Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-dga1182-il-200000-n5 Airfoil,dga1182-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,37.4932 Max Cl/Cd alpha,7.25 Url,http://airfoiltools.com/polar/csv?polar=xf-dga1182-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.6137,0.09705,0.09190,0.0044,0.1602,0.0188 -8.250,-0.6116,0.09208,0.08695,-0.0002,0.1602,0.0189 -8.000,-0.6118,0.08676,0.08163,-0.0060,0.1601,0.0189 -7.750,-0.6090,0.08178,0.07657,-0.0103,0.1600,0.0189 -7.500,-0.6045,0.07728,0.07196,-0.0132,0.1600,0.0190 -7.250,-0.5978,0.07293,0.06747,-0.0154,0.1599,0.0191 -7.000,-0.5891,0.06866,0.06305,-0.0169,0.1598,0.0191 -6.750,-0.5782,0.06443,0.05863,-0.0180,0.1597,0.0192 -6.500,-0.5656,0.06027,0.05426,-0.0188,0.1596,0.0192 -6.250,-0.5515,0.05623,0.04997,-0.0192,0.1596,0.0193 -5.750,-0.5317,0.04538,0.03880,-0.0203,0.1595,0.0155 -5.500,-0.5118,0.04079,0.03384,-0.0199,0.1594,0.0135 -5.250,-0.4901,0.03772,0.03042,-0.0196,0.1594,0.0148 -5.000,-0.4671,0.03447,0.02678,-0.0189,0.1593,0.0152 -4.750,-0.4431,0.03091,0.02277,-0.0180,0.1593,0.0138 -4.500,-0.4176,0.02768,0.01904,-0.0170,0.1593,0.0127 -4.250,-0.3912,0.02511,0.01600,-0.0160,0.1593,0.0121 -4.000,-0.3648,0.02313,0.01368,-0.0153,0.1594,0.0119 -3.750,-0.3384,0.02148,0.01177,-0.0147,0.1595,0.0121 -3.500,-0.3122,0.02010,0.01018,-0.0142,0.1597,0.0125 -3.250,-0.2861,0.01915,0.00910,-0.0138,0.1599,0.0142 -3.000,-0.2601,0.01822,0.00805,-0.0133,0.1601,0.0160 -2.750,-0.2343,0.01727,0.00700,-0.0127,0.1603,0.0168 -2.500,-0.2083,0.01654,0.00613,-0.0123,0.1605,0.0179 -2.250,-0.1820,0.01595,0.00541,-0.0121,0.1608,0.0206 -2.000,-0.1553,0.01552,0.00485,-0.0119,0.1610,0.0248 -1.750,-0.1280,0.01532,0.00448,-0.0117,0.1605,0.0306 -1.500,-0.1014,0.01469,0.00427,-0.0117,0.1594,0.1797 -1.250,-0.0748,0.01445,0.00437,-0.0118,0.1578,0.3458 -1.000,-0.0468,0.01518,0.00485,-0.0118,0.1560,0.3809 -0.750,-0.0196,0.01538,0.00490,-0.0117,0.1549,0.3853 -0.500,0.0075,0.01550,0.00491,-0.0117,0.1545,0.3881 -0.250,0.0342,0.01580,0.00505,-0.0116,0.1532,0.3908 0.000,0.0613,0.01598,0.00512,-0.0116,0.1516,0.3934 0.250,0.0887,0.01604,0.00511,-0.0115,0.1503,0.3947 0.500,0.1159,0.01616,0.00516,-0.0115,0.1493,0.3957 0.750,0.1430,0.01632,0.00524,-0.0115,0.1483,0.3966 1.000,0.1700,0.01647,0.00536,-0.0114,0.1470,0.3976 1.250,0.1967,0.01664,0.00550,-0.0114,0.1456,0.3989 1.500,0.2232,0.01701,0.00581,-0.0113,0.1436,0.4002 1.750,0.2503,0.01711,0.00595,-0.0113,0.1400,0.4014 2.000,0.2773,0.01725,0.00615,-0.0113,0.1344,0.4022 2.250,0.3044,0.01730,0.00627,-0.0113,0.1298,0.4030 2.500,0.3316,0.01733,0.00639,-0.0112,0.1256,0.4042 2.750,0.3588,0.01738,0.00653,-0.0112,0.1217,0.4054 3.000,0.3863,0.01725,0.00657,-0.0112,0.1158,0.4062 3.250,0.4138,0.01718,0.00670,-0.0110,0.1016,0.4069 3.500,0.4412,0.01712,0.00675,-0.0110,0.0923,0.4078 3.750,0.4696,0.01681,0.00649,-0.0112,0.0865,0.4089 4.000,0.4985,0.01651,0.00619,-0.0113,0.0795,0.4100 4.250,0.5247,0.01682,0.00657,-0.0111,0.0718,0.4108 4.500,0.5509,0.01713,0.00695,-0.0110,0.0655,0.4117 4.750,0.5768,0.01749,0.00746,-0.0107,0.0611,0.4128 5.000,0.6026,0.01788,0.00798,-0.0105,0.0580,0.4143 5.250,0.6283,0.01828,0.00848,-0.0103,0.0551,0.4160 5.500,0.6536,0.01878,0.00914,-0.0100,0.0527,0.4177 5.750,0.6789,0.01934,0.00987,-0.0097,0.0513,0.4190 6.000,0.7040,0.01998,0.01069,-0.0093,0.0497,0.4200 6.250,0.7292,0.02060,0.01149,-0.0090,0.0476,0.4207 6.500,0.7547,0.02077,0.01173,-0.0089,0.0428,0.4214 6.750,0.7800,0.02114,0.01226,-0.0088,0.0371,0.4222 7.000,0.8044,0.02164,0.01287,-0.0086,0.0311,0.4230 7.250,0.8301,0.02214,0.01362,-0.0084,0.0235,0.4239 7.500,0.8543,0.02301,0.01459,-0.0080,0.0172,0.4248 7.750,0.8782,0.02397,0.01564,-0.0077,0.0130,0.4258 8.000,0.8981,0.02611,0.01811,-0.0067,0.0108,0.4269 8.250,0.9184,0.02833,0.02077,-0.0058,0.0100,0.4280 8.500,0.9368,0.03107,0.02398,-0.0049,0.0093,0.4292 8.750,0.9551,0.03352,0.02681,-0.0041,0.0083,0.4306 9.000,0.9732,0.03543,0.02897,-0.0036,0.0075,0.4321 9.250,0.9832,0.03932,0.03334,-0.0025,0.0070,0.4333 9.500,0.9829,0.04519,0.03982,-0.0011,0.0069,0.4341 10.000,0.9577,0.05897,0.05454,0.0004,0.0069,0.4346 10.250,0.9337,0.06566,0.06149,0.0001,0.0070,0.4345