Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rc08b3-il-100000-n5 Airfoil,rc08b3-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,41.5216 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-rc08b3-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.4829,0.08388,0.07907,-0.0172,1.0000,0.0409 -8.500,-0.5987,0.08361,0.07864,-0.0179,1.0000,0.0421 -8.250,-0.6004,0.07938,0.07441,-0.0187,1.0000,0.0398 -8.000,-0.6152,0.06904,0.06370,-0.0249,1.0000,0.0329 -7.750,-0.6126,0.06500,0.05961,-0.0247,1.0000,0.0322 -7.500,-0.6090,0.06094,0.05543,-0.0244,1.0000,0.0318 -7.250,-0.6045,0.05680,0.05113,-0.0239,1.0000,0.0313 -7.000,-0.5986,0.05267,0.04678,-0.0230,1.0000,0.0309 -6.750,-0.5915,0.04865,0.04247,-0.0217,1.0000,0.0305 -6.500,-0.5831,0.04481,0.03832,-0.0201,1.0000,0.0303 -6.250,-0.5733,0.04128,0.03445,-0.0181,1.0000,0.0301 -6.000,-0.5620,0.03814,0.03090,-0.0159,1.0000,0.0308 -5.750,-0.5493,0.03541,0.02770,-0.0134,1.0000,0.0320 -5.500,-0.5350,0.03303,0.02487,-0.0111,1.0000,0.0325 -5.250,-0.5195,0.03069,0.02216,-0.0089,1.0000,0.0326 -5.000,-0.5025,0.02860,0.01967,-0.0069,1.0000,0.0327 -4.750,-0.4840,0.02677,0.01749,-0.0051,1.0000,0.0329 -4.500,-0.4644,0.02504,0.01549,-0.0035,1.0000,0.0332 -4.250,-0.4441,0.02328,0.01355,-0.0022,1.0000,0.0339 -4.000,-0.4232,0.02196,0.01211,-0.0009,1.0000,0.0348 -3.750,-0.4022,0.02089,0.01096,0.0003,1.0000,0.0360 -3.500,-0.3814,0.02008,0.01006,0.0016,1.0000,0.0383 -3.250,-0.3604,0.01940,0.00928,0.0028,1.0000,0.0418 -3.000,-0.3393,0.01870,0.00848,0.0041,1.0000,0.0441 -2.750,-0.3195,0.01780,0.00761,0.0054,1.0000,0.0469 -2.500,-0.2961,0.01719,0.00697,0.0061,0.9990,0.0516 -2.250,-0.2623,0.01651,0.00624,0.0047,0.9945,0.0623 -2.000,-0.2295,0.01580,0.00572,0.0034,0.9893,0.1010 -1.750,-0.1998,0.01413,0.00539,0.0020,0.9859,0.3746 -1.500,-0.0500,0.01312,0.00596,-0.0192,1.0000,1.0000 -1.250,-0.0408,0.01319,0.00592,-0.0161,1.0000,1.0000 -1.000,-0.0260,0.01326,0.00587,-0.0142,0.9984,1.0000 -0.750,0.0125,0.01328,0.00575,-0.0169,0.9908,1.0000 -0.500,0.0522,0.01330,0.00565,-0.0198,0.9837,1.0000 -0.250,0.0917,0.01330,0.00557,-0.0226,0.9756,1.0000 0.000,0.1317,0.01329,0.00550,-0.0255,0.9673,1.0000 0.250,0.1730,0.01326,0.00544,-0.0285,0.9594,1.0000 0.500,0.2096,0.01323,0.00540,-0.0304,0.9479,1.0000 0.750,0.2455,0.01319,0.00536,-0.0322,0.9355,1.0000 1.000,0.2791,0.01314,0.00533,-0.0333,0.9218,1.0000 1.250,0.3098,0.01309,0.00532,-0.0337,0.9070,1.0000 1.500,0.3387,0.01304,0.00529,-0.0336,0.8911,1.0000 1.750,0.3659,0.01299,0.00527,-0.0331,0.8744,1.0000 2.000,0.3907,0.01296,0.00530,-0.0321,0.8558,1.0000 2.250,0.4146,0.01293,0.00532,-0.0309,0.8355,1.0000 2.500,0.4383,0.01288,0.00530,-0.0295,0.8128,1.0000 2.750,0.4616,0.01285,0.00529,-0.0279,0.7869,1.0000 3.000,0.4842,0.01284,0.00533,-0.0263,0.7558,1.0000 3.250,0.5065,0.01286,0.00532,-0.0245,0.7164,1.0000 3.500,0.5280,0.01294,0.00528,-0.0225,0.6596,1.0000 3.750,0.5485,0.01321,0.00524,-0.0203,0.5764,1.0000 4.000,0.5674,0.01379,0.00534,-0.0182,0.4734,1.0000 4.250,0.5857,0.01460,0.00567,-0.0165,0.3695,1.0000 4.500,0.6042,0.01549,0.00610,-0.0151,0.2734,1.0000 4.750,0.6228,0.01645,0.00663,-0.0138,0.1877,1.0000 5.000,0.6414,0.01747,0.00726,-0.0125,0.1227,1.0000 5.250,0.6607,0.01840,0.00801,-0.0112,0.0916,1.0000 5.500,0.6799,0.01932,0.00885,-0.0098,0.0746,1.0000 5.750,0.6996,0.02013,0.00972,-0.0084,0.0648,1.0000 6.000,0.7183,0.02110,0.01075,-0.0068,0.0591,1.0000 6.250,0.7375,0.02199,0.01170,-0.0054,0.0535,1.0000 6.500,0.7556,0.02309,0.01280,-0.0039,0.0489,1.0000 6.750,0.7753,0.02415,0.01401,-0.0025,0.0458,1.0000 7.000,0.7950,0.02537,0.01539,-0.0011,0.0433,1.0000 7.250,0.8149,0.02670,0.01680,0.0002,0.0413,1.0000 7.500,0.8344,0.02832,0.01848,0.0014,0.0395,1.0000 7.750,0.8539,0.03007,0.02044,0.0027,0.0373,1.0000 8.000,0.8729,0.03164,0.02235,0.0041,0.0349,1.0000 8.250,0.8906,0.03373,0.02476,0.0056,0.0336,1.0000 8.500,0.9063,0.03601,0.02742,0.0073,0.0324,1.0000 8.750,0.9196,0.03840,0.03015,0.0091,0.0314,1.0000 9.000,0.9317,0.04040,0.03238,0.0107,0.0300,1.0000 9.250,0.9404,0.04314,0.03525,0.0123,0.0285,1.0000 9.500,0.9429,0.04610,0.03874,0.0149,0.0275,1.0000 9.750,0.9412,0.04967,0.04279,0.0175,0.0270,1.0000 10.000,0.9344,0.05350,0.04703,0.0201,0.0267,1.0000 10.250,0.9224,0.05743,0.05130,0.0225,0.0265,1.0000 10.500,0.9046,0.06115,0.05527,0.0250,0.0265,1.0000 10.750,0.8841,0.06526,0.05959,0.0261,0.0265,1.0000 11.000,0.8624,0.07026,0.06476,0.0251,0.0266,1.0000 11.250,0.8399,0.07650,0.07115,0.0216,0.0268,1.0000 11.500,0.8174,0.08454,0.07928,0.0158,0.0271,1.0000