Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca16009-il-1000000-n5 Airfoil,naca16009-il Reynolds number,1000000 Ncrit,5 Mach,0 Max Cl/Cd,47.0661 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-naca16009-il-1000000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.6648,0.07769,0.07613,-0.0369,1.0000,0.0020 -10.000,-0.6854,0.07178,0.07017,-0.0399,1.0000,0.0020 -9.750,-0.7091,0.06780,0.06615,-0.0383,1.0000,0.0019 -8.750,-0.8460,0.02448,0.02069,-0.0170,0.9882,0.0020 -8.500,-0.8290,0.02170,0.01751,-0.0157,0.9866,0.0021 -8.250,-0.8058,0.02025,0.01583,-0.0155,0.9854,0.0023 -8.000,-0.7804,0.01914,0.01454,-0.0156,0.9845,0.0023 -7.750,-0.7588,0.01675,0.01179,-0.0150,0.9836,0.0026 -7.500,-0.7315,0.01595,0.01088,-0.0155,0.9829,0.0029 -7.250,-0.7032,0.01541,0.01026,-0.0162,0.9823,0.0030 -7.000,-0.6762,0.01477,0.00954,-0.0165,0.9814,0.0032 -6.750,-0.6547,0.01417,0.00886,-0.0154,0.9786,0.0035 -6.500,-0.6304,0.01349,0.00805,-0.0150,0.9766,0.0037 -6.250,-0.6048,0.01288,0.00735,-0.0149,0.9748,0.0041 -6.000,-0.5779,0.01240,0.00681,-0.0150,0.9733,0.0046 -5.750,-0.5505,0.01199,0.00635,-0.0153,0.9719,0.0050 -5.500,-0.5232,0.01156,0.00586,-0.0155,0.9706,0.0052 -5.250,-0.4983,0.01076,0.00494,-0.0151,0.9691,0.0059 -5.000,-0.4755,0.01025,0.00435,-0.0142,0.9665,0.0066 -4.750,-0.4517,0.00991,0.00394,-0.0135,0.9635,0.0072 -4.500,-0.4261,0.00961,0.00359,-0.0132,0.9612,0.0077 -4.250,-0.3996,0.00934,0.00329,-0.0132,0.9591,0.0084 -4.000,-0.3728,0.00908,0.00299,-0.0131,0.9573,0.0089 -3.750,-0.3452,0.00885,0.00271,-0.0133,0.9557,0.0095 -3.500,-0.3204,0.00866,0.00251,-0.0127,0.9527,0.0123 -3.250,-0.2959,0.00841,0.00230,-0.0122,0.9495,0.0257 -3.000,-0.2704,0.00817,0.00213,-0.0119,0.9468,0.0454 -2.750,-0.2441,0.00795,0.00198,-0.0118,0.9444,0.0663 -2.500,-0.2175,0.00769,0.00183,-0.0118,0.9424,0.0973 -2.250,-0.1953,0.00731,0.00169,-0.0109,0.9386,0.1666 -2.000,-0.1787,0.00646,0.00149,-0.0090,0.9341,0.3474 -1.750,-0.1654,0.00541,0.00122,-0.0064,0.9301,0.5672 -1.500,-0.1482,0.00489,0.00110,-0.0042,0.9258,0.6777 -1.250,-0.1268,0.00463,0.00104,-0.0029,0.9216,0.7366 -1.000,-0.1046,0.00439,0.00102,-0.0016,0.9181,0.7999 -0.750,-0.0800,0.00425,0.00106,-0.0008,0.9152,0.8531 -0.500,-0.0548,0.00424,0.00113,-0.0002,0.9109,0.8810 -0.250,-0.0276,0.00424,0.00117,0.0000,0.9067,0.8942 0.000,0.0000,0.00424,0.00114,0.0000,0.9023,0.9024 0.250,0.0276,0.00424,0.00117,0.0000,0.8942,0.9067 0.500,0.0548,0.00424,0.00113,0.0002,0.8810,0.9109 0.750,0.0800,0.00425,0.00106,0.0008,0.8535,0.9152 1.000,0.1045,0.00438,0.00102,0.0016,0.7998,0.9181 1.250,0.1267,0.00463,0.00104,0.0029,0.7361,0.9216 1.500,0.1482,0.00489,0.00110,0.0042,0.6782,0.9257 1.750,0.1658,0.00539,0.00121,0.0063,0.5719,0.9300 2.000,0.1791,0.00643,0.00148,0.0089,0.3539,0.9340 2.250,0.1953,0.00731,0.00169,0.0109,0.1666,0.9386 2.500,0.2175,0.00770,0.00183,0.0118,0.0966,0.9424 2.750,0.2441,0.00795,0.00198,0.0118,0.0662,0.9444 3.000,0.2705,0.00817,0.00213,0.0119,0.0457,0.9467 3.250,0.2959,0.00841,0.00230,0.0122,0.0256,0.9495 3.500,0.3204,0.00867,0.00251,0.0127,0.0122,0.9527 3.750,0.3452,0.00885,0.00271,0.0133,0.0095,0.9557 4.000,0.3728,0.00908,0.00298,0.0131,0.0089,0.9572 4.250,0.3996,0.00934,0.00329,0.0132,0.0084,0.9591 4.500,0.4261,0.00961,0.00359,0.0132,0.0077,0.9611 4.750,0.4516,0.00992,0.00394,0.0135,0.0072,0.9636 5.000,0.4753,0.01025,0.00435,0.0142,0.0067,0.9666 5.250,0.4983,0.01077,0.00495,0.0151,0.0059,0.9692 5.500,0.5232,0.01155,0.00585,0.0155,0.0052,0.9706 5.750,0.5505,0.01199,0.00635,0.0153,0.0050,0.9719 6.000,0.5778,0.01242,0.00683,0.0150,0.0046,0.9733 6.250,0.6048,0.01285,0.00732,0.0149,0.0041,0.9748 6.500,0.6303,0.01349,0.00805,0.0150,0.0037,0.9766 6.750,0.6547,0.01415,0.00884,0.0154,0.0035,0.9787 7.000,0.6759,0.01479,0.00956,0.0166,0.0033,0.9815 7.250,0.7034,0.01544,0.01030,0.0162,0.0031,0.9823 7.500,0.7317,0.01596,0.01089,0.0155,0.0029,0.9830 7.750,0.7588,0.01677,0.01181,0.0150,0.0026,0.9836 8.000,0.7800,0.01920,0.01461,0.0157,0.0023,0.9845 8.250,0.8060,0.02014,0.01571,0.0155,0.0023,0.9854 8.500,0.8289,0.02172,0.01753,0.0158,0.0021,0.9866 8.750,0.8460,0.02449,0.02070,0.0170,0.0020,0.9882 9.250,0.7535,0.06020,0.05839,0.0308,0.0019,0.9984 9.500,0.7358,0.06540,0.06370,0.0330,0.0019,1.0000 9.750,0.7092,0.06781,0.06616,0.0383,0.0019,1.0000 10.000,0.6854,0.07184,0.07023,0.0398,0.0020,1.0000 10.250,0.6656,0.07765,0.07609,0.0368,0.0020,1.0000