Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-cp-080-050-gn-1000000 Airfoil,cp-080-050-gn Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,50.7179 Max Cl/Cd alpha,8.25 Url,http://airfoiltools.com/polar/csv?polar=xf-cp-080-050-gn-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.0603,0.10778,0.10578,-0.0956,0.9757,0.0358 -9.250,-0.0505,0.10453,0.10252,-0.0975,0.9748,0.0368 -9.000,-0.0533,0.09919,0.09716,-0.1013,0.9739,0.0374 -8.750,-0.0381,0.09626,0.09424,-0.1025,0.9733,0.0375 -8.500,-0.0239,0.09351,0.09149,-0.1041,0.9726,0.0377 -8.250,-0.0092,0.09088,0.08886,-0.1059,0.9720,0.0379 -8.000,0.0056,0.08805,0.08604,-0.1080,0.9713,0.0382 -7.750,0.0193,0.08526,0.08325,-0.1100,0.9707,0.0387 -7.500,0.0314,0.08239,0.08038,-0.1117,0.9685,0.0392 -7.250,0.0342,0.07848,0.07646,-0.1142,0.9646,0.0408 -7.000,0.0419,0.07372,0.07168,-0.1183,0.9616,0.0410 -6.750,0.0565,0.07103,0.06900,-0.1195,0.9612,0.0411 -6.500,0.0795,0.06800,0.06596,-0.1226,0.9588,0.0413 -6.250,0.1001,0.06516,0.06311,-0.1256,0.9572,0.0415 -6.000,0.1135,0.06276,0.06071,-0.1270,0.9525,0.0418 -5.750,0.1285,0.06031,0.05826,-0.1289,0.9471,0.0423 -5.500,0.1496,0.05721,0.05513,-0.1327,0.9427,0.0431 -5.250,0.1337,0.05275,0.05062,-0.1379,0.9311,0.0446 -5.000,0.1534,0.04978,0.04763,-0.1387,0.9270,0.0448 -4.750,0.1627,0.04796,0.04581,-0.1376,0.9181,0.0449 -4.500,0.1749,0.04597,0.04380,-0.1381,0.9111,0.0450 -4.250,0.1800,0.04442,0.04224,-0.1370,0.9030,0.0452 -4.000,0.1860,0.04271,0.04050,-0.1367,0.8937,0.0454 -3.750,0.1942,0.04106,0.03885,-0.1367,0.8859,0.0458 -3.500,0.2033,0.03913,0.03689,-0.1372,0.8774,0.0462 -3.250,0.2124,0.03716,0.03489,-0.1378,0.8678,0.0469 -3.000,0.2164,0.03120,0.02879,-0.1466,0.8615,0.0486 -2.750,0.2304,0.02939,0.02694,-0.1460,0.8534,0.0488 -2.500,0.2451,0.02787,0.02541,-0.1454,0.8438,0.0489 -2.250,0.2614,0.02640,0.02390,-0.1452,0.8347,0.0490 -2.000,0.2780,0.02500,0.02247,-0.1450,0.8244,0.0493 -1.750,0.2946,0.02364,0.02105,-0.1449,0.8093,0.0496 -1.500,0.3114,0.02226,0.01958,-0.1449,0.7912,0.0501 -1.250,0.3274,0.02093,0.01811,-0.1446,0.7649,0.0511 -1.000,0.3754,0.03047,0.02722,-0.1611,0.7744,0.0529 -0.750,0.3800,0.03005,0.02648,-0.1568,0.7073,0.0531 -0.500,0.3698,0.03055,0.02630,-0.1492,0.5584,0.0532 -0.250,0.3450,0.03230,0.02675,-0.1393,0.2292,0.0532 0.000,0.3501,0.03242,0.02634,-0.1354,0.0587,0.0533 0.250,0.3698,0.03162,0.02549,-0.1344,0.0545,0.0536 0.500,0.3902,0.03078,0.02462,-0.1334,0.0528,0.0540 0.750,0.4111,0.02978,0.02356,-0.1325,0.0512,0.0547 1.000,0.4382,0.02538,0.01878,-0.1328,0.0506,0.0576 1.250,0.4572,0.02486,0.01825,-0.1312,0.0494,0.0578 1.500,0.4762,0.02435,0.01772,-0.1296,0.0490,0.0581 1.750,0.4948,0.02386,0.01720,-0.1278,0.0484,0.0585 2.000,0.5138,0.02332,0.01662,-0.1260,0.0480,0.0591 2.250,0.5337,0.02255,0.01576,-0.1243,0.0475,0.0604 2.500,0.5554,0.02013,0.01301,-0.1225,0.0472,0.0629 2.750,0.5747,0.01985,0.01271,-0.1207,0.0467,0.0632 3.000,0.5944,0.01958,0.01241,-0.1190,0.0463,0.0637 3.250,0.6143,0.01927,0.01205,-0.1172,0.0459,0.0644 3.500,0.6356,0.01817,0.01064,-0.1152,0.0454,0.0682 3.750,0.6549,0.01801,0.01047,-0.1134,0.0451,0.0686 4.000,0.6727,0.01800,0.01044,-0.1112,0.0444,0.0690 4.250,0.6888,0.01812,0.01054,-0.1087,0.0439,0.0697 4.500,0.7082,0.01806,0.01044,-0.1067,0.0437,0.0711 4.750,0.7291,0.01778,0.00994,-0.1048,0.0435,0.0742 5.000,0.7483,0.01775,0.00993,-0.1029,0.0433,0.0748 5.250,0.7675,0.01782,0.00999,-0.1010,0.0431,0.0755 5.500,0.7864,0.01794,0.01010,-0.0989,0.0429,0.0767 5.750,0.8053,0.01807,0.01012,-0.0968,0.0427,0.0810 6.000,0.8237,0.01817,0.01024,-0.0948,0.0425,0.0818 6.250,0.8423,0.01835,0.01042,-0.0928,0.0422,0.0830 6.500,0.8608,0.01859,0.01063,-0.0907,0.0420,0.0845 6.750,0.8798,0.01879,0.01080,-0.0888,0.0418,0.0890 7.000,0.8985,0.01901,0.01103,-0.0868,0.0415,0.0900 7.250,0.9187,0.01844,0.01019,-0.0843,0.0412,0.0676 7.500,0.9377,0.01863,0.01038,-0.0824,0.0409,0.0679 7.750,0.9568,0.01892,0.01069,-0.0805,0.0406,0.0683 8.000,0.9764,0.01929,0.01107,-0.0788,0.0404,0.0685 8.250,0.9961,0.01964,0.01143,-0.0771,0.0401,0.0688 8.500,1.0164,0.02005,0.01184,-0.0755,0.0398,0.0692 8.750,1.0380,0.02053,0.01232,-0.0741,0.0396,0.0696 9.000,1.0644,0.02123,0.01301,-0.0737,0.0392,0.0704 9.250,1.1100,0.02253,0.01428,-0.0767,0.0388,0.0717 9.500,1.1285,0.02285,0.01465,-0.0747,0.0387,0.0721 9.750,1.1475,0.02320,0.01507,-0.0728,0.0385,0.0728 10.000,1.1702,0.02370,0.01561,-0.0717,0.0383,0.0737 10.250,1.1947,0.02428,0.01625,-0.0708,0.0381,0.0754 10.500,1.2181,0.02485,0.01687,-0.0698,0.0379,0.0767 10.750,1.2406,0.02545,0.01753,-0.0686,0.0375,0.0789 11.000,1.2638,0.02611,0.01825,-0.0676,0.0371,0.0831 11.250,1.2872,0.02681,0.01905,-0.0667,0.0369,0.1059 11.500,1.3464,0.02708,0.02083,-0.0736,0.0364,1.0000 11.750,1.3670,0.02786,0.02163,-0.0723,0.0362,1.0000 12.000,1.3864,0.02861,0.02241,-0.0707,0.0359,1.0000 12.250,1.4053,0.02938,0.02321,-0.0691,0.0357,1.0000 12.500,1.4246,0.03025,0.02411,-0.0676,0.0355,1.0000 12.750,1.4425,0.03105,0.02493,-0.0659,0.0354,1.0000 13.000,1.4579,0.03173,0.02562,-0.0639,0.0352,1.0000 13.250,1.4746,0.03260,0.02652,-0.0621,0.0350,1.0000 13.500,1.4926,0.03369,0.02764,-0.0606,0.0348,1.0000 13.750,1.5129,0.03524,0.02924,-0.0596,0.0346,1.0000 14.000,1.5236,0.03856,0.03283,-0.0577,0.0341,1.0000 14.250,1.5241,0.03925,0.03365,-0.0535,0.0339,1.0000 14.500,1.5258,0.04064,0.03521,-0.0498,0.0337,1.0000 14.750,1.5270,0.04246,0.03721,-0.0463,0.0335,1.0000 15.000,1.5242,0.04467,0.03964,-0.0426,0.0333,1.0000 15.250,1.5186,0.04723,0.04242,-0.0388,0.0330,1.0000 15.500,1.5072,0.05025,0.04567,-0.0348,0.0328,1.0000 15.750,1.4946,0.05322,0.04886,-0.0310,0.0326,1.0000 16.000,1.4774,0.05668,0.05254,-0.0274,0.0324,1.0000 16.250,1.4553,0.06065,0.05674,-0.0239,0.0323,1.0000 16.500,1.4184,0.06645,0.06283,-0.0207,0.0323,1.0000 16.750,1.3822,0.07235,0.06900,-0.0186,0.0322,1.0000 17.000,1.3552,0.07749,0.07432,-0.0177,0.0321,1.0000 17.250,1.3080,0.08574,0.08283,-0.0183,0.0321,1.0000 17.500,1.1996,0.10534,0.10291,-0.0267,0.0328,1.0000