Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-giiib-il-50000-n5 Airfoil,giiib-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,29.5833 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-giiib-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.6297,0.09473,0.08788,-0.0160,1.0000,0.0467 -10.000,-0.6382,0.08825,0.08142,-0.0203,1.0000,0.0463 -9.750,-0.6509,0.08234,0.07550,-0.0238,1.0000,0.0459 -9.500,-0.6663,0.07717,0.07029,-0.0258,1.0000,0.0455 -9.250,-0.6824,0.07269,0.06572,-0.0259,1.0000,0.0452 -9.000,-0.6958,0.06831,0.06120,-0.0254,1.0000,0.0450 -8.750,-0.7053,0.06397,0.05665,-0.0244,1.0000,0.0449 -8.500,-0.7113,0.05972,0.05210,-0.0230,1.0000,0.0450 -8.250,-0.7138,0.05558,0.04761,-0.0213,1.0000,0.0452 -8.000,-0.7133,0.05163,0.04321,-0.0192,1.0000,0.0461 -7.750,-0.7100,0.04795,0.03892,-0.0168,1.0000,0.0476 -7.500,-0.7007,0.04484,0.03556,-0.0151,1.0000,0.0496 -7.250,-0.6874,0.04233,0.03283,-0.0136,1.0000,0.0517 -7.000,-0.6724,0.03956,0.02969,-0.0118,1.0000,0.0533 -6.750,-0.6549,0.03689,0.02661,-0.0102,1.0000,0.0554 -6.500,-0.6350,0.03453,0.02376,-0.0087,1.0000,0.0591 -6.250,-0.6149,0.03263,0.02168,-0.0076,1.0000,0.0641 -6.000,-0.5920,0.03087,0.01972,-0.0065,1.0000,0.0694 -5.750,-0.5665,0.02908,0.01772,-0.0057,1.0000,0.0755 -5.500,-0.5439,0.02787,0.01637,-0.0047,1.0000,0.0863 -5.250,-0.5207,0.02653,0.01506,-0.0037,1.0000,0.0970 -5.000,-0.4991,0.02544,0.01393,-0.0025,1.0000,0.1151 -4.750,-0.4802,0.02429,0.01285,-0.0010,1.0000,0.1373 -4.500,-0.4633,0.02320,0.01190,0.0007,1.0000,0.1726 -4.250,-0.4487,0.02204,0.01104,0.0026,1.0000,0.2222 -4.000,-0.4368,0.02076,0.01025,0.0049,1.0000,0.2987 -3.750,-0.4328,0.01913,0.00978,0.0091,1.0000,0.4574 -3.500,-0.4003,0.01898,0.01067,0.0119,1.0000,0.7459 -3.250,-0.3645,0.01962,0.01108,0.0129,1.0000,0.8282 -3.000,-0.3265,0.02014,0.01129,0.0126,1.0000,0.8741 -2.750,-0.2773,0.02057,0.01137,0.0096,1.0000,0.9078 -2.500,-0.1823,0.02102,0.01128,-0.0017,1.0000,0.9475 -2.250,-0.0916,0.02078,0.01062,-0.0136,1.0000,0.9788 -2.000,-0.0522,0.02041,0.01008,-0.0170,1.0000,0.9892 -1.750,-0.0159,0.02006,0.00961,-0.0199,1.0000,0.9980 -1.500,-0.0027,0.01993,0.00943,-0.0185,1.0000,1.0000 -1.250,0.0001,0.01993,0.00940,-0.0153,1.0000,1.0000 -1.000,0.0002,0.01998,0.00943,-0.0117,1.0000,1.0000 -0.750,-0.0013,0.02008,0.00950,-0.0078,1.0000,1.0000 -0.500,0.0163,0.02018,0.00954,-0.0074,0.9941,1.0000 -0.250,0.0587,0.02022,0.00951,-0.0115,0.9801,1.0000 0.000,0.1016,0.02026,0.00951,-0.0155,0.9667,1.0000 0.250,0.1447,0.02029,0.00952,-0.0194,0.9535,1.0000 0.500,0.1869,0.02031,0.00956,-0.0230,0.9402,1.0000 0.750,0.2263,0.02033,0.00961,-0.0258,0.9261,1.0000 1.000,0.2632,0.02036,0.00969,-0.0281,0.9114,1.0000 1.250,0.2988,0.02037,0.00976,-0.0299,0.8956,1.0000 1.500,0.3340,0.02026,0.00970,-0.0310,0.8750,1.0000 1.750,0.3656,0.02004,0.00953,-0.0308,0.8488,1.0000 2.000,0.3897,0.01988,0.00937,-0.0292,0.8204,1.0000 2.250,0.4105,0.01981,0.00934,-0.0272,0.7936,1.0000 2.500,0.4308,0.01981,0.00938,-0.0254,0.7695,1.0000 2.750,0.4517,0.01979,0.00943,-0.0235,0.7458,1.0000 3.000,0.4720,0.01978,0.00947,-0.0216,0.7210,1.0000 3.250,0.4921,0.01980,0.00954,-0.0196,0.6949,1.0000 3.500,0.5124,0.01983,0.00961,-0.0176,0.6673,1.0000 3.750,0.5326,0.01989,0.00972,-0.0156,0.6373,1.0000 4.000,0.5526,0.01999,0.00982,-0.0135,0.6050,1.0000 4.250,0.5718,0.02017,0.01000,-0.0115,0.5681,1.0000 4.500,0.5908,0.02043,0.01021,-0.0094,0.5279,1.0000 4.750,0.6095,0.02079,0.01050,-0.0074,0.4844,1.0000 5.000,0.6278,0.02126,0.01091,-0.0054,0.4406,1.0000 5.250,0.6461,0.02184,0.01136,-0.0036,0.4031,1.0000 5.500,0.6649,0.02250,0.01193,-0.0020,0.3725,1.0000 5.750,0.6841,0.02320,0.01260,-0.0005,0.3477,1.0000 6.000,0.7040,0.02393,0.01334,0.0008,0.3277,1.0000 6.250,0.7244,0.02471,0.01422,0.0020,0.3102,1.0000 6.500,0.7446,0.02552,0.01511,0.0033,0.2933,1.0000 6.750,0.7624,0.02634,0.01593,0.0049,0.2724,1.0000 7.000,0.7752,0.02709,0.01667,0.0070,0.2437,1.0000 7.250,0.7866,0.02783,0.01746,0.0092,0.2139,1.0000 7.500,0.7985,0.02863,0.01837,0.0112,0.1848,1.0000 8.000,0.8188,0.03087,0.02064,0.0156,0.1085,1.0000 8.250,0.8282,0.03251,0.02207,0.0177,0.0840,1.0000 8.500,0.8383,0.03434,0.02385,0.0198,0.0720,1.0000 8.750,0.8483,0.03622,0.02575,0.0218,0.0635,1.0000 9.000,0.8578,0.03808,0.02766,0.0236,0.0569,1.0000 9.250,0.8698,0.04023,0.02997,0.0254,0.0531,1.0000 9.500,0.8833,0.04248,0.03252,0.0271,0.0498,1.0000 9.750,0.8932,0.04471,0.03493,0.0287,0.0466,1.0000 10.000,0.9010,0.04723,0.03744,0.0301,0.0438,1.0000 10.250,0.9056,0.04993,0.04059,0.0319,0.0418,1.0000 10.500,0.9058,0.05283,0.04386,0.0338,0.0405,1.0000 10.750,0.9019,0.05604,0.04740,0.0355,0.0398,1.0000 11.000,0.8939,0.05959,0.05124,0.0366,0.0393,1.0000 11.250,0.8820,0.06358,0.05551,0.0369,0.0391,1.0000 11.500,0.8667,0.06818,0.06036,0.0361,0.0390,1.0000 11.750,0.8482,0.07361,0.06601,0.0340,0.0391,1.0000 12.000,0.8272,0.08012,0.07270,0.0304,0.0394,1.0000 12.250,0.8042,0.08789,0.08063,0.0255,0.0399,1.0000 12.500,0.7808,0.09689,0.08967,0.0196,0.0406,1.0000