Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-eh0009-il-200000 Airfoil,eh0009-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,47.6976 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-eh0009-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.6738,0.08718,0.08386,-0.0061,1.0000,0.0574 -9.500,-0.6850,0.08025,0.07698,-0.0115,1.0000,0.0582 -9.250,-0.7791,0.05756,0.05377,-0.0239,1.0000,0.0266 -9.000,-0.7904,0.05390,0.04980,-0.0227,1.0000,0.0277 -8.750,-0.7986,0.04896,0.04464,-0.0216,1.0000,0.0265 -8.500,-0.8016,0.04433,0.03966,-0.0201,1.0000,0.0257 -8.250,-0.7976,0.04060,0.03552,-0.0184,1.0000,0.0264 -8.000,-0.7915,0.03635,0.03081,-0.0165,1.0000,0.0259 -7.750,-0.7815,0.03212,0.02607,-0.0144,1.0000,0.0250 -7.500,-0.7665,0.02869,0.02217,-0.0126,1.0000,0.0249 -7.250,-0.7478,0.02594,0.01902,-0.0110,1.0000,0.0255 -7.000,-0.7269,0.02373,0.01649,-0.0096,1.0000,0.0267 -6.750,-0.7044,0.02267,0.01512,-0.0085,1.0000,0.0291 -6.500,-0.6853,0.01989,0.01226,-0.0072,1.0000,0.0323 -6.250,-0.6642,0.01853,0.01084,-0.0059,1.0000,0.0357 -6.000,-0.6426,0.01745,0.00962,-0.0045,1.0000,0.0398 -5.750,-0.6243,0.01608,0.00829,-0.0029,1.0000,0.0486 -5.500,-0.6050,0.01497,0.00718,-0.0014,1.0000,0.0619 -5.250,-0.5872,0.01369,0.00613,0.0003,1.0000,0.0985 -5.000,-0.5692,0.01257,0.00540,0.0017,1.0000,0.1701 -4.750,-0.5497,0.01181,0.00492,0.0029,1.0000,0.2399 -4.500,-0.5296,0.01121,0.00458,0.0041,1.0000,0.3032 -4.250,-0.5092,0.01071,0.00429,0.0054,1.0000,0.3637 -4.000,-0.4892,0.01025,0.00407,0.0067,1.0000,0.4258 -3.750,-0.4689,0.00989,0.00389,0.0082,1.0000,0.4795 -3.500,-0.4483,0.00960,0.00373,0.0096,1.0000,0.5280 -3.250,-0.4279,0.00934,0.00359,0.0111,1.0000,0.5731 -3.000,-0.4076,0.00912,0.00352,0.0127,1.0000,0.6170 -2.750,-0.3875,0.00895,0.00347,0.0143,1.0000,0.6580 -2.500,-0.3676,0.00883,0.00346,0.0160,1.0000,0.6967 -2.250,-0.3480,0.00876,0.00349,0.0177,1.0000,0.7344 -2.000,-0.3291,0.00871,0.00355,0.0197,1.0000,0.7692 -1.750,-0.3108,0.00871,0.00361,0.0217,1.0000,0.8034 -1.500,-0.2915,0.00875,0.00373,0.0235,0.9995,0.8362 -1.250,-0.2494,0.00888,0.00391,0.0208,0.9911,0.8690 -1.000,-0.2055,0.00902,0.00405,0.0179,0.9833,0.8971 -0.750,-0.1599,0.00914,0.00416,0.0146,0.9755,0.9188 -0.500,-0.1076,0.00927,0.00427,0.0100,0.9697,0.9355 -0.250,-0.0555,0.00935,0.00434,0.0053,0.9628,0.9479 0.000,0.0000,0.00938,0.00436,0.0000,0.9568,0.9568 0.250,0.0555,0.00935,0.00434,-0.0053,0.9479,0.9629 0.500,0.1077,0.00927,0.00427,-0.0100,0.9356,0.9698 0.750,0.1599,0.00914,0.00416,-0.0146,0.9190,0.9756 1.000,0.2055,0.00902,0.00404,-0.0179,0.8970,0.9833 1.250,0.2494,0.00888,0.00390,-0.0208,0.8692,0.9912 1.500,0.2915,0.00874,0.00373,-0.0235,0.8365,0.9996 1.750,0.3106,0.00871,0.00361,-0.0216,0.8035,1.0000 2.000,0.3288,0.00871,0.00355,-0.0196,0.7692,1.0000 2.250,0.3477,0.00875,0.00348,-0.0177,0.7344,1.0000 2.500,0.3673,0.00883,0.00346,-0.0159,0.6969,1.0000 2.750,0.3872,0.00895,0.00347,-0.0142,0.6582,1.0000 3.000,0.4073,0.00912,0.00351,-0.0126,0.6172,1.0000 3.250,0.4276,0.00933,0.00359,-0.0110,0.5734,1.0000 3.500,0.4480,0.00960,0.00373,-0.0095,0.5282,1.0000 3.750,0.4686,0.00989,0.00389,-0.0081,0.4796,1.0000 4.000,0.4889,0.01025,0.00407,-0.0067,0.4262,1.0000 4.250,0.5089,0.01070,0.00429,-0.0053,0.3643,1.0000 4.500,0.5293,0.01120,0.00457,-0.0040,0.3035,1.0000 4.750,0.5494,0.01181,0.00492,-0.0028,0.2399,1.0000 5.000,0.5689,0.01257,0.00540,-0.0016,0.1704,1.0000 5.250,0.5870,0.01369,0.00613,-0.0002,0.0985,1.0000 5.500,0.6049,0.01497,0.00718,0.0014,0.0621,1.0000 5.750,0.6242,0.01607,0.00828,0.0030,0.0486,1.0000 6.000,0.6426,0.01744,0.00962,0.0045,0.0398,1.0000 6.250,0.6642,0.01852,0.01083,0.0059,0.0356,1.0000 6.500,0.6854,0.01988,0.01225,0.0072,0.0323,1.0000 6.750,0.7043,0.02275,0.01520,0.0085,0.0291,1.0000 7.000,0.7270,0.02374,0.01650,0.0096,0.0267,1.0000 7.250,0.7480,0.02593,0.01900,0.0110,0.0255,1.0000 7.500,0.7667,0.02870,0.02217,0.0126,0.0249,1.0000 7.750,0.7816,0.03216,0.02612,0.0144,0.0250,1.0000 8.000,0.7918,0.03630,0.03076,0.0164,0.0259,1.0000 8.250,0.7972,0.04083,0.03574,0.0183,0.0268,1.0000 8.500,0.8006,0.04474,0.04006,0.0200,0.0264,1.0000 8.750,0.7982,0.04923,0.04489,0.0215,0.0269,1.0000 9.000,0.7920,0.05336,0.04933,0.0228,0.0267,1.0000 9.250,0.7796,0.05801,0.05415,0.0236,0.0276,1.0000