Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca16009-il-500000-n5 Airfoil,naca16009-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,38.014 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-naca16009-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.6315,0.08401,0.08178,-0.0317,1.0000,0.0037 -9.750,-0.6473,0.07710,0.07487,-0.0375,1.0000,0.0036 -9.500,-0.6673,0.07229,0.07002,-0.0383,1.0000,0.0036 -9.250,-0.6902,0.06890,0.06659,-0.0355,1.0000,0.0035 -9.000,-0.7145,0.06639,0.06405,-0.0302,1.0000,0.0035 -8.750,-0.7333,0.06303,0.06060,-0.0258,1.0000,0.0035 -8.500,-0.7501,0.05952,0.05699,-0.0211,1.0000,0.0034 -8.250,-0.7542,0.05376,0.05100,-0.0195,0.9981,0.0034 -8.000,-0.7521,0.04698,0.04390,-0.0183,0.9953,0.0034 -7.750,-0.7490,0.04003,0.03653,-0.0159,0.9928,0.0034 -7.500,-0.7457,0.03307,0.02903,-0.0122,0.9892,0.0036 -7.250,-0.7351,0.02743,0.02279,-0.0093,0.9865,0.0040 -7.000,-0.7163,0.02400,0.01887,-0.0078,0.9848,0.0044 -6.750,-0.6926,0.02177,0.01626,-0.0073,0.9836,0.0047 -6.500,-0.6657,0.02045,0.01465,-0.0074,0.9827,0.0051 -6.250,-0.6395,0.01862,0.01252,-0.0075,0.9819,0.0058 -6.000,-0.6181,0.01715,0.01086,-0.0064,0.9797,0.0063 -5.750,-0.5950,0.01601,0.00956,-0.0056,0.9774,0.0066 -5.500,-0.5699,0.01508,0.00852,-0.0053,0.9754,0.0071 -5.250,-0.5435,0.01430,0.00764,-0.0052,0.9738,0.0078 -5.000,-0.5163,0.01362,0.00687,-0.0054,0.9723,0.0086 -4.750,-0.4882,0.01302,0.00618,-0.0057,0.9711,0.0093 -4.500,-0.4585,0.01265,0.00571,-0.0065,0.9701,0.0102 -4.250,-0.4297,0.01205,0.00502,-0.0070,0.9692,0.0110 -4.000,-0.4044,0.01157,0.00443,-0.0066,0.9670,0.0121 -3.750,-0.3818,0.01124,0.00406,-0.0056,0.9634,0.0150 -3.500,-0.3544,0.01091,0.00375,-0.0057,0.9614,0.0257 -3.250,-0.3261,0.01057,0.00349,-0.0062,0.9597,0.0484 -3.000,-0.2977,0.01021,0.00324,-0.0067,0.9582,0.0833 -2.750,-0.2705,0.00969,0.00300,-0.0070,0.9568,0.1578 -2.500,-0.2536,0.00854,0.00271,-0.0055,0.9539,0.3730 -2.250,-0.2448,0.00751,0.00245,-0.0018,0.9483,0.5719 -2.000,-0.2306,0.00666,0.00233,0.0011,0.9451,0.7492 -1.750,-0.2030,0.00647,0.00234,0.0013,0.9436,0.8106 -1.500,-0.1722,0.00642,0.00234,0.0007,0.9425,0.8421 -1.250,-0.1462,0.00653,0.00255,0.0014,0.9394,0.8833 -1.000,-0.1185,0.00671,0.00277,0.0018,0.9366,0.9068 -0.750,-0.0913,0.00676,0.00281,0.0020,0.9339,0.9165 -0.500,-0.0585,0.00681,0.00283,0.0008,0.9322,0.9198 -0.250,-0.0268,0.00681,0.00282,-0.0001,0.9304,0.9230 0.000,0.0000,0.00679,0.00279,0.0000,0.9274,0.9274 0.250,0.0268,0.00681,0.00282,0.0001,0.9230,0.9304 0.500,0.0585,0.00681,0.00283,-0.0008,0.9198,0.9321 0.750,0.0913,0.00676,0.00281,-0.0020,0.9165,0.9338 1.000,0.1185,0.00671,0.00277,-0.0018,0.9068,0.9366 1.250,0.1462,0.00653,0.00255,-0.0014,0.8834,0.9394 1.500,0.1722,0.00642,0.00234,-0.0007,0.8424,0.9425 1.750,0.2030,0.00647,0.00234,-0.0013,0.8106,0.9436 2.000,0.2306,0.00665,0.00234,-0.0011,0.7504,0.9451 2.250,0.2449,0.00751,0.00245,0.0018,0.5724,0.9483 2.500,0.2535,0.00855,0.00271,0.0055,0.3716,0.9539 2.750,0.2704,0.00970,0.00301,0.0070,0.1552,0.9568 3.000,0.2977,0.01021,0.00324,0.0067,0.0835,0.9582 3.250,0.3260,0.01057,0.00349,0.0062,0.0480,0.9597 3.500,0.3543,0.01091,0.00375,0.0057,0.0255,0.9614 3.750,0.3817,0.01124,0.00406,0.0056,0.0150,0.9635 4.000,0.4041,0.01157,0.00443,0.0066,0.0121,0.9670 4.250,0.4295,0.01205,0.00501,0.0070,0.0110,0.9692 4.500,0.4585,0.01264,0.00570,0.0065,0.0102,0.9701 4.750,0.4883,0.01303,0.00618,0.0057,0.0093,0.9712 5.000,0.5164,0.01362,0.00687,0.0053,0.0086,0.9724 5.250,0.5436,0.01430,0.00764,0.0052,0.0078,0.9738 5.500,0.5697,0.01507,0.00851,0.0053,0.0071,0.9754 5.750,0.5949,0.01600,0.00955,0.0056,0.0066,0.9774 6.000,0.6180,0.01715,0.01085,0.0064,0.0063,0.9797 6.250,0.6394,0.01863,0.01253,0.0075,0.0057,0.9819 6.500,0.6656,0.02046,0.01467,0.0075,0.0051,0.9827 6.750,0.6926,0.02175,0.01624,0.0073,0.0047,0.9837 7.000,0.7163,0.02402,0.01889,0.0078,0.0044,0.9849 7.250,0.7352,0.02744,0.02280,0.0093,0.0040,0.9866 7.500,0.7458,0.03311,0.02907,0.0122,0.0036,0.9893 7.750,0.7491,0.04006,0.03656,0.0158,0.0034,0.9928 8.000,0.7522,0.04700,0.04391,0.0183,0.0034,0.9954 8.250,0.7543,0.05377,0.05102,0.0195,0.0034,0.9981 8.500,0.7501,0.05951,0.05698,0.0212,0.0034,1.0000 8.750,0.7333,0.06302,0.06060,0.0258,0.0035,1.0000 9.000,0.7145,0.06638,0.06404,0.0302,0.0035,1.0000 9.250,0.6902,0.06891,0.06661,0.0355,0.0035,1.0000 9.500,0.6675,0.07231,0.07005,0.0382,0.0036,1.0000 9.750,0.6477,0.07713,0.07491,0.0374,0.0036,1.0000 10.000,0.6320,0.08409,0.08186,0.0316,0.0037,1.0000