Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e694-il-200000-n5 Airfoil,e694-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,59.4305 Max Cl/Cd alpha,7.75 Url,http://airfoiltools.com/polar/csv?polar=xf-e694-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.750,-0.0774,0.10749,0.10325,-0.1372,0.9291,0.0206 -11.500,-0.0712,0.10497,0.10073,-0.1378,0.9272,0.0200 -11.000,-0.0831,0.09045,0.08625,-0.1450,0.9239,0.0167 -10.750,-0.0767,0.08642,0.08220,-0.1480,0.9229,0.0165 -10.500,-0.0718,0.08159,0.07738,-0.1519,0.9220,0.0164 -10.250,-0.0942,0.07985,0.07571,-0.1470,0.9140,0.0162 -10.000,-0.1018,0.07372,0.06962,-0.1505,0.9112,0.0161 -9.500,-0.1590,0.05733,0.05314,-0.1583,0.8993,0.0153 -9.250,-0.1848,0.05169,0.04730,-0.1606,0.8945,0.0151 -9.000,-0.2229,0.05054,0.04611,-0.1532,0.8839,0.0151 -8.750,-0.2419,0.04648,0.04180,-0.1521,0.8791,0.0150 -8.500,-0.2704,0.04509,0.04028,-0.1450,0.8681,0.0148 -8.250,-0.2748,0.04082,0.03560,-0.1442,0.8645,0.0149 -8.000,-0.2911,0.03917,0.03373,-0.1385,0.8554,0.0148 -7.750,-0.2857,0.03622,0.03037,-0.1371,0.8516,0.0149 -7.500,-0.2696,0.03332,0.02702,-0.1371,0.8498,0.0150 -7.250,-0.2476,0.03094,0.02423,-0.1376,0.8487,0.0152 -7.000,-0.2536,0.03051,0.02363,-0.1323,0.8398,0.0153 -6.750,-0.2312,0.02901,0.02177,-0.1322,0.8377,0.0162 -6.500,-0.2053,0.02772,0.02013,-0.1326,0.8363,0.0167 -6.250,-0.1791,0.02631,0.01857,-0.1330,0.8353,0.0171 -6.000,-0.1515,0.02519,0.01734,-0.1336,0.8345,0.0174 -5.750,-0.1459,0.02512,0.01722,-0.1302,0.8285,0.0177 -5.500,-0.1255,0.02455,0.01656,-0.1295,0.8255,0.0180 -5.250,-0.0991,0.02383,0.01577,-0.1298,0.8238,0.0186 -5.000,-0.0708,0.02315,0.01501,-0.1304,0.8226,0.0193 -4.750,-0.0414,0.02252,0.01430,-0.1313,0.8217,0.0201 -4.250,0.0202,0.02140,0.01305,-0.1336,0.8203,0.0232 -4.000,0.0258,0.02190,0.01352,-0.1303,0.8133,0.0248 -3.750,0.0535,0.02161,0.01318,-0.1309,0.8116,0.0276 -3.500,0.0835,0.02126,0.01280,-0.1318,0.8103,0.0327 -3.250,0.1155,0.02079,0.01240,-0.1332,0.8093,0.0513 -3.000,0.1486,0.02029,0.01209,-0.1349,0.8085,0.0987 -2.750,0.1836,0.01962,0.01182,-0.1374,0.8078,0.1916 -2.500,0.2226,0.01870,0.01162,-0.1411,0.8074,0.3747 -2.000,0.2618,0.01881,0.01268,-0.1393,0.7998,0.6169 -1.750,0.2811,0.01898,0.01303,-0.1372,0.7977,0.6777 -1.500,0.3072,0.01910,0.01312,-0.1366,0.7964,0.7157 -1.250,0.3352,0.01916,0.01312,-0.1365,0.7953,0.7374 -1.000,0.3642,0.01920,0.01308,-0.1365,0.7945,0.7571 -0.750,0.3729,0.02006,0.01393,-0.1332,0.7889,0.7720 -0.500,0.3919,0.02041,0.01424,-0.1314,0.7857,0.7851 -0.250,0.4212,0.02045,0.01421,-0.1318,0.7841,0.7950 0.000,0.4471,0.02039,0.01411,-0.1313,0.7828,0.8001 0.250,0.4779,0.02025,0.01391,-0.1318,0.7818,0.8066 0.500,0.5089,0.02007,0.01368,-0.1324,0.7810,0.8128 0.750,0.5384,0.01985,0.01343,-0.1324,0.7802,0.8191 1.750,0.6351,0.02035,0.01386,-0.1308,0.7675,0.8382 2.000,0.6715,0.02005,0.01354,-0.1326,0.7666,0.8416 2.250,0.7055,0.01966,0.01314,-0.1337,0.7658,0.8440 2.500,0.7428,0.01922,0.01269,-0.1355,0.7650,0.8465 3.000,0.7771,0.02003,0.01354,-0.1325,0.7529,0.8537 3.250,0.8161,0.01963,0.01315,-0.1348,0.7517,0.8563 3.500,0.8550,0.01908,0.01262,-0.1367,0.7504,0.8582 4.000,0.8920,0.01950,0.01312,-0.1338,0.7376,0.8647 4.250,0.9342,0.01892,0.01256,-0.1365,0.7355,0.8673 4.500,0.9806,0.01831,0.01198,-0.1400,0.7335,0.8694 4.750,0.9725,0.01937,0.01312,-0.1340,0.7218,0.8731 5.000,1.0112,0.01890,0.01269,-0.1360,0.7189,0.8748 5.500,1.0441,0.01948,0.01341,-0.1326,0.7029,0.8799 5.750,1.0421,0.02055,0.01457,-0.1280,0.6897,0.8831 6.250,1.0610,0.02190,0.01607,-0.1228,0.6659,0.8875 6.500,1.0849,0.02183,0.01607,-0.1223,0.6559,0.8896 6.750,1.1110,0.02164,0.01592,-0.1221,0.6427,0.8916 7.000,1.1405,0.02133,0.01562,-0.1224,0.6269,0.8933 7.250,1.1732,0.02094,0.01522,-0.1232,0.6085,0.8949 7.500,1.2066,0.02059,0.01480,-0.1242,0.5857,0.8963 7.750,1.2314,0.02072,0.01483,-0.1239,0.5577,0.8980 8.000,1.2497,0.02115,0.01514,-0.1226,0.5283,0.8999 8.250,1.2619,0.02181,0.01571,-0.1203,0.4992,0.9022 8.500,1.2692,0.02276,0.01652,-0.1174,0.4673,0.9047 8.750,1.2734,0.02395,0.01756,-0.1142,0.4326,0.9070 9.000,1.2736,0.02544,0.01886,-0.1106,0.3945,0.9093 9.250,1.2740,0.02706,0.02028,-0.1073,0.3556,0.9116 9.500,1.2726,0.02883,0.02185,-0.1039,0.3161,0.9139 9.750,1.2724,0.03058,0.02343,-0.1008,0.2770,0.9161 10.000,1.2744,0.03230,0.02499,-0.0981,0.2467,0.9188 10.250,1.2802,0.03387,0.02647,-0.0961,0.2218,0.9217 10.500,1.2872,0.03545,0.02796,-0.0943,0.1952,0.9246 10.750,1.2922,0.03718,0.02956,-0.0924,0.1657,0.9272 11.000,1.2959,0.03902,0.03125,-0.0903,0.1369,0.9299 11.250,1.3007,0.04087,0.03299,-0.0886,0.1112,0.9328 11.500,1.3052,0.04282,0.03481,-0.0869,0.0861,0.9359 12.000,1.3171,0.04652,0.03840,-0.0839,0.0515,0.9434 12.250,1.3210,0.04860,0.04042,-0.0823,0.0366,0.9485 12.500,1.3252,0.05061,0.04244,-0.0808,0.0274,0.9560 12.750,1.3287,0.05260,0.04447,-0.0793,0.0217,0.9776 13.000,1.3355,0.05474,0.04670,-0.0784,0.0187,1.0000 13.250,1.3428,0.05696,0.04901,-0.0777,0.0170,1.0000 13.500,1.3501,0.05924,0.05139,-0.0771,0.0156,1.0000 13.750,1.3554,0.06176,0.05400,-0.0765,0.0146,1.0000 14.000,1.3608,0.06430,0.05667,-0.0760,0.0138,1.0000 14.250,1.3660,0.06691,0.05942,-0.0755,0.0134,1.0000 14.500,1.3697,0.06974,0.06238,-0.0751,0.0129,1.0000 14.750,1.3728,0.07271,0.06550,-0.0748,0.0125,1.0000 15.000,1.3748,0.07586,0.06878,-0.0747,0.0122,1.0000 15.250,1.3759,0.07918,0.07224,-0.0746,0.0119,1.0000 15.500,1.3759,0.08269,0.07588,-0.0746,0.0117,1.0000 15.750,1.3746,0.08643,0.07973,-0.0748,0.0115,1.0000 16.000,1.3724,0.09036,0.08378,-0.0752,0.0113,1.0000 16.250,1.3708,0.09426,0.08779,-0.0757,0.0111,1.0000 16.500,1.3712,0.09793,0.09161,-0.0763,0.0110,1.0000