Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-giiih-il-50000-n5 Airfoil,giiih-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,32.7009 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-giiih-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.4463,0.10610,0.09953,-0.0106,1.0000,0.1234 -9.500,-0.4642,0.10310,0.09663,-0.0140,1.0000,0.1276 -9.250,-0.4616,0.09847,0.09204,-0.0143,1.0000,0.1298 -9.000,-0.4550,0.09417,0.08775,-0.0141,1.0000,0.1320 -8.750,-0.4556,0.09002,0.08364,-0.0150,1.0000,0.1335 -8.500,-0.4599,0.08569,0.07936,-0.0166,1.0000,0.1336 -8.000,-0.5791,0.08101,0.07412,-0.0254,1.0000,0.0576 -7.500,-0.5688,0.07235,0.06534,-0.0262,1.0000,0.0557 -7.250,-0.5638,0.06806,0.06096,-0.0267,1.0000,0.0541 -7.000,-0.5580,0.06375,0.05649,-0.0272,1.0000,0.0526 -6.750,-0.5508,0.05948,0.05200,-0.0273,1.0000,0.0512 -6.500,-0.5419,0.05533,0.04757,-0.0270,1.0000,0.0501 -6.250,-0.5312,0.05137,0.04327,-0.0263,1.0000,0.0493 -6.000,-0.5189,0.04767,0.03919,-0.0253,1.0000,0.0489 -5.750,-0.5049,0.04461,0.03579,-0.0241,1.0000,0.0503 -5.500,-0.4897,0.04184,0.03264,-0.0228,1.0000,0.0530 -5.250,-0.4732,0.03905,0.02937,-0.0213,1.0000,0.0549 -5.000,-0.4551,0.03633,0.02619,-0.0197,1.0000,0.0555 -4.750,-0.4353,0.03382,0.02321,-0.0182,1.0000,0.0563 -4.500,-0.4138,0.03160,0.02046,-0.0167,1.0000,0.0575 -4.250,-0.3927,0.02950,0.01815,-0.0157,1.0000,0.0606 -4.000,-0.3714,0.02806,0.01657,-0.0146,1.0000,0.0666 -3.750,-0.3471,0.02651,0.01469,-0.0134,1.0000,0.0708 -3.500,-0.3223,0.02498,0.01307,-0.0124,1.0000,0.0750 -3.250,-0.2993,0.02405,0.01196,-0.0113,1.0000,0.0854 -3.000,-0.2767,0.02294,0.01081,-0.0103,1.0000,0.0935 -2.750,-0.2558,0.02203,0.00976,-0.0090,1.0000,0.1021 -2.500,-0.2373,0.02125,0.00901,-0.0077,1.0000,0.1196 -2.250,-0.2183,0.02046,0.00822,-0.0064,1.0000,0.1423 -2.000,-0.0587,0.01733,0.00771,-0.0247,1.0000,1.0000 -1.750,-0.0536,0.01724,0.00750,-0.0215,1.0000,1.0000 -1.500,-0.0510,0.01720,0.00734,-0.0179,1.0000,1.0000 -1.250,-0.0495,0.01720,0.00721,-0.0142,1.0000,1.0000 -1.000,-0.0470,0.01723,0.00709,-0.0106,1.0000,1.0000 -0.750,-0.0423,0.01729,0.00701,-0.0074,1.0000,1.0000 -0.500,-0.0343,0.01739,0.00696,-0.0048,1.0000,1.0000 -0.250,-0.0056,0.01759,0.00699,-0.0060,0.9939,1.0000 0.000,0.0316,0.01783,0.00708,-0.0089,0.9847,1.0000 0.250,0.0693,0.01808,0.00720,-0.0117,0.9757,1.0000 0.500,0.1056,0.01833,0.00737,-0.0142,0.9658,1.0000 0.750,0.1415,0.01857,0.00757,-0.0166,0.9554,1.0000 1.000,0.1787,0.01882,0.00780,-0.0191,0.9449,1.0000 1.250,0.2192,0.01905,0.00804,-0.0221,0.9340,1.0000 1.500,0.2623,0.01924,0.00828,-0.0255,0.9227,1.0000 1.750,0.3012,0.01940,0.00853,-0.0278,0.9098,1.0000 2.000,0.3365,0.01955,0.00877,-0.0294,0.8962,1.0000 2.250,0.3701,0.01970,0.00903,-0.0305,0.8823,1.0000 2.500,0.4025,0.01984,0.00933,-0.0313,0.8680,1.0000 2.750,0.4334,0.01995,0.00960,-0.0316,0.8529,1.0000 3.000,0.4604,0.02010,0.00990,-0.0312,0.8357,1.0000 3.250,0.4876,0.02021,0.01018,-0.0306,0.8179,1.0000 3.500,0.5155,0.02027,0.01048,-0.0299,0.7997,1.0000 3.750,0.5419,0.02030,0.01073,-0.0289,0.7795,1.0000 4.000,0.5671,0.02027,0.01091,-0.0274,0.7557,1.0000 4.250,0.5887,0.01999,0.01079,-0.0244,0.7177,1.0000 4.500,0.6078,0.01952,0.01039,-0.0205,0.6579,1.0000 4.750,0.6261,0.01936,0.01013,-0.0169,0.5799,1.0000 5.000,0.6429,0.01966,0.01002,-0.0134,0.4652,1.0000 5.250,0.6542,0.02096,0.01043,-0.0103,0.3182,1.0000 5.500,0.6644,0.02297,0.01157,-0.0081,0.1843,1.0000 5.750,0.6787,0.02488,0.01297,-0.0066,0.1285,1.0000 6.000,0.6958,0.02651,0.01452,-0.0052,0.1060,1.0000 6.250,0.7150,0.02808,0.01612,-0.0039,0.0927,1.0000 6.500,0.7353,0.02958,0.01765,-0.0029,0.0800,1.0000 6.750,0.7592,0.03117,0.01948,-0.0018,0.0722,1.0000 7.000,0.7840,0.03326,0.02156,-0.0011,0.0670,1.0000 7.250,0.8081,0.03512,0.02382,-0.0003,0.0602,1.0000 7.500,0.8299,0.03736,0.02618,0.0003,0.0554,1.0000 7.750,0.8522,0.04030,0.02956,0.0013,0.0533,1.0000 8.000,0.8706,0.04347,0.03331,0.0026,0.0513,1.0000 8.250,0.8845,0.04651,0.03687,0.0039,0.0482,1.0000 8.500,0.8972,0.04916,0.03977,0.0050,0.0449,1.0000 8.750,0.9072,0.05251,0.04336,0.0061,0.0432,1.0000 9.000,0.9129,0.05672,0.04789,0.0073,0.0424,1.0000 9.250,0.9128,0.06084,0.05242,0.0088,0.0421,1.0000 9.500,0.9085,0.06502,0.05700,0.0101,0.0420,1.0000 9.750,0.9003,0.06924,0.06154,0.0112,0.0419,1.0000 10.000,0.8879,0.07340,0.06594,0.0120,0.0419,1.0000 10.250,0.8722,0.07756,0.07027,0.0124,0.0420,1.0000 10.500,0.8562,0.08220,0.07503,0.0114,0.0421,1.0000 10.750,0.8408,0.08740,0.08033,0.0092,0.0423,1.0000