Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh78-il-50000-n5 Airfoil,mh78-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,18.4025 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-mh78-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.5402,0.10038,0.09416,0.0159,1.0000,0.0490 -9.750,-0.5454,0.09401,0.08785,0.0119,1.0000,0.0485 -9.500,-0.5569,0.08597,0.07982,0.0058,1.0000,0.0478 -9.250,-0.5802,0.07789,0.07169,-0.0004,1.0000,0.0469 -9.000,-0.6084,0.07132,0.06498,-0.0037,1.0000,0.0460 -8.750,-0.6341,0.06615,0.05960,-0.0039,1.0000,0.0455 -8.500,-0.6451,0.06189,0.05513,-0.0036,1.0000,0.0456 -8.250,-0.6486,0.05809,0.05111,-0.0030,1.0000,0.0458 -8.000,-0.6464,0.05465,0.04743,-0.0023,1.0000,0.0465 -7.750,-0.6410,0.05128,0.04378,-0.0015,1.0000,0.0472 -7.500,-0.6323,0.04801,0.04017,-0.0007,1.0000,0.0480 -7.250,-0.6201,0.04482,0.03658,0.0001,1.0000,0.0489 -7.000,-0.6038,0.04180,0.03310,0.0006,1.0000,0.0498 -6.750,-0.5717,0.03949,0.03061,-0.0010,0.8922,0.0509 -6.500,-0.5497,0.03781,0.02862,0.0002,0.8394,0.0521 -6.250,-0.5313,0.03633,0.02677,0.0023,0.8019,0.0538 -6.000,-0.5115,0.03485,0.02482,0.0044,0.7707,0.0563 -5.750,-0.4917,0.03380,0.02367,0.0062,0.7439,0.0589 -5.500,-0.4685,0.03258,0.02216,0.0076,0.7188,0.0624 -5.250,-0.4449,0.03141,0.02087,0.0090,0.6959,0.0656 -5.000,-0.4204,0.03040,0.01962,0.0103,0.6747,0.0710 -4.750,-0.3965,0.02944,0.01862,0.0114,0.6547,0.0773 -4.250,-0.3469,0.02760,0.01659,0.0134,0.6183,0.0994 -4.000,-0.3229,0.02664,0.01570,0.0144,0.6020,0.1199 -3.750,-0.3001,0.02556,0.01485,0.0155,0.5871,0.1612 -3.500,-0.2786,0.02444,0.01417,0.0164,0.5714,0.2385 -3.250,-0.2597,0.02346,0.01369,0.0180,0.5575,0.3394 -3.000,-0.2440,0.02254,0.01338,0.0206,0.5460,0.4612 -2.750,-0.2139,0.02192,0.01374,0.0226,0.5304,0.6477 -2.500,-0.1567,0.02273,0.01462,0.0214,0.5128,0.7820 -2.250,-0.1226,0.02333,0.01489,0.0222,0.4999,0.8363 -2.000,-0.0839,0.02384,0.01504,0.0218,0.4867,0.8736 -1.750,-0.0383,0.02427,0.01515,0.0196,0.4724,0.9030 -1.500,0.0085,0.02455,0.01508,0.0170,0.4601,0.9283 -1.250,0.0603,0.02467,0.01486,0.0131,0.4474,0.9512 -1.000,0.1137,0.02473,0.01467,0.0085,0.4345,0.9729 -0.750,0.1685,0.02455,0.01412,0.0034,0.4240,0.9919 -0.500,0.2065,0.02452,0.01397,0.0008,0.4132,1.0000 -0.250,0.2276,0.02458,0.01377,0.0017,0.4069,1.0000 0.000,0.2509,0.02482,0.01396,0.0019,0.3987,1.0000 0.250,0.2733,0.02500,0.01399,0.0025,0.3917,1.0000 0.500,0.2951,0.02516,0.01391,0.0034,0.3862,1.0000 0.750,0.3187,0.02556,0.01434,0.0036,0.3781,1.0000 1.000,0.3410,0.02584,0.01448,0.0043,0.3722,1.0000 1.250,0.3628,0.02607,0.01450,0.0052,0.3677,1.0000 1.500,0.3861,0.02669,0.01520,0.0053,0.3603,1.0000 1.750,0.4083,0.02709,0.01552,0.0060,0.3546,1.0000 2.000,0.4300,0.02738,0.01563,0.0070,0.3503,1.0000 2.250,0.4524,0.02811,0.01641,0.0072,0.3444,1.0000 2.500,0.4742,0.02878,0.01709,0.0077,0.3387,1.0000 2.750,0.4957,0.02922,0.01744,0.0086,0.3344,1.0000 3.000,0.5171,0.02954,0.01758,0.0097,0.3309,1.0000 3.250,0.5374,0.03078,0.01903,0.0097,0.3246,1.0000 3.500,0.5575,0.03161,0.01987,0.0103,0.3198,1.0000 3.750,0.5780,0.03217,0.02036,0.0113,0.3161,1.0000 4.000,0.5990,0.03255,0.02059,0.0125,0.3131,1.0000 4.250,0.6148,0.03432,0.02263,0.0125,0.3072,1.0000 4.500,0.6316,0.03552,0.02391,0.0132,0.3026,1.0000 4.750,0.6500,0.03630,0.02466,0.0142,0.2991,1.0000 5.000,0.6697,0.03682,0.02508,0.0155,0.2965,1.0000 5.250,0.6800,0.03891,0.02737,0.0160,0.2919,1.0000 5.500,0.6862,0.04129,0.02994,0.0164,0.2868,1.0000 5.750,0.6981,0.04266,0.03134,0.0175,0.2832,1.0000 6.000,0.7143,0.04347,0.03211,0.0189,0.2805,1.0000 6.250,0.7338,0.04396,0.03251,0.0203,0.2785,1.0000 6.500,0.6723,0.05318,0.04224,0.0191,0.2704,1.0000 6.750,0.6581,0.05690,0.04598,0.0194,0.2661,1.0000 7.000,0.6715,0.05778,0.04681,0.0209,0.2637,1.0000 7.250,0.6928,0.05792,0.04690,0.0226,0.2620,1.0000 7.750,0.5705,0.07772,0.06676,0.0149,0.2484,1.0000 8.000,0.5880,0.07858,0.06758,0.0160,0.2463,1.0000 8.250,0.5651,0.08472,0.07372,0.0135,0.2423,1.0000 8.500,0.5495,0.08994,0.07895,0.0115,0.2387,1.0000 8.750,0.5504,0.09311,0.08212,0.0108,0.2355,1.0000 9.000,0.5606,0.09519,0.08418,0.0108,0.2328,1.0000 9.250,0.5764,0.09663,0.08562,0.0114,0.2307,1.0000 9.500,0.5795,0.09988,0.08886,0.0107,0.2287,1.0000 9.750,0.5616,0.10563,0.09465,0.0079,0.2255,1.0000