-0.0820,0.0438,0.0575 3.000,0.3607,0.01216,0.00340,-0.0809,0.0437,0.0577 3.250,0.3856,0.01220,0.00344,-0.0798,0.0436,0.0580 3.500,0.4104,0.01224,0.00348,-0.0787,0.0435,0.0583 3.750,0.4350,0.01229,0.00352,-0.0775,0.0434,0.0585 4.000,0.4595,0.01234,0.00357,-0.0763,0.0433,0.0587 4.250,0.4838,0.01239,0.00362,-0.0750,0.0432,0.0588 4.500,0.5080,0.01245,0.00368,-0.0738,0.0431,0.0591 4.750,0.5320,0.01252,0.00375,-0.0724,0.0430,0.0593 5.000,0.5558,0.01259,0.00382,-0.0711,0.0429,0.0594 5.250,0.5795,0.01267,0.00390,-0.0697,0.0427,0.0597 5.500,0.6030,0.01275,0.00399,-0.0683,0.0424,0.0599 5.750,0.6263,0.01285,0.00408,-0.0668,0.0422,0.0602 6.000,0.6492,0.01294,0.00418,-0.0653,0.0419,0.0606 6.250,0.6713,0.01304,0.00428,-0.0636,0.0418,0.0609 6.500,0.6928,0.01313,0.00438,-0.0617,0.0416,0.0610 6.750,0.7141,0.01324,0.00450,-0.0598,0.0414,0.0613 7.000,0.7353,0.01335,0.00462,-0.0580,0.0413,0.0613 7.250,0.7566,0.01348,0.00475,-0.0561,0.0412,0.0615 7.500,0.7778,0.01361,0.00490,-0.0542,0.0410,0.0616 7.750,0.7989,0.01377,0.00506,-0.0524,0.0409,0.0618 8.000,0.8200,0.01394,0.00524,-0.0505,0.0407,0.0619 8.250,0.8412,0.01411,0.00542,-0.0487,0.0406,0.0619 8.500,0.8622,0.01430,0.00562,-0.0468,0.0405,0.0621 8.750,0.8834,0.01447,0.00579,-0.0450,0.0401,0.0622 9.000,0.9040,0.01467,0.00601,-0.0431,0.0400,0.0623 9.250,0.9247,0.01487,0.00623,-0.0412,0.0399,0.0625 9.500,0.9453,0.01508,0.00645,-0.0393,0.0397,0.0626 9.750,0.9655,0.01531,0.00670,-0.0373,0.0396,0.0629 10.000,0.9855,0.01555,0.00696,-0.0354,0.0395,0.0632 10.250,1.0053,0.01580,0.00723,-0.0334,0.0394,0.0635 10.500,1.0250,0.01605,0.00751,-0.0314,0.0394,0.0641 10.750,1.0446,0.01631,0.00779,-0.0294,0.0392,0.0645 11.000,1.0638,0.01659,0.00810,-0.0274,0.0392,0.0650 11.250,1.0828,0.01688,0.00841,-0.0254,0.0391,0.0651 11.500,1.1020,0.01717,0.00873,-0.0234,0.0390,0.0655 11.750,1.1206,0.01749,0.00907,-0.0213,0.0388,0.0658 12.000,1.1390,0.01781,0.00942,-0.0193,0.0388,0.0663 12.250,1.1574,0.01814,0.00979,-0.0172,0.0386,0.0663 12.500,1.1755,0.01849,0.01017,-0.0152,0.0385,0.0671 12.750,1.1933,0.01886,0.01056,-0.0131,0.0384,0.0675 13.000,1.2109,0.01924,0.01097,-0.0110,0.0382,0.0680 13.250,1.2285,0.01962,0.01140,-0.0090,0.0381,0.0695 13.500,1.2459,0.02002,0.01182,-0.0069,0.0379,0.0704 13.750,1.2630,0.02042,0.01226,-0.0049,0.0375,0.0714 14.250,1.2967,0.02131,0.01322,-0.0008,0.0373,0.0752 14.500,1.3132,0.02174,0.01370,0.0012,0.0369,0.0990 15.250,1.4319,0.02254,0.01611,-0.0069,0.0363,1.0000 15.500,1.4483,0.02314,0.01673,-0.0051,0.0362,1.0000 15.750,1.4643,0.02374,0.01736,-0.0032,0.0361,1.0000 16.000,1.4804,0.02436,0.01799,-0.0014,0.0360,1.0000 16.250,1.4962,0.02500,0.01866,0.0004,0.0358,1.0000 16.500,1.5113,0.02569,0.01937,0.0023,0.0358,1.0000 16.750,1.5256,0.02645,0.02016,0.0041,0.0356,1.0000 17.000,1.5399,0.02722,0.02097,0.0059,0.0355,1.0000 17.250,1.5533,0.02806,0.02185,0.0078,0.0355,1.0000 17.500,1.5667,0.02890,0.02273,0.0095,0.0354,1.0000 17.750,1.5793,0.02982,0.02369,0.0113,0.0352,1.0000 18.000,1.5920,0.03073,0.02464,0.0130,0.0350,1.0000 18.250,1.6044,0.03169,0.02565,0.0147,0.0348,1.0000 18.500,1.6161,0.03272,0.02671,0.0164,0.0345,1.0000 18.750,1.6275,0.03378,0.02782,0.0180,0.0344,1.0000 19.000,1.6379,0.03493,0.02903,0.0196,0.0342,1.0000 19.250,1.6483,0.03612,0.03027,0.0211,0.0341,1.0000