Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-eiffel385-il-50000 Airfoil,eiffel385-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,25.2358 Max Cl/Cd alpha,9 Url,http://airfoiltools.com/polar/csv?polar=xf-eiffel385-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.000,-0.2773,0.12290,0.11513,-0.0309,1.0000,0.2376 -12.750,-0.3016,0.12412,0.11649,-0.0314,1.0000,0.2410 -12.500,-0.2861,0.11881,0.11121,-0.0307,1.0000,0.2437 -12.250,-0.2706,0.11497,0.10738,-0.0294,1.0000,0.2496 -12.000,-0.2806,0.11413,0.10664,-0.0288,1.0000,0.2570 -11.750,-0.3128,0.11559,0.10828,-0.0282,1.0000,0.2592 -11.500,-0.2734,0.10840,0.10104,-0.0265,1.0000,0.2670 -11.250,-0.2839,0.10743,0.10017,-0.0252,1.0000,0.2743 -11.000,-0.3220,0.10905,0.10201,-0.0232,1.0000,0.2770 -10.750,-0.2871,0.10268,0.09558,-0.0218,1.0000,0.2838 -10.500,-0.3032,0.10219,0.09522,-0.0194,1.0000,0.2923 -10.250,-0.3442,0.10363,0.09688,-0.0160,1.0000,0.2946 -10.000,-0.3112,0.09821,0.09142,-0.0145,1.0000,0.3067 -9.750,-0.3485,0.09921,0.09261,-0.0106,1.0000,0.3113 -9.500,-0.3431,0.09602,0.08949,-0.0084,1.0000,0.3176 -9.250,-0.3577,0.09527,0.08884,-0.0048,1.0000,0.3257 -9.000,-0.4013,0.09642,0.09019,-0.0002,1.0000,0.3290 -8.750,-0.3994,0.09356,0.08738,0.0024,1.0000,0.3356 -8.500,-0.4183,0.09298,0.08690,0.0053,1.0000,0.3451 -8.250,-0.4379,0.09150,0.08552,0.0071,1.0000,0.3509 -8.000,-0.4469,0.09022,0.08429,0.0094,1.0000,0.3641 -7.500,-0.4612,0.08585,0.08001,0.0130,1.0000,0.3863 -7.250,-0.4709,0.08416,0.07835,0.0136,1.0000,0.4018 -7.000,-0.4728,0.08191,0.07613,0.0159,1.0000,0.4192 -6.750,-0.4651,0.07928,0.07350,0.0189,0.9985,0.4392 -6.500,-0.4440,0.07666,0.07083,0.0182,0.9905,0.4740 -6.250,-0.3612,0.06151,0.05454,-0.0294,0.9815,0.3299 -6.000,-0.3295,0.05820,0.05104,-0.0339,0.9734,0.3274 -5.750,-0.2892,0.05496,0.04747,-0.0409,0.9650,0.3269 -5.500,-0.2479,0.05220,0.04430,-0.0476,0.9567,0.3284 -5.250,-0.2112,0.04989,0.04155,-0.0530,0.9484,0.3307 -5.000,-0.1760,0.04892,0.04056,-0.0553,0.9399,0.3366 -4.750,-0.1498,0.04781,0.03920,-0.0571,0.9311,0.3428 -4.500,-0.1047,0.04654,0.03750,-0.0623,0.9225,0.3496 -4.250,-0.0834,0.04591,0.03684,-0.0624,0.9130,0.3555 -4.000,-0.0448,0.04535,0.03594,-0.0657,0.9042,0.3674 -3.750,-0.0207,0.04499,0.03555,-0.0660,0.8945,0.3771 -3.500,0.0124,0.04463,0.03499,-0.0680,0.8850,0.3879 -3.250,0.0448,0.04444,0.03460,-0.0697,0.8749,0.4021 -3.000,0.0701,0.04442,0.03450,-0.0702,0.8647,0.4155 -2.750,0.1124,0.04434,0.03433,-0.0729,0.8546,0.4321 -2.500,0.1272,0.04445,0.03443,-0.0718,0.8435,0.4434 -2.250,0.1608,0.04457,0.03450,-0.0731,0.8328,0.4603 -2.000,0.1912,0.04475,0.03466,-0.0741,0.8217,0.4776 -1.750,0.2155,0.04514,0.03498,-0.0744,0.8099,0.4924 -1.500,0.2589,0.04536,0.03514,-0.0772,0.7992,0.5109 -1.250,0.2859,0.04582,0.03555,-0.0779,0.7872,0.5257 -1.000,0.3120,0.04636,0.03611,-0.0785,0.7751,0.5407 -0.750,0.3590,0.04648,0.03633,-0.0815,0.7646,0.5662 -0.500,0.3836,0.04699,0.03699,-0.0819,0.7519,0.5922 -0.250,0.4067,0.04757,0.03784,-0.0821,0.7396,0.6296 0.000,0.4583,0.04671,0.03793,-0.0857,0.7286,1.0000 0.250,0.4895,0.04782,0.03861,-0.0874,0.7161,1.0000 0.500,0.5025,0.04935,0.03995,-0.0866,0.7033,1.0000 0.750,0.5346,0.05028,0.04069,-0.0874,0.6924,1.0000 1.000,0.5596,0.05136,0.04165,-0.0874,0.6808,1.0000 1.250,0.5646,0.05333,0.04356,-0.0859,0.6685,1.0000 1.500,0.6114,0.05360,0.04374,-0.0876,0.6595,1.0000 1.750,0.6059,0.05612,0.04623,-0.0854,0.6470,1.0000 2.000,0.6176,0.05805,0.04812,-0.0847,0.6367,1.0000 2.250,0.6448,0.05918,0.04921,-0.0848,0.6269,1.0000 2.500,0.6402,0.06203,0.05205,-0.0833,0.6168,1.0000 2.750,0.6720,0.06306,0.05308,-0.0837,0.6082,1.0000 3.000,0.6611,0.06641,0.05642,-0.0822,0.5992,1.0000 3.250,0.6875,0.06776,0.05777,-0.0823,0.5906,1.0000 3.500,0.6842,0.07096,0.06098,-0.0814,0.5837,1.0000 3.750,0.6816,0.07409,0.06414,-0.0808,0.5773,1.0000 4.000,0.7193,0.07508,0.06515,-0.0813,0.5690,1.0000 4.250,0.6977,0.07946,0.06955,-0.0803,0.5650,1.0000 4.500,0.6930,0.08308,0.07320,-0.0801,0.5627,1.0000 4.750,0.6930,0.08647,0.07662,-0.0801,0.5605,1.0000 5.000,0.6896,0.09035,0.08054,-0.0804,0.5624,1.0000 5.250,0.6967,0.09432,0.08457,-0.0814,0.5676,1.0000 9.000,1.3486,0.05344,0.04510,-0.0521,0.2833,1.0000 9.250,1.2400,0.06743,0.05950,-0.0497,0.2943,1.0000 9.500,0.9948,0.11236,0.10410,-0.0639,0.2973,1.0000 9.750,0.9839,0.11703,0.10880,-0.0642,0.2791,1.0000 10.000,0.9813,0.12067,0.11248,-0.0642,0.2617,1.0000 10.250,0.9893,0.12274,0.11462,-0.0635,0.2466,1.0000 10.500,1.3197,0.06967,0.06126,-0.0409,0.1985,1.0000 10.750,1.2815,0.07706,0.06892,-0.0411,0.1962,1.0000 11.000,1.3088,0.07730,0.06906,-0.0399,0.1859,1.0000 11.250,1.2542,0.08752,0.07956,-0.0417,0.1866,1.0000 11.500,0.9347,0.15670,0.14856,-0.0749,0.2142,1.0000