Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e378-il-1000000 Airfoil,e378-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,40.9519 Max Cl/Cd alpha,14 Url,http://airfoiltools.com/polar/csv?polar=xf-e378-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -20.000,-0.5429,0.23192,0.23010,0.0619,0.8113,0.0030 -19.750,-0.5313,0.22895,0.22713,0.0578,0.8086,0.0030 -19.500,-0.5235,0.22597,0.22415,0.0556,0.8076,0.0031 -19.250,-0.5230,0.22327,0.22142,0.0569,0.8111,0.0031 -19.000,-0.5122,0.22026,0.21841,0.0533,0.8082,0.0031 -18.750,-0.5042,0.21740,0.21555,0.0510,0.8080,0.0031 -18.500,-0.4999,0.21453,0.21267,0.0506,0.8091,0.0032 -18.250,-0.4890,0.21174,0.20987,0.0470,0.8070,0.0032 -18.000,-0.4798,0.20896,0.20709,0.0442,0.8056,0.0032 -17.750,-0.4799,0.20627,0.20436,0.0460,0.8106,0.0032 -17.500,-0.4682,0.20359,0.20168,0.0420,0.8071,0.0032 -17.250,-0.4602,0.20091,0.19900,0.0399,0.8061,0.0032 -17.000,-0.4560,0.19825,0.19632,0.0396,0.8076,0.0032 -16.750,-0.4472,0.19564,0.19370,0.0372,0.8062,0.0032 -16.500,-0.4398,0.19309,0.19114,0.0353,0.8057,0.0032 -16.250,-0.4318,0.19054,0.18859,0.0331,0.8050,0.0032 -16.000,-0.4221,0.18805,0.18608,0.0301,0.8022,0.0032 -15.750,-0.4216,0.18538,0.18340,0.0318,0.8070,0.0032 -15.500,-0.4088,0.18315,0.18115,0.0272,0.8012,0.0032 -15.250,-0.4056,0.18060,0.17860,0.0273,0.8042,0.0032 -15.000,-0.3931,0.17862,0.17658,0.0226,0.7979,0.0032 -14.750,-0.3921,0.17628,0.17424,0.0236,0.8016,0.0032 -14.500,-0.3791,0.17470,0.17265,0.0182,0.7963,0.0032 -14.250,-0.3815,0.17176,0.16969,0.0214,0.8028,0.0033 -14.000,-0.3670,0.16945,0.16737,0.0159,0.7961,0.0033 -13.750,-0.3628,0.16651,0.16440,0.0161,0.7970,0.0033 -13.500,-0.3528,0.16367,0.16158,0.0132,0.7953,0.0033 -13.250,-0.3448,0.16079,0.15869,0.0114,0.7936,0.0033 -13.000,-0.3385,0.15776,0.15565,0.0104,0.7936,0.0033 -11.250,-0.3544,0.14117,0.13879,-0.0013,0.7913,0.0034 -11.000,-0.3429,0.13883,0.13643,-0.0047,0.7851,0.0036 -10.750,-0.3337,0.13625,0.13385,-0.0064,0.7824,0.0037 -10.500,-0.3244,0.13312,0.13072,-0.0079,0.7819,0.0036 -10.250,-0.3146,0.13023,0.12783,-0.0097,0.7801,0.0042 -10.000,-0.3046,0.12733,0.12494,-0.0117,0.7775,0.0048 -9.750,-0.2973,0.12404,0.12163,-0.0117,0.7776,0.0047 -9.500,-0.2872,0.12108,0.11867,-0.0133,0.7745,0.0052 -9.250,-0.2773,0.11846,0.11603,-0.0152,0.7711,0.0053 -9.000,-0.2404,0.12088,0.11865,-0.0379,0.7390,0.0053 -8.750,-0.2363,0.11705,0.11475,-0.0358,0.7391,0.0054 -8.500,-0.2253,0.11399,0.11172,-0.0385,0.7383,0.0054 -8.250,-0.2213,0.11045,0.10821,-0.0361,0.7379,0.0054 -8.000,-0.2182,0.10698,0.10473,-0.0330,0.7380,0.0054 -7.750,-0.2150,0.10359,0.10135,-0.0298,0.7398,0.0054 -5.750,-0.0862,0.08280,0.08030,-0.0615,0.6021,0.0055 -5.500,-0.0634,0.08018,0.07765,-0.0658,0.5944,0.0055 -5.250,-0.0423,0.07713,0.07455,-0.0686,0.5888,0.0055 -5.000,-0.0239,0.07322,0.07062,-0.0711,0.5831,0.0056 -4.750,-0.0011,0.07068,0.06804,-0.0744,0.5771,0.0058 -4.500,0.0244,0.06820,0.06554,-0.0781,0.5707,0.0059 -4.250,0.0517,0.06575,0.06302,-0.0820,0.5648,0.0062 -4.000,0.0812,0.06350,0.06075,-0.0867,0.5588,0.0065 -3.750,0.1096,0.06074,0.05792,-0.0898,0.5541,0.0068 -3.500,0.1413,0.05837,0.05549,-0.0942,0.5487,0.0075 -3.250,0.1797,0.05635,0.05341,-0.0999,0.5426,0.0081 -3.000,0.2077,0.05571,0.05268,-0.1051,0.5360,0.0082 -2.750,0.2293,0.05453,0.05145,-0.1073,0.5309,0.0082 14.000,1.7036,0.04160,0.03613,-0.0532,0.0015,0.8383 14.250,1.6949,0.04701,0.04160,-0.0557,0.0014,0.8023 14.750,1.6649,0.05707,0.05214,-0.0554,0.0013,0.8363 15.000,1.6492,0.06363,0.05883,-0.0582,0.0013,0.8248 15.250,1.6417,0.06772,0.06306,-0.0577,0.0013,0.8338 15.500,1.6329,0.07269,0.06815,-0.0589,0.0013,0.8330 15.750,1.6192,0.07919,0.07477,-0.0623,0.0013,0.8250 16.000,1.6099,0.08414,0.07985,-0.0631,0.0013,0.8324 16.500,1.5848,0.09662,0.09259,-0.0676,0.0013,0.8299 16.750,1.5746,0.10260,0.09869,-0.0698,0.0013,0.8306 17.000,1.5639,0.10879,0.10501,-0.0721,0.0012,0.8313 17.250,1.5536,0.11501,0.11136,-0.0745,0.0012,0.8313 17.500,1.5426,0.12175,0.11823,-0.0778,0.0012,0.8306 17.750,1.5315,0.12839,0.12500,-0.0807,0.0012,0.8307 18.000,1.5217,0.13483,0.13156,-0.0834,0.0012,0.8306 18.250,1.5118,0.14143,0.13829,-0.0866,0.0012,0.8302 18.500,1.5022,0.14822,0.14520,-0.0904,0.0012,0.8302 18.750,1.4929,0.15522,0.15231,-0.0947,0.0012,0.8296 19.000,1.4839,0.16192,0.15913,-0.0982,0.0012,0.8300 20.000,1.4502,0.19071,0.18836,-0.1168,0.0012,0.8220