Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e184-il-200000-n5 Airfoil,e184-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,53.5398 Max Cl/Cd alpha,4.5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-e184-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.6718,0.08829,0.08532,0.0204,1.0000,0.0158 -8.750,-0.6814,0.08151,0.07860,0.0154,1.0000,0.0155 -8.500,-0.7068,0.06989,0.06700,0.0058,1.0000,0.0145 -8.250,-0.7153,0.06110,0.05804,0.0015,1.0000,0.0141 -8.000,-0.7192,0.05442,0.05111,-0.0003,1.0000,0.0140 -7.750,-0.7189,0.04866,0.04502,-0.0010,1.0000,0.0140 -7.500,-0.7167,0.04319,0.03918,-0.0012,1.0000,0.0144 -7.250,-0.7042,0.04015,0.03591,-0.0013,1.0000,0.0152 -7.000,-0.6867,0.03804,0.03362,-0.0014,1.0000,0.0162 -6.750,-0.6700,0.03381,0.02889,-0.0012,0.9551,0.0165 -6.500,-0.6540,0.02986,0.02431,0.0002,0.9151,0.0163 -6.250,-0.6375,0.02706,0.02098,0.0020,0.8913,0.0164 -6.000,-0.6184,0.02484,0.01832,0.0037,0.8734,0.0166 -5.750,-0.5972,0.02296,0.01606,0.0050,0.8583,0.0169 -5.500,-0.5746,0.02137,0.01414,0.0062,0.8450,0.0174 -5.250,-0.5514,0.02001,0.01244,0.0073,0.8329,0.0179 -5.000,-0.5273,0.01881,0.01102,0.0081,0.8217,0.0184 -4.750,-0.5026,0.01795,0.00998,0.0089,0.8112,0.0197 -4.500,-0.4777,0.01719,0.00906,0.0096,0.8016,0.0209 -4.250,-0.4534,0.01632,0.00804,0.0104,0.7927,0.0212 -4.000,-0.4286,0.01554,0.00712,0.0111,0.7836,0.0215 -3.750,-0.4039,0.01482,0.00627,0.0118,0.7756,0.0220 -3.500,-0.3787,0.01418,0.00549,0.0124,0.7675,0.0232 -3.250,-0.3528,0.01370,0.00486,0.0129,0.7599,0.0254 -3.000,-0.3267,0.01331,0.00437,0.0134,0.7525,0.0297 -2.750,-0.3008,0.01281,0.00393,0.0138,0.7453,0.0516 -2.500,-0.2758,0.01224,0.00358,0.0143,0.7385,0.1118 -2.250,-0.2512,0.01161,0.00332,0.0146,0.7316,0.2023 -2.000,-0.2280,0.01088,0.00308,0.0152,0.7251,0.3313 -1.750,-0.2087,0.00989,0.00292,0.0166,0.7187,0.5293 -1.500,-0.1893,0.00911,0.00282,0.0188,0.7125,0.7004 -1.250,-0.1474,0.00872,0.00288,0.0168,0.7068,0.8620 -1.000,-0.0871,0.00880,0.00289,0.0105,0.7003,0.9305 -0.750,-0.0450,0.00892,0.00287,0.0078,0.6948,0.9589 -0.500,-0.0060,0.00899,0.00285,0.0056,0.6880,0.9784 -0.250,0.0365,0.00903,0.00277,0.0025,0.6823,0.9919 0.000,0.0774,0.00902,0.00268,-0.0004,0.6757,1.0000 0.250,0.1028,0.00902,0.00260,0.0001,0.6697,1.0000 0.500,0.1285,0.00904,0.00257,0.0004,0.6635,1.0000 0.750,0.1542,0.00906,0.00254,0.0008,0.6571,1.0000 1.000,0.1800,0.00910,0.00253,0.0012,0.6510,1.0000 1.250,0.2060,0.00913,0.00255,0.0016,0.6439,1.0000 1.500,0.2319,0.00917,0.00256,0.0020,0.6365,1.0000 1.750,0.2578,0.00921,0.00257,0.0024,0.6279,1.0000 2.000,0.2839,0.00924,0.00262,0.0027,0.6183,1.0000 2.250,0.3099,0.00929,0.00267,0.0032,0.6082,1.0000 2.500,0.3358,0.00934,0.00270,0.0036,0.5977,1.0000 2.750,0.3620,0.00938,0.00277,0.0040,0.5861,1.0000 3.000,0.3881,0.00944,0.00284,0.0044,0.5728,1.0000 3.250,0.4143,0.00950,0.00292,0.0048,0.5585,1.0000 3.500,0.4404,0.00958,0.00304,0.0052,0.5430,1.0000 3.750,0.4667,0.00966,0.00316,0.0055,0.5234,1.0000 4.000,0.4927,0.00977,0.00328,0.0059,0.5002,1.0000 4.250,0.5187,0.00992,0.00342,0.0063,0.4688,1.0000 4.500,0.5445,0.01017,0.00358,0.0067,0.4235,1.0000 4.750,0.5684,0.01104,0.00390,0.0067,0.2979,1.0000 5.000,0.5921,0.01214,0.00448,0.0065,0.1916,1.0000 5.250,0.6160,0.01303,0.00506,0.0064,0.1237,1.0000 5.500,0.6391,0.01404,0.00573,0.0065,0.0617,1.0000 5.750,0.6617,0.01515,0.00656,0.0068,0.0205,1.0000 6.000,0.6850,0.01599,0.00743,0.0073,0.0148,1.0000 6.250,0.7083,0.01673,0.00837,0.0078,0.0132,1.0000 6.500,0.7310,0.01757,0.00937,0.0085,0.0122,1.0000 6.750,0.7527,0.01852,0.01045,0.0091,0.0115,1.0000 7.000,0.7732,0.01962,0.01167,0.0100,0.0109,1.0000 7.250,0.7928,0.02081,0.01296,0.0109,0.0103,1.0000 7.500,0.8084,0.02277,0.01503,0.0121,0.0091,1.0000 7.750,0.8282,0.02391,0.01630,0.0130,0.0088,1.0000 8.000,0.8472,0.02526,0.01783,0.0141,0.0084,1.0000 8.250,0.8650,0.02702,0.01985,0.0153,0.0082,1.0000 8.500,0.8817,0.02899,0.02207,0.0165,0.0079,1.0000 8.750,0.8967,0.03125,0.02463,0.0178,0.0078,1.0000 9.000,0.9092,0.03377,0.02747,0.0191,0.0077,1.0000 9.250,0.9181,0.03656,0.03062,0.0204,0.0077,1.0000 9.500,0.9223,0.03966,0.03409,0.0219,0.0076,1.0000 9.750,0.9212,0.04295,0.03773,0.0234,0.0076,1.0000 10.000,0.9142,0.04614,0.04120,0.0249,0.0077,1.0000 10.250,0.9008,0.04935,0.04464,0.0262,0.0077,1.0000 10.500,0.8878,0.05299,0.04848,0.0260,0.0077,1.0000 10.750,0.8732,0.05734,0.05302,0.0246,0.0078,1.0000 11.000,0.8586,0.06217,0.05802,0.0222,0.0078,1.0000 11.250,0.8399,0.06838,0.06439,0.0184,0.0079,1.0000 11.500,0.8199,0.07581,0.07197,0.0133,0.0079,1.0000 11.750,0.8011,0.08433,0.08061,0.0072,0.0080,1.0000