Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fx69h083-il-100000-n5 Airfoil,fx69h083-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,52.3556 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-fx69h083-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.4808,0.09437,0.08989,-0.0101,1.0000,0.0380 -8.000,-0.4782,0.09040,0.08597,-0.0130,1.0000,0.0384 -7.750,-0.4764,0.08629,0.08192,-0.0165,1.0000,0.0387 -7.500,-0.4727,0.08194,0.07759,-0.0206,1.0000,0.0388 -7.000,-0.4582,0.07144,0.06701,-0.0290,1.0000,0.0287 -6.750,-0.4503,0.06667,0.06219,-0.0316,1.0000,0.0265 -6.500,-0.4411,0.06195,0.05738,-0.0339,1.0000,0.0255 -6.250,-0.4318,0.05781,0.05313,-0.0351,1.0000,0.0256 -6.000,-0.4245,0.05422,0.04941,-0.0349,1.0000,0.0262 -5.750,-0.4200,0.05100,0.04604,-0.0335,1.0000,0.0266 -5.500,-0.4133,0.04766,0.04251,-0.0321,0.9991,0.0266 -5.250,-0.3841,0.04232,0.03673,-0.0350,0.9907,0.0256 -5.000,-0.3536,0.03723,0.03110,-0.0370,0.9834,0.0246 -4.750,-0.3213,0.03284,0.02611,-0.0387,0.9774,0.0244 -4.500,-0.2904,0.02938,0.02206,-0.0396,0.9702,0.0248 -4.250,-0.2578,0.02690,0.01901,-0.0407,0.9639,0.0275 -4.000,-0.2246,0.02469,0.01622,-0.0414,0.9574,0.0305 -3.750,-0.1920,0.02264,0.01369,-0.0419,0.9508,0.0316 -3.500,-0.1597,0.02074,0.01149,-0.0425,0.9443,0.0333 -3.250,-0.1299,0.01965,0.01034,-0.0431,0.9367,0.0393 -3.000,-0.0993,0.01851,0.00905,-0.0434,0.9296,0.0418 -2.750,-0.0720,0.01763,0.00804,-0.0430,0.9209,0.0440 -2.500,-0.0445,0.01682,0.00709,-0.0428,0.9131,0.0479 -2.250,-0.0184,0.01627,0.00643,-0.0423,0.9036,0.0562 -2.000,0.0070,0.01559,0.00587,-0.0417,0.8942,0.0890 -1.750,0.0275,0.01354,0.00550,-0.0409,0.8865,0.4889 -1.500,0.1268,0.01244,0.00536,-0.0532,0.8894,1.0000 -1.250,0.1505,0.01246,0.00517,-0.0523,0.8781,1.0000 -1.000,0.1741,0.01248,0.00501,-0.0514,0.8671,1.0000 -0.750,0.1976,0.01250,0.00484,-0.0505,0.8565,1.0000 -0.500,0.2211,0.01251,0.00470,-0.0495,0.8459,1.0000 -0.250,0.2445,0.01254,0.00460,-0.0485,0.8339,1.0000 0.000,0.2680,0.01257,0.00451,-0.0475,0.8220,1.0000 0.250,0.2916,0.01260,0.00443,-0.0466,0.8104,1.0000 0.500,0.3154,0.01263,0.00437,-0.0456,0.7994,1.0000 0.750,0.3392,0.01266,0.00432,-0.0447,0.7888,1.0000 1.000,0.3634,0.01272,0.00431,-0.0439,0.7775,1.0000 1.250,0.3876,0.01278,0.00435,-0.0431,0.7656,1.0000 1.500,0.4119,0.01284,0.00437,-0.0423,0.7535,1.0000 1.750,0.4361,0.01291,0.00440,-0.0415,0.7410,1.0000 2.000,0.4604,0.01298,0.00444,-0.0406,0.7280,1.0000 2.250,0.4848,0.01305,0.00452,-0.0398,0.7144,1.0000 2.500,0.5090,0.01312,0.00458,-0.0390,0.6993,1.0000 2.750,0.5334,0.01320,0.00465,-0.0381,0.6837,1.0000 3.000,0.5579,0.01330,0.00475,-0.0373,0.6682,1.0000 3.250,0.5825,0.01341,0.00492,-0.0365,0.6526,1.0000 3.500,0.6071,0.01354,0.00506,-0.0358,0.6357,1.0000 3.750,0.6316,0.01369,0.00525,-0.0350,0.6168,1.0000 4.000,0.6560,0.01385,0.00543,-0.0342,0.5978,1.0000 4.250,0.6804,0.01404,0.00566,-0.0335,0.5777,1.0000 4.500,0.7049,0.01426,0.00598,-0.0328,0.5576,1.0000 4.750,0.7293,0.01450,0.00629,-0.0321,0.5376,1.0000 5.000,0.7538,0.01476,0.00666,-0.0314,0.5168,1.0000 5.250,0.7779,0.01504,0.00703,-0.0307,0.4939,1.0000 5.500,0.8017,0.01536,0.00744,-0.0299,0.4687,1.0000 5.750,0.8246,0.01575,0.00788,-0.0290,0.4347,1.0000 6.000,0.8422,0.01650,0.00834,-0.0273,0.3493,1.0000 6.250,0.8523,0.01836,0.00914,-0.0255,0.1745,1.0000 6.500,0.8636,0.02049,0.01053,-0.0239,0.0793,1.0000 6.750,0.8784,0.02221,0.01204,-0.0222,0.0371,1.0000 7.000,0.8943,0.02367,0.01356,-0.0207,0.0272,1.0000 7.250,0.9105,0.02502,0.01511,-0.0191,0.0237,1.0000 7.500,0.9244,0.02657,0.01681,-0.0174,0.0215,1.0000 7.750,0.9347,0.02867,0.01904,-0.0152,0.0200,1.0000 8.000,0.9513,0.03021,0.02073,-0.0137,0.0185,1.0000 8.250,0.9686,0.03181,0.02252,-0.0123,0.0165,1.0000 8.500,0.9860,0.03381,0.02482,-0.0109,0.0154,1.0000 8.750,1.0038,0.03617,0.02741,-0.0096,0.0148,1.0000 9.000,1.0203,0.03879,0.03032,-0.0083,0.0144,1.0000 9.250,1.0342,0.04166,0.03353,-0.0068,0.0140,1.0000 9.500,1.0439,0.04475,0.03699,-0.0051,0.0138,1.0000 9.750,1.0492,0.04802,0.04063,-0.0032,0.0137,1.0000 10.000,1.0497,0.05140,0.04439,-0.0012,0.0136,1.0000 10.250,1.0441,0.05472,0.04804,0.0012,0.0136,1.0000 10.500,1.0342,0.05812,0.05174,0.0033,0.0137,1.0000 10.750,1.0218,0.06180,0.05569,0.0046,0.0137,1.0000 11.000,1.0071,0.06589,0.06004,0.0050,0.0137,1.0000 11.250,0.9902,0.07060,0.06500,0.0043,0.0138,1.0000 11.500,0.9715,0.07604,0.07067,0.0024,0.0140,1.0000 11.750,0.9515,0.08235,0.07718,-0.0008,0.0141,1.0000 12.000,0.9307,0.08965,0.08465,-0.0052,0.0143,1.0000 12.250,0.9098,0.09805,0.09319,-0.0108,0.0146,1.0000