Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe187-il-100000-n5 Airfoil,goe187-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,58.2213 Max Cl/Cd alpha,6.75 Url,http://airfoiltools.com/polar/csv?polar=xf-goe187-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.3076,0.10640,0.10180,-0.0253,1.0000,0.0244 -8.000,-0.3051,0.10407,0.09954,-0.0268,1.0000,0.0245 -7.750,-0.3032,0.10176,0.09732,-0.0282,1.0000,0.0245 -7.500,-0.2984,0.09924,0.09486,-0.0306,1.0000,0.0246 -7.250,-0.2932,0.09668,0.09237,-0.0328,1.0000,0.0247 -7.000,-0.2882,0.09415,0.08991,-0.0347,1.0000,0.0247 -6.750,-0.2836,0.09169,0.08751,-0.0362,1.0000,0.0248 -6.500,-0.2808,0.08942,0.08528,-0.0368,1.0000,0.0248 -6.250,-0.2680,0.08414,0.08008,-0.0388,0.9955,0.0252 -6.000,-0.2568,0.07868,0.07467,-0.0375,0.9896,0.0262 -5.750,-0.2310,0.07416,0.07010,-0.0424,0.9807,0.0273 -5.500,-0.2008,0.06972,0.06560,-0.0488,0.9709,0.0285 -5.250,-0.1680,0.06534,0.06114,-0.0555,0.9608,0.0299 -5.000,-0.1332,0.06106,0.05675,-0.0622,0.9506,0.0315 -4.750,-0.0918,0.05699,0.05249,-0.0697,0.9408,0.0338 -4.500,-0.0418,0.05434,0.04936,-0.0773,0.9290,0.0352 -4.250,-0.0135,0.04948,0.04441,-0.0805,0.9174,0.0359 -4.000,0.0099,0.04526,0.04018,-0.0824,0.9040,0.0376 -3.750,0.0403,0.04208,0.03680,-0.0846,0.8886,0.0400 -3.500,0.0735,0.03935,0.03375,-0.0866,0.8726,0.0433 -3.250,0.1085,0.03692,0.03081,-0.0882,0.8576,0.0478 -3.000,0.1317,0.03399,0.02784,-0.0888,0.8437,0.0529 -2.750,0.1603,0.03180,0.02533,-0.0896,0.8303,0.0652 -2.500,0.1902,0.03084,0.02389,-0.0901,0.8172,0.0877 -2.000,0.2556,0.02543,0.01769,-0.0888,0.7942,0.0310 -1.750,0.2862,0.02366,0.01547,-0.0883,0.7830,0.0279 -1.500,0.3166,0.02233,0.01362,-0.0876,0.7715,0.0260 -1.250,0.3444,0.02101,0.01208,-0.0874,0.7595,0.0280 -1.000,0.3728,0.01999,0.01079,-0.0869,0.7479,0.0303 -0.750,0.4011,0.01896,0.00950,-0.0863,0.7366,0.0307 -0.500,0.4289,0.01807,0.00839,-0.0856,0.7255,0.0318 -0.250,0.4561,0.01745,0.00760,-0.0849,0.7134,0.0359 0.000,0.4822,0.01664,0.00677,-0.0844,0.7013,0.0397 0.250,0.5091,0.01624,0.00618,-0.0839,0.6892,0.0455 0.500,0.5363,0.01587,0.00561,-0.0835,0.6768,0.0557 0.750,0.5643,0.01562,0.00520,-0.0832,0.6639,0.0758 1.000,0.5945,0.01347,0.00498,-0.0836,0.6508,1.0000 1.250,0.6212,0.01363,0.00483,-0.0832,0.6371,1.0000 1.500,0.6478,0.01380,0.00478,-0.0828,0.6233,1.0000 1.750,0.6742,0.01397,0.00476,-0.0824,0.6087,1.0000 2.000,0.7006,0.01415,0.00479,-0.0821,0.5933,1.0000 2.250,0.7268,0.01434,0.00484,-0.0817,0.5775,1.0000 2.500,0.7530,0.01454,0.00493,-0.0814,0.5616,1.0000 2.750,0.7791,0.01476,0.00504,-0.0811,0.5464,1.0000 3.000,0.8052,0.01500,0.00518,-0.0807,0.5319,1.0000 3.250,0.8311,0.01525,0.00536,-0.0804,0.5180,1.0000 3.500,0.8570,0.01552,0.00554,-0.0801,0.5048,1.0000 3.750,0.8828,0.01581,0.00575,-0.0798,0.4930,1.0000 4.000,0.9085,0.01612,0.00604,-0.0795,0.4813,1.0000 4.250,0.9340,0.01644,0.00632,-0.0791,0.4689,1.0000 4.500,0.9589,0.01677,0.00660,-0.0787,0.4552,1.0000 4.750,0.9836,0.01712,0.00690,-0.0782,0.4408,1.0000 5.000,1.0081,0.01749,0.00727,-0.0778,0.4270,1.0000 5.250,1.0327,0.01786,0.00764,-0.0773,0.4145,1.0000 5.500,1.0572,0.01825,0.00804,-0.0769,0.4036,1.0000 5.750,1.0816,0.01864,0.00851,-0.0765,0.3932,1.0000 6.000,1.1064,0.01903,0.00901,-0.0761,0.3840,1.0000 6.250,1.1308,0.01944,0.00949,-0.0757,0.3760,1.0000 6.500,1.1547,0.01984,0.01002,-0.0752,0.3651,1.0000 6.750,1.1784,0.02024,0.01061,-0.0747,0.3540,1.0000 7.000,1.2018,0.02067,0.01118,-0.0741,0.3439,1.0000 7.250,1.2246,0.02112,0.01175,-0.0735,0.3329,1.0000 7.500,1.2475,0.02155,0.01242,-0.0728,0.3211,1.0000 7.750,1.2697,0.02201,0.01315,-0.0721,0.3082,1.0000 8.000,1.2895,0.02250,0.01379,-0.0710,0.2852,1.0000 8.250,1.3030,0.02331,0.01439,-0.0692,0.2220,1.0000 8.500,1.3078,0.02517,0.01564,-0.0667,0.1570,1.0000 8.750,1.3173,0.02679,0.01705,-0.0647,0.1142,1.0000 9.000,1.3243,0.02855,0.01861,-0.0624,0.0866,1.0000 9.250,1.3241,0.03078,0.02052,-0.0594,0.0291,1.0000 9.500,1.3203,0.03298,0.02265,-0.0558,0.0201,1.0000 9.750,1.3206,0.03481,0.02466,-0.0527,0.0178,1.0000 10.000,1.3202,0.03685,0.02691,-0.0500,0.0164,1.0000 10.250,1.3179,0.03921,0.02949,-0.0477,0.0151,1.0000 10.500,1.3131,0.04200,0.03259,-0.0458,0.0140,1.0000 10.750,1.3075,0.04510,0.03592,-0.0445,0.0132,1.0000 11.000,1.3045,0.04811,0.03917,-0.0437,0.0127,1.0000 11.250,1.2995,0.05154,0.04283,-0.0432,0.0123,1.0000 11.500,1.2931,0.05530,0.04682,-0.0431,0.0120,1.0000 11.750,1.2857,0.05937,0.05110,-0.0434,0.0118,1.0000 12.000,1.2775,0.06366,0.05559,-0.0438,0.0116,1.0000 12.250,1.2689,0.06815,0.06028,-0.0445,0.0115,1.0000 12.500,1.2602,0.07274,0.06505,-0.0453,0.0113,1.0000 12.750,1.2517,0.07740,0.06988,-0.0462,0.0112,1.0000 13.000,1.2439,0.08203,0.07468,-0.0471,0.0111,1.0000 13.250,1.2371,0.08656,0.07936,-0.0480,0.0109,1.0000 13.500,1.2314,0.09099,0.08395,-0.0488,0.0107,1.0000