Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-dormoy-il-50000-n5 Airfoil,dormoy-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,36.2098 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-dormoy-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.4139,0.10202,0.09595,-0.0276,1.0000,0.1509 -9.250,-0.3935,0.09655,0.09048,-0.0254,1.0000,0.1551 -8.750,-0.4199,0.09281,0.08707,-0.0290,1.0000,0.1660 -8.500,-0.4032,0.08818,0.08245,-0.0258,1.0000,0.1693 -7.500,-0.4010,0.06891,0.06324,-0.0388,1.0000,0.0764 -7.250,-0.3966,0.06437,0.05860,-0.0399,1.0000,0.0629 -7.000,-0.3914,0.05985,0.05375,-0.0413,1.0000,0.0535 -6.750,-0.3864,0.05670,0.05063,-0.0397,1.0000,0.0508 -6.500,-0.3802,0.05321,0.04699,-0.0389,1.0000,0.0476 -6.250,-0.3670,0.04995,0.04286,-0.0387,1.0000,0.0421 -6.000,-0.3577,0.04639,0.03937,-0.0374,1.0000,0.0405 -5.750,-0.3455,0.04342,0.03615,-0.0364,1.0000,0.0388 -5.500,-0.3303,0.04049,0.03278,-0.0354,1.0000,0.0369 -5.250,-0.3122,0.03776,0.02952,-0.0344,1.0000,0.0350 -5.000,-0.2771,0.03542,0.02623,-0.0353,0.9948,0.0328 -4.750,-0.2426,0.03269,0.02310,-0.0369,0.9887,0.0322 -4.500,-0.2076,0.03045,0.02043,-0.0382,0.9822,0.0317 -4.250,-0.1715,0.02885,0.01834,-0.0393,0.9757,0.0327 -4.000,-0.1375,0.02696,0.01628,-0.0405,0.9695,0.0352 -3.750,-0.1036,0.02570,0.01478,-0.0413,0.9624,0.0370 -3.500,-0.0662,0.02470,0.01345,-0.0429,0.9559,0.0388 -3.250,-0.0332,0.02390,0.01236,-0.0438,0.9474,0.0431 -2.750,0.0382,0.02183,0.01062,-0.0471,0.9320,0.1931 -2.500,0.0991,0.01915,0.01036,-0.0523,0.9298,1.0000 -2.250,0.1366,0.01924,0.00991,-0.0542,0.9179,1.0000 -2.000,0.1759,0.01928,0.00954,-0.0564,0.9055,1.0000 -1.750,0.2169,0.01926,0.00917,-0.0588,0.8925,1.0000 -1.500,0.2567,0.01918,0.00877,-0.0609,0.8783,1.0000 -1.250,0.2939,0.01912,0.00849,-0.0623,0.8642,1.0000 -1.000,0.3282,0.01910,0.00831,-0.0633,0.8507,1.0000 -0.750,0.3599,0.01916,0.00821,-0.0639,0.8382,1.0000 -0.500,0.3905,0.01923,0.00819,-0.0643,0.8257,1.0000 -0.250,0.4202,0.01929,0.00818,-0.0644,0.8119,1.0000 0.000,0.4486,0.01935,0.00820,-0.0642,0.7968,1.0000 0.250,0.4759,0.01941,0.00823,-0.0637,0.7805,1.0000 0.500,0.5030,0.01944,0.00824,-0.0631,0.7632,1.0000 0.750,0.5284,0.01949,0.00832,-0.0622,0.7447,1.0000 1.000,0.5513,0.01959,0.00844,-0.0609,0.7242,1.0000 1.250,0.5764,0.01962,0.00850,-0.0600,0.7047,1.0000 1.500,0.5992,0.01972,0.00866,-0.0587,0.6827,1.0000 1.750,0.6235,0.01974,0.00877,-0.0576,0.6591,1.0000 2.000,0.6467,0.01977,0.00882,-0.0561,0.6309,1.0000 2.250,0.6685,0.01984,0.00887,-0.0545,0.5960,1.0000 2.500,0.6900,0.01997,0.00892,-0.0528,0.5576,1.0000 2.750,0.7111,0.02023,0.00919,-0.0512,0.5204,1.0000 3.000,0.7327,0.02059,0.00955,-0.0500,0.4892,1.0000 3.250,0.7546,0.02100,0.01004,-0.0489,0.4627,1.0000 3.500,0.7767,0.02145,0.01060,-0.0479,0.4400,1.0000 3.750,0.7915,0.02213,0.01103,-0.0456,0.3854,1.0000 4.000,0.8029,0.02318,0.01162,-0.0432,0.3204,1.0000 4.250,0.8206,0.02397,0.01246,-0.0418,0.2782,1.0000 4.500,0.8360,0.02499,0.01332,-0.0401,0.1992,1.0000 4.750,0.8387,0.02781,0.01506,-0.0376,0.0645,1.0000 5.000,0.8512,0.02985,0.01729,-0.0356,0.0439,1.0000 5.250,0.8666,0.03135,0.01907,-0.0339,0.0344,1.0000 5.500,0.8803,0.03289,0.02094,-0.0321,0.0309,1.0000 5.750,0.8905,0.03464,0.02291,-0.0301,0.0286,1.0000 6.000,0.8990,0.03637,0.02489,-0.0279,0.0270,1.0000 6.250,0.9046,0.03816,0.02688,-0.0255,0.0250,1.0000 6.500,0.9086,0.03999,0.02888,-0.0232,0.0237,1.0000 6.750,0.9110,0.04204,0.03108,-0.0209,0.0226,1.0000 7.000,0.9150,0.04424,0.03342,-0.0188,0.0222,1.0000 7.250,0.9262,0.04640,0.03571,-0.0169,0.0219,1.0000 7.500,0.9598,0.04872,0.03813,-0.0160,0.0217,1.0000 7.750,1.0048,0.05214,0.04178,-0.0169,0.0217,1.0000 8.000,1.0313,0.05585,0.04590,-0.0166,0.0217,1.0000 8.250,1.0441,0.05926,0.04966,-0.0153,0.0217,1.0000 8.500,1.0479,0.06241,0.05316,-0.0134,0.0216,1.0000 8.750,1.0457,0.06560,0.05668,-0.0112,0.0215,1.0000 9.000,1.0402,0.06871,0.06009,-0.0092,0.0214,1.0000 9.250,1.0321,0.07204,0.06369,-0.0077,0.0214,1.0000 9.500,1.0214,0.07567,0.06757,-0.0067,0.0214,1.0000 9.750,1.0081,0.07955,0.07168,-0.0065,0.0214,1.0000 10.000,0.9958,0.08376,0.07609,-0.0069,0.0215,1.0000 10.250,0.9840,0.08827,0.08077,-0.0079,0.0217,1.0000 10.500,0.9700,0.09327,0.08594,-0.0096,0.0217,1.0000 10.750,0.9563,0.09852,0.09134,-0.0119,0.0218,1.0000 11.000,0.9383,0.10409,0.09719,-0.0157,0.0223,1.0000 11.250,0.9139,0.11202,0.10531,-0.0216,0.0229,1.0000