Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-giiie-il-100000-n5 Airfoil,giiie-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,44.598 Max Cl/Cd alpha,4.5 Url,http://airfoiltools.com/polar/csv?polar=xf-giiie-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.5900,0.08902,0.08432,-0.0098,1.0000,0.0233 -8.750,-0.5951,0.08309,0.07844,-0.0149,1.0000,0.0228 -8.500,-0.6032,0.07735,0.07272,-0.0194,1.0000,0.0224 -8.250,-0.6100,0.07188,0.06719,-0.0222,1.0000,0.0219 -8.000,-0.6139,0.06620,0.06140,-0.0243,1.0000,0.0215 -7.750,-0.6151,0.06058,0.05561,-0.0254,1.0000,0.0212 -7.500,-0.6130,0.05531,0.05011,-0.0257,1.0000,0.0211 -7.250,-0.6062,0.05130,0.04588,-0.0253,1.0000,0.0219 -7.000,-0.5976,0.04736,0.04166,-0.0247,1.0000,0.0231 -6.750,-0.5881,0.04313,0.03701,-0.0235,1.0000,0.0242 -6.500,-0.5775,0.03886,0.03228,-0.0219,1.0000,0.0247 -6.250,-0.5649,0.03488,0.02778,-0.0201,1.0000,0.0250 -6.000,-0.5499,0.03141,0.02378,-0.0182,1.0000,0.0256 -5.750,-0.5325,0.02850,0.02034,-0.0163,1.0000,0.0265 -5.500,-0.5130,0.02649,0.01784,-0.0146,1.0000,0.0282 -5.250,-0.4950,0.02454,0.01574,-0.0133,1.0000,0.0310 -5.000,-0.4754,0.02307,0.01410,-0.0119,1.0000,0.0331 -4.750,-0.4557,0.02165,0.01249,-0.0104,1.0000,0.0352 -4.500,-0.4368,0.02044,0.01110,-0.0087,1.0000,0.0378 -4.250,-0.4135,0.01939,0.00994,-0.0083,0.9974,0.0431 -4.000,-0.3793,0.01838,0.00882,-0.0098,0.9899,0.0510 -3.750,-0.3460,0.01738,0.00780,-0.0113,0.9824,0.0625 -3.500,-0.3118,0.01661,0.00710,-0.0130,0.9755,0.0874 -3.250,-0.2795,0.01594,0.00653,-0.0143,0.9674,0.1230 -3.000,-0.2479,0.01529,0.00601,-0.0155,0.9594,0.1680 -2.750,-0.2172,0.01441,0.00554,-0.0168,0.9521,0.2619 -2.500,-0.2015,0.01256,0.00558,-0.0142,0.9436,0.6972 -2.250,-0.1715,0.01258,0.00571,-0.0133,0.9377,0.8027 -2.000,-0.1420,0.01269,0.00573,-0.0126,0.9299,0.8508 -1.750,-0.1063,0.01284,0.00576,-0.0132,0.9246,0.8851 -1.500,-0.0700,0.01299,0.00579,-0.0142,0.9182,0.9124 -1.250,-0.0222,0.01320,0.00584,-0.0174,0.9147,0.9405 -1.000,0.0351,0.01330,0.00580,-0.0229,0.9127,0.9619 -0.750,0.0744,0.01323,0.00563,-0.0256,0.9054,0.9679 -0.500,0.1100,0.01316,0.00546,-0.0275,0.8976,0.9731 -0.250,0.1450,0.01310,0.00534,-0.0293,0.8891,0.9783 0.000,0.1804,0.01304,0.00522,-0.0311,0.8819,0.9833 0.250,0.2150,0.01300,0.00516,-0.0329,0.8731,0.9887 0.500,0.2496,0.01296,0.00510,-0.0347,0.8653,0.9943 0.750,0.2845,0.01291,0.00505,-0.0364,0.8560,0.9994 1.000,0.3082,0.01290,0.00505,-0.0357,0.8430,1.0000 1.250,0.3298,0.01289,0.00502,-0.0344,0.8283,1.0000 1.500,0.3512,0.01289,0.00501,-0.0330,0.8137,1.0000 1.750,0.3732,0.01293,0.00506,-0.0319,0.8006,1.0000 2.000,0.3954,0.01299,0.00517,-0.0308,0.7885,1.0000 2.250,0.4177,0.01305,0.00528,-0.0298,0.7762,1.0000 2.500,0.4401,0.01312,0.00540,-0.0287,0.7637,1.0000 2.750,0.4624,0.01319,0.00554,-0.0276,0.7504,1.0000 3.000,0.4847,0.01325,0.00568,-0.0264,0.7361,1.0000 3.250,0.5070,0.01331,0.00587,-0.0252,0.7202,1.0000 3.500,0.5292,0.01335,0.00599,-0.0239,0.7020,1.0000 3.750,0.5508,0.01335,0.00608,-0.0224,0.6764,1.0000 4.000,0.5713,0.01331,0.00603,-0.0204,0.6363,1.0000 4.250,0.5911,0.01338,0.00602,-0.0182,0.5795,1.0000 4.500,0.6101,0.01368,0.00608,-0.0161,0.4989,1.0000 4.750,0.6246,0.01451,0.00627,-0.0136,0.3793,1.0000 5.000,0.6398,0.01557,0.00682,-0.0117,0.2797,1.0000 5.250,0.6547,0.01682,0.00748,-0.0100,0.1671,1.0000 5.500,0.6704,0.01816,0.00834,-0.0085,0.0939,1.0000 5.750,0.6882,0.01933,0.00933,-0.0070,0.0654,1.0000 6.000,0.7069,0.02038,0.01046,-0.0057,0.0527,1.0000 6.250,0.7247,0.02160,0.01175,-0.0041,0.0465,1.0000 6.500,0.7437,0.02270,0.01297,-0.0028,0.0411,1.0000 6.750,0.7613,0.02406,0.01433,-0.0015,0.0360,1.0000 7.000,0.7814,0.02544,0.01589,-0.0002,0.0333,1.0000 7.250,0.8021,0.02705,0.01766,0.0010,0.0308,1.0000 7.500,0.8220,0.02850,0.01918,0.0018,0.0277,1.0000 7.750,0.8415,0.03072,0.02163,0.0028,0.0252,1.0000 8.000,0.8621,0.03307,0.02434,0.0040,0.0240,1.0000 8.250,0.8801,0.03584,0.02754,0.0053,0.0230,1.0000 8.500,0.8947,0.03884,0.03100,0.0069,0.0220,1.0000 8.750,0.9065,0.04152,0.03407,0.0084,0.0205,1.0000 9.000,0.9169,0.04381,0.03665,0.0097,0.0190,1.0000 9.250,0.9238,0.04638,0.03948,0.0111,0.0180,1.0000 9.500,0.9255,0.04975,0.04318,0.0127,0.0176,1.0000 9.750,0.9223,0.05338,0.04714,0.0144,0.0174,1.0000 10.000,0.9141,0.05708,0.05113,0.0161,0.0173,1.0000 10.250,0.9005,0.06070,0.05500,0.0177,0.0172,1.0000 10.500,0.8845,0.06476,0.05929,0.0180,0.0173,1.0000 10.750,0.8661,0.06962,0.06436,0.0167,0.0174,1.0000 11.000,0.8447,0.07584,0.07080,0.0133,0.0176,1.0000 11.250,0.8181,0.08486,0.08000,0.0068,0.0181,1.0000