Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rae104-il-500000-n5 Airfoil,rae104-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,49.7009 Max Cl/Cd alpha,6.75 Url,http://airfoiltools.com/polar/csv?polar=xf-rae104-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.250,-0.8703,0.05332,0.05063,-0.0429,1.0000,0.0056 -12.000,-0.8855,0.04915,0.04629,-0.0435,1.0000,0.0058 -11.750,-0.9215,0.04317,0.03999,-0.0423,1.0000,0.0057 -11.500,-0.9329,0.04036,0.03697,-0.0401,1.0000,0.0058 -11.250,-0.9558,0.03651,0.03280,-0.0360,1.0000,0.0057 -11.000,-0.9625,0.03443,0.03051,-0.0322,1.0000,0.0059 -10.750,-0.9696,0.03204,0.02783,-0.0280,1.0000,0.0059 -10.500,-0.9671,0.03003,0.02557,-0.0250,1.0000,0.0061 -10.250,-0.9617,0.02808,0.02336,-0.0222,1.0000,0.0063 -10.000,-0.9534,0.02632,0.02132,-0.0197,1.0000,0.0064 -9.750,-0.9424,0.02481,0.01959,-0.0174,1.0000,0.0066 -9.500,-0.9296,0.02347,0.01805,-0.0152,1.0000,0.0068 -9.250,-0.9145,0.02247,0.01688,-0.0134,1.0000,0.0071 -9.000,-0.8993,0.02144,0.01568,-0.0115,1.0000,0.0072 -8.750,-0.8866,0.02007,0.01416,-0.0092,1.0000,0.0076 -8.500,-0.8709,0.01925,0.01326,-0.0073,1.0000,0.0080 -8.250,-0.8545,0.01856,0.01250,-0.0055,1.0000,0.0083 -8.000,-0.8384,0.01789,0.01174,-0.0036,1.0000,0.0087 -7.750,-0.8121,0.01707,0.01082,-0.0038,0.9973,0.0091 -7.500,-0.7840,0.01627,0.00993,-0.0044,0.9920,0.0097 -7.250,-0.7554,0.01554,0.00910,-0.0051,0.9866,0.0103 -7.000,-0.7255,0.01492,0.00838,-0.0060,0.9818,0.0108 -6.750,-0.6979,0.01404,0.00743,-0.0065,0.9753,0.0117 -6.500,-0.6657,0.01353,0.00687,-0.0079,0.9705,0.0131 -6.250,-0.6352,0.01310,0.00640,-0.0088,0.9632,0.0146 -6.000,-0.6027,0.01266,0.00589,-0.0102,0.9568,0.0158 -5.750,-0.5732,0.01206,0.00525,-0.0109,0.9481,0.0181 -5.500,-0.5418,0.01167,0.00481,-0.0120,0.9400,0.0209 -5.250,-0.5124,0.01133,0.00442,-0.0126,0.9300,0.0239 -5.000,-0.4850,0.01097,0.00405,-0.0127,0.9194,0.0295 -4.750,-0.4582,0.01069,0.00373,-0.0126,0.9091,0.0354 -4.250,-0.4081,0.01011,0.00317,-0.0118,0.8885,0.0612 -4.000,-0.3840,0.00981,0.00292,-0.0112,0.8791,0.0849 -3.500,-0.3381,0.00905,0.00245,-0.0097,0.8622,0.1745 -3.250,-0.3169,0.00853,0.00220,-0.0087,0.8550,0.2531 -3.000,-0.2964,0.00799,0.00198,-0.0076,0.8476,0.3423 -2.750,-0.2776,0.00735,0.00174,-0.0061,0.8412,0.4548 -2.500,-0.2603,0.00673,0.00158,-0.0041,0.8345,0.5725 -2.250,-0.2385,0.00649,0.00156,-0.0028,0.8287,0.6495 -2.000,-0.2134,0.00642,0.00154,-0.0022,0.8233,0.6831 -1.750,-0.1875,0.00638,0.00153,-0.0017,0.8182,0.7047 -1.500,-0.1612,0.00636,0.00151,-0.0014,0.8138,0.7223 -1.250,-0.1347,0.00634,0.00150,-0.0011,0.8087,0.7364 -1.000,-0.1080,0.00633,0.00149,-0.0008,0.8038,0.7482 -0.750,-0.0811,0.00633,0.00148,-0.0006,0.7994,0.7586 -0.500,-0.0541,0.00632,0.00148,-0.0004,0.7942,0.7679 -0.250,-0.0271,0.00631,0.00148,-0.0002,0.7886,0.7756 0.000,0.0000,0.00632,0.00147,0.0000,0.7829,0.7829 0.250,0.0271,0.00631,0.00148,0.0002,0.7756,0.7886 0.500,0.0541,0.00632,0.00148,0.0004,0.7679,0.7942 0.750,0.0811,0.00633,0.00148,0.0006,0.7585,0.7994 1.000,0.1080,0.00633,0.00149,0.0008,0.7482,0.8038 1.250,0.1347,0.00634,0.00150,0.0011,0.7364,0.8088 1.500,0.1612,0.00636,0.00151,0.0014,0.7221,0.8138 1.750,0.1875,0.00638,0.00153,0.0017,0.7046,0.8182 2.000,0.2134,0.00642,0.00154,0.0022,0.6834,0.8233 2.250,0.2385,0.00649,0.00156,0.0028,0.6486,0.8287 2.500,0.2603,0.00672,0.00158,0.0041,0.5731,0.8345 2.750,0.2777,0.00734,0.00174,0.0061,0.4550,0.8412 3.000,0.2964,0.00798,0.00198,0.0076,0.3429,0.8476 3.250,0.3168,0.00854,0.00220,0.0087,0.2518,0.8550 3.500,0.3381,0.00905,0.00245,0.0097,0.1746,0.8622 3.750,0.3607,0.00945,0.00268,0.0105,0.1230,0.8705 4.000,0.3840,0.00981,0.00292,0.0112,0.0844,0.8791 4.250,0.4081,0.01011,0.00317,0.0118,0.0613,0.8886 4.750,0.4582,0.01069,0.00373,0.0126,0.0355,0.9092 5.000,0.4850,0.01097,0.00405,0.0127,0.0295,0.9194 5.250,0.5125,0.01132,0.00441,0.0125,0.0243,0.9300 5.500,0.5418,0.01167,0.00481,0.0120,0.0210,0.9401 5.750,0.5732,0.01205,0.00524,0.0109,0.0182,0.9481 6.000,0.6026,0.01266,0.00589,0.0102,0.0158,0.9569 6.250,0.6351,0.01309,0.00639,0.0089,0.0146,0.9632 6.500,0.6656,0.01353,0.00687,0.0079,0.0131,0.9705 6.750,0.6978,0.01404,0.00742,0.0065,0.0117,0.9753 7.000,0.7255,0.01491,0.00836,0.0060,0.0108,0.9818 7.250,0.7554,0.01553,0.00908,0.0051,0.0103,0.9866 7.500,0.7839,0.01627,0.00992,0.0045,0.0097,0.9920 7.750,0.8121,0.01704,0.01079,0.0038,0.0091,0.9972 8.000,0.8386,0.01787,0.01174,0.0035,0.0087,1.0000 8.250,0.8549,0.01851,0.01245,0.0054,0.0082,1.0000 8.500,0.8708,0.01927,0.01329,0.0073,0.0080,1.0000 8.750,0.8862,0.02014,0.01424,0.0093,0.0077,1.0000 9.000,0.8986,0.02157,0.01583,0.0116,0.0072,1.0000 9.250,0.9140,0.02256,0.01698,0.0134,0.0071,1.0000 9.500,0.9293,0.02353,0.01811,0.0153,0.0069,1.0000 9.750,0.9418,0.02492,0.01972,0.0175,0.0067,1.0000 10.000,0.9532,0.02636,0.02137,0.0197,0.0065,1.0000 10.250,0.9602,0.02831,0.02362,0.0224,0.0064,1.0000 10.500,0.9666,0.03010,0.02565,0.0250,0.0061,1.0000 10.750,0.9680,0.03226,0.02808,0.0282,0.0060,1.0000 11.000,0.9602,0.03470,0.03079,0.0325,0.0059,1.0000 11.250,0.9515,0.03698,0.03332,0.0364,0.0058,1.0000 11.500,0.9409,0.03955,0.03611,0.0396,0.0057,1.0000 11.750,0.9247,0.04287,0.03967,0.0421,0.0056,1.0000 12.000,0.8969,0.04784,0.04492,0.0435,0.0056,1.0000 12.250,0.8783,0.05233,0.04960,0.0430,0.0056,1.0000