Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fx69h083-il-50000-n5 Airfoil,fx69h083-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,37.0068 Max Cl/Cd alpha,6.5 Url,http://airfoiltools.com/polar/csv?polar=xf-fx69h083-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.4932,0.11458,0.10807,-0.0032,1.0000,0.0952 -9.000,-0.4975,0.11184,0.10543,-0.0072,1.0000,0.0990 -8.750,-0.5072,0.10941,0.10312,-0.0134,1.0000,0.1002 -8.500,-0.4923,0.10384,0.09756,-0.0113,1.0000,0.1022 -8.250,-0.4832,0.09978,0.09352,-0.0113,1.0000,0.1051 -8.000,-0.4802,0.09613,0.08994,-0.0133,1.0000,0.1082 -7.750,-0.4941,0.09358,0.08746,-0.0230,1.0000,0.1140 -7.500,-0.3856,0.07289,0.06710,-0.0284,1.0000,0.0666 -7.250,-0.3919,0.06774,0.06195,-0.0317,1.0000,0.0554 -7.000,-0.4586,0.07589,0.06960,-0.0310,1.0000,0.0567 -6.750,-0.4505,0.07158,0.06529,-0.0316,1.0000,0.0526 -6.500,-0.4412,0.06598,0.05923,-0.0364,1.0000,0.0451 -6.250,-0.4318,0.06197,0.05527,-0.0359,1.0000,0.0440 -6.000,-0.4229,0.05822,0.05141,-0.0357,1.0000,0.0432 -5.750,-0.4140,0.05464,0.04763,-0.0353,1.0000,0.0432 -5.500,-0.4053,0.05133,0.04402,-0.0342,1.0000,0.0439 -5.250,-0.3959,0.04827,0.04055,-0.0328,1.0000,0.0447 -5.000,-0.3847,0.04558,0.03740,-0.0310,1.0000,0.0453 -4.500,-0.3589,0.03980,0.03093,-0.0276,1.0000,0.0453 -4.250,-0.3431,0.03714,0.02785,-0.0260,1.0000,0.0453 -4.000,-0.3259,0.03437,0.02466,-0.0247,1.0000,0.0458 -3.750,-0.3070,0.03199,0.02196,-0.0236,1.0000,0.0470 -3.500,-0.2881,0.03046,0.02026,-0.0227,1.0000,0.0518 -3.250,-0.2659,0.02891,0.01823,-0.0216,1.0000,0.0564 -3.000,-0.2298,0.02701,0.01580,-0.0227,0.9952,0.0584 -2.750,-0.1924,0.02516,0.01379,-0.0243,0.9895,0.0618 -2.500,-0.1534,0.02391,0.01226,-0.0262,0.9835,0.0676 -2.250,-0.1148,0.02293,0.01102,-0.0284,0.9771,0.0819 -2.000,-0.0785,0.02193,0.00998,-0.0304,0.9694,0.1081 -1.750,-0.0129,0.01791,0.00911,-0.0363,0.9745,1.0000 -1.500,0.0280,0.01806,0.00868,-0.0393,0.9653,1.0000 -1.250,0.0689,0.01821,0.00835,-0.0423,0.9559,1.0000 -1.000,0.1074,0.01836,0.00817,-0.0449,0.9455,1.0000 -0.750,0.1443,0.01853,0.00806,-0.0471,0.9348,1.0000 -0.500,0.1808,0.01870,0.00797,-0.0491,0.9243,1.0000 -0.250,0.2170,0.01886,0.00795,-0.0510,0.9140,1.0000 0.000,0.2479,0.01905,0.00800,-0.0518,0.9019,1.0000 0.250,0.2770,0.01925,0.00808,-0.0522,0.8893,1.0000 0.500,0.3053,0.01944,0.00817,-0.0523,0.8766,1.0000 0.750,0.3326,0.01962,0.00828,-0.0522,0.8636,1.0000 1.000,0.3590,0.01980,0.00841,-0.0519,0.8506,1.0000 1.250,0.3847,0.01998,0.00857,-0.0514,0.8374,1.0000 1.500,0.4099,0.02015,0.00872,-0.0507,0.8244,1.0000 1.750,0.4348,0.02033,0.00889,-0.0500,0.8115,1.0000 2.000,0.4595,0.02051,0.00908,-0.0492,0.7988,1.0000 2.250,0.4844,0.02068,0.00932,-0.0484,0.7861,1.0000 2.500,0.5093,0.02085,0.00954,-0.0476,0.7734,1.0000 2.750,0.5339,0.02101,0.00976,-0.0468,0.7605,1.0000 3.000,0.5584,0.02118,0.01001,-0.0458,0.7473,1.0000 3.250,0.5825,0.02136,0.01028,-0.0448,0.7335,1.0000 3.500,0.6062,0.02154,0.01064,-0.0438,0.7187,1.0000 3.750,0.6297,0.02173,0.01095,-0.0427,0.7032,1.0000 4.000,0.6533,0.02189,0.01126,-0.0415,0.6870,1.0000 4.250,0.6772,0.02204,0.01155,-0.0403,0.6707,1.0000 4.500,0.7013,0.02218,0.01193,-0.0391,0.6544,1.0000 4.750,0.7257,0.02232,0.01225,-0.0379,0.6383,1.0000 5.000,0.7486,0.02252,0.01265,-0.0366,0.6184,1.0000 5.250,0.7722,0.02258,0.01288,-0.0350,0.5972,1.0000 5.500,0.7944,0.02271,0.01320,-0.0333,0.5719,1.0000 5.750,0.8164,0.02288,0.01357,-0.0316,0.5452,1.0000 6.000,0.8381,0.02310,0.01413,-0.0300,0.5168,1.0000 6.250,0.8587,0.02333,0.01455,-0.0280,0.4823,1.0000 6.500,0.8741,0.02362,0.01483,-0.0252,0.4201,1.0000 6.750,0.8790,0.02477,0.01523,-0.0215,0.2822,1.0000 7.000,0.8766,0.02781,0.01693,-0.0187,0.1345,1.0000 7.250,0.8796,0.03084,0.01942,-0.0164,0.0797,1.0000 7.500,0.8883,0.03306,0.02162,-0.0144,0.0574,1.0000 7.750,0.8979,0.03513,0.02380,-0.0123,0.0498,1.0000 8.000,0.9092,0.03712,0.02593,-0.0103,0.0446,1.0000 8.250,0.9230,0.03923,0.02815,-0.0085,0.0401,1.0000 8.500,0.9410,0.04118,0.03039,-0.0070,0.0349,1.0000 8.750,0.9600,0.04353,0.03290,-0.0058,0.0321,1.0000 9.000,0.9823,0.04686,0.03654,-0.0048,0.0304,1.0000 9.250,1.0006,0.05038,0.04043,-0.0037,0.0296,1.0000 9.500,1.0118,0.05387,0.04439,-0.0022,0.0292,1.0000 9.750,1.0166,0.05746,0.04843,-0.0006,0.0288,1.0000 10.000,1.0155,0.06107,0.05246,0.0012,0.0284,1.0000 10.250,1.0082,0.06459,0.05632,0.0030,0.0281,1.0000 10.500,0.9969,0.06826,0.06029,0.0044,0.0279,1.0000 10.750,0.9833,0.07230,0.06458,0.0049,0.0278,1.0000 11.000,0.9681,0.07676,0.06928,0.0044,0.0279,1.0000 11.250,0.9516,0.08175,0.07446,0.0030,0.0280,1.0000 11.500,0.9347,0.08731,0.08018,0.0006,0.0282,1.0000 11.750,0.9179,0.09346,0.08645,-0.0026,0.0286,1.0000