Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca2424-il-50000-n5 Airfoil,naca2424-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,15.5906 Max Cl/Cd alpha,5.75 Url,http://www.airfoiltools.com/polar/csv?polar=xf-naca2424-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.000,-0.4088,0.12127,0.11196,-0.0470,1.0000,0.1800 -12.750,-0.4096,0.11923,0.10996,-0.0460,1.0000,0.1832 -12.500,-0.4709,0.10762,0.09833,-0.0494,1.0000,0.1909 -12.250,-0.4576,0.10811,0.09888,-0.0471,1.0000,0.1927 -11.750,-0.5468,0.09134,0.08208,-0.0497,1.0000,0.2062 -11.500,-0.5349,0.09199,0.08281,-0.0472,1.0000,0.2084 -11.250,-0.7998,0.06275,0.05294,-0.0493,1.0000,0.2193 -11.000,-0.8248,0.06046,0.05062,-0.0456,1.0000,0.2219 -10.750,-0.8184,0.06026,0.05052,-0.0431,1.0000,0.2250 -10.500,-0.8138,0.05795,0.04810,-0.0442,0.9932,0.2301 -10.250,-0.8447,0.05398,0.04375,-0.0423,0.9828,0.2351 -10.000,-0.8176,0.05334,0.04315,-0.0436,0.9764,0.2401 -9.750,-0.7994,0.05250,0.04231,-0.0438,0.9681,0.2453 -9.500,-0.8094,0.05061,0.04018,-0.0410,0.9580,0.2506 -9.250,-0.7969,0.04951,0.03899,-0.0404,0.9499,0.2561 -9.000,-0.7774,0.04906,0.03860,-0.0398,0.9407,0.2613 -8.750,-0.7697,0.04789,0.03725,-0.0384,0.9327,0.2677 -8.500,-0.7732,0.04674,0.03596,-0.0346,0.9209,0.2729 -8.250,-0.7348,0.04647,0.03580,-0.0368,0.9152,0.2797 -8.000,-0.7356,0.04561,0.03482,-0.0330,0.9035,0.2855 -7.750,-0.7165,0.04467,0.03376,-0.0326,0.8962,0.2927 -7.500,-0.7001,0.04437,0.03353,-0.0309,0.8861,0.2985 -7.250,-0.6865,0.04355,0.03258,-0.0293,0.8773,0.3062 -7.000,-0.6627,0.04289,0.03189,-0.0292,0.8703,0.3136 -6.750,-0.6519,0.04259,0.03163,-0.0266,0.8589,0.3199 -6.500,-0.6332,0.04169,0.03053,-0.0256,0.8520,0.3291 -6.250,-0.6206,0.04146,0.03039,-0.0232,0.8414,0.3353 -6.000,-0.5983,0.04103,0.02995,-0.0225,0.8331,0.3436 -5.750,-0.5705,0.04021,0.02901,-0.0227,0.8277,0.3536 -5.500,-0.5662,0.04020,0.02909,-0.0189,0.8149,0.3596 -5.250,-0.5422,0.03959,0.02838,-0.0183,0.8082,0.3698 -5.000,-0.5276,0.03931,0.02811,-0.0162,0.7988,0.3777 -4.750,-0.5088,0.03905,0.02789,-0.0147,0.7896,0.3867 -4.250,-0.4736,0.03848,0.02731,-0.0113,0.7725,0.4053 -4.000,-0.4532,0.03796,0.02668,-0.0100,0.7652,0.4169 -3.750,-0.4120,0.03746,0.02629,-0.0118,0.7612,0.4285 -3.500,-0.4192,0.03769,0.02647,-0.0063,0.7475,0.4369 -3.250,-0.3871,0.03725,0.02608,-0.0066,0.7418,0.4486 -3.000,-0.3524,0.03657,0.02533,-0.0073,0.7380,0.4632 -2.750,-0.3588,0.03713,0.02598,-0.0020,0.7236,0.4706 -2.500,-0.3285,0.03665,0.02549,-0.0020,0.7185,0.4850 -2.250,-0.3075,0.03662,0.02552,-0.0007,0.7107,0.4967 -2.000,-0.3014,0.03675,0.02563,0.0028,0.7000,0.5089 -1.750,-0.2645,0.03636,0.02532,0.0019,0.6954,0.5238 -1.500,-0.2570,0.03650,0.02543,0.0051,0.6862,0.5374 -1.250,-0.2392,0.03667,0.02569,0.0069,0.6770,0.5506 -1.000,-0.2041,0.03626,0.02530,0.0063,0.6724,0.5675 -0.750,-0.1928,0.03643,0.02547,0.0090,0.6640,0.5831 -0.500,-0.1790,0.03681,0.02596,0.0112,0.6542,0.5973 -0.250,-0.1428,0.03639,0.02556,0.0105,0.6495,0.6161 0.000,-0.1007,0.03582,0.02499,0.0091,0.6463,0.6369 0.250,-0.1159,0.03718,0.02647,0.0149,0.6316,0.6491 0.500,-0.0770,0.03683,0.02616,0.0139,0.6270,0.6692 0.750,-0.0288,0.03627,0.02562,0.0117,0.6238,0.6909 1.000,-0.0469,0.03781,0.02727,0.0176,0.6093,0.7060 1.250,0.0000,0.03756,0.02708,0.0154,0.6048,0.7266 1.500,0.0575,0.03709,0.02662,0.0117,0.6016,0.7473 2.000,0.0872,0.03865,0.02830,0.0149,0.5827,0.7858 2.250,0.1625,0.03824,0.02787,0.0084,0.5795,0.8024 2.750,0.2018,0.04010,0.02982,0.0095,0.5608,0.8386 3.000,0.2902,0.03954,0.02919,0.0010,0.5574,0.8490 3.250,0.2821,0.04165,0.03141,0.0043,0.5445,0.8668 3.500,0.3404,0.04159,0.03130,0.0000,0.5388,0.8792 3.750,0.4115,0.04086,0.03048,-0.0057,0.5350,0.8906 4.000,0.3959,0.04341,0.03314,-0.0018,0.5219,0.9087 4.250,0.4606,0.04304,0.03272,-0.0072,0.5162,0.9179 4.500,0.5299,0.04204,0.03160,-0.0125,0.5124,0.9296 4.750,0.5113,0.04503,0.03474,-0.0092,0.4987,0.9473 5.000,0.5752,0.04427,0.03391,-0.0143,0.4934,0.9576 5.250,0.6552,0.04286,0.03236,-0.0212,0.4896,0.9659 5.500,0.6299,0.04638,0.03608,-0.0181,0.4754,0.9839 5.750,0.7022,0.04504,0.03464,-0.0241,0.4706,0.9920 6.000,0.6806,0.04772,0.03741,-0.0207,0.4598,1.0000 6.250,0.6639,0.04875,0.03840,-0.0156,0.4524,1.0000 6.500,0.6953,0.04763,0.03716,-0.0150,0.4486,1.0000 7.000,0.6192,0.05296,0.04248,-0.0023,0.4296,1.0000 7.250,0.6569,0.05146,0.04087,-0.0018,0.4269,1.0000 7.750,0.6044,0.05715,0.04654,0.0069,0.4076,1.0000 8.250,0.5702,0.06294,0.05230,0.0126,0.3886,1.0000 8.500,0.6043,0.06150,0.05078,0.0137,0.3865,1.0000 9.000,0.5163,0.07414,0.06349,0.0181,0.3578,1.0000 9.250,0.5273,0.07503,0.06435,0.0195,0.3523,1.0000 9.500,0.5516,0.07444,0.06371,0.0209,0.3494,1.0000 10.000,0.5332,0.08113,0.07039,0.0229,0.3319,1.0000 10.250,0.5467,0.08190,0.07114,0.0241,0.3276,1.0000 10.750,0.5414,0.08744,0.07668,0.0256,0.3125,1.0000 11.250,0.5251,0.09471,0.08396,0.0264,0.2964,1.0000 11.750,0.5106,0.10211,0.09138,0.0266,0.2816,1.0000 12.000,0.5315,0.10214,0.09139,0.0276,0.2783,1.0000 12.500,0.5156,0.11009,0.09937,0.0272,0.2638,1.0000 12.750,0.5379,0.10997,0.09923,0.0282,0.2609,1.0000 13.000,0.5095,0.11697,0.10627,0.0268,0.2512,1.0000 13.250,0.5218,0.11824,0.10754,0.0272,0.2469,1.0000 13.500,0.5437,0.11821,0.10750,0.0281,0.2444,1.0000 14.000,0.5269,0.12692,0.11625,0.0265,0.2310,1.0000 14.250,0.5487,0.12690,0.11621,0.0274,0.2286,1.0000 14.750,0.5315,0.13600,0.12537,0.0252,0.2160,1.0000 15.000,0.5517,0.13623,0.12558,0.0259,0.2137,1.0000