Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n0009sm-il-100000 Airfoil,n0009sm-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,37.3033 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-n0009sm-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.6402,0.09783,0.09278,-0.0047,1.0000,0.1611 -9.500,-0.7228,0.07389,0.06897,-0.0257,1.0000,0.0911 -9.250,-0.7280,0.07174,0.06685,-0.0244,1.0000,0.0992 -9.000,-0.8160,0.05631,0.05037,-0.0241,1.0000,0.0670 -8.750,-0.8199,0.05152,0.04526,-0.0220,1.0000,0.0667 -8.500,-0.8242,0.04803,0.04118,-0.0189,1.0000,0.0677 -8.250,-0.8075,0.04520,0.03868,-0.0187,1.0000,0.0739 -8.000,-0.8037,0.04147,0.03449,-0.0160,1.0000,0.0757 -7.750,-0.7970,0.03798,0.03045,-0.0132,1.0000,0.0777 -7.500,-0.7890,0.03532,0.02710,-0.0102,1.0000,0.0816 -7.250,-0.7711,0.03273,0.02452,-0.0090,1.0000,0.0861 -7.000,-0.7540,0.03062,0.02204,-0.0071,1.0000,0.0904 -6.750,-0.7372,0.02863,0.01959,-0.0051,1.0000,0.0958 -6.500,-0.7158,0.02676,0.01761,-0.0039,1.0000,0.1004 -6.250,-0.6939,0.02517,0.01574,-0.0025,1.0000,0.1053 -6.000,-0.6719,0.02363,0.01415,-0.0014,1.0000,0.1123 -5.750,-0.6496,0.02250,0.01283,-0.0001,1.0000,0.1202 -5.500,-0.6265,0.02104,0.01145,0.0008,1.0000,0.1273 -5.250,-0.6042,0.01990,0.01027,0.0021,1.0000,0.1373 -5.000,-0.5836,0.01889,0.00933,0.0035,1.0000,0.1519 -4.750,-0.5639,0.01787,0.00846,0.0051,1.0000,0.1707 -4.500,-0.5459,0.01676,0.00758,0.0071,1.0000,0.2011 -4.250,-0.5316,0.01542,0.00682,0.0095,1.0000,0.2743 -4.000,-0.5198,0.01424,0.00639,0.0125,1.0000,0.3983 -3.750,-0.5050,0.01356,0.00614,0.0152,1.0000,0.4932 -3.500,-0.4884,0.01309,0.00595,0.0179,1.0000,0.5720 -3.250,-0.4707,0.01273,0.00586,0.0206,1.0000,0.6441 -3.000,-0.4511,0.01247,0.00584,0.0232,1.0000,0.7119 -2.750,-0.4276,0.01237,0.00591,0.0252,1.0000,0.7777 -2.500,-0.3961,0.01253,0.00614,0.0261,1.0000,0.8439 -2.250,-0.3457,0.01306,0.00661,0.0235,1.0000,0.8996 -2.000,-0.2781,0.01364,0.00698,0.0169,1.0000,0.9314 -1.750,-0.2084,0.01399,0.00711,0.0092,1.0000,0.9547 -1.500,-0.1341,0.01406,0.00699,0.0001,1.0000,0.9730 -1.250,-0.0629,0.01388,0.00666,-0.0089,1.0000,0.9911 -1.000,-0.0197,0.01352,0.00623,-0.0132,1.0000,1.0000 -0.750,-0.0138,0.01323,0.00594,-0.0103,1.0000,1.0000 -0.500,-0.0085,0.01303,0.00575,-0.0071,1.0000,1.0000 -0.250,-0.0040,0.01291,0.00563,-0.0036,1.0000,1.0000 0.000,0.0000,0.01287,0.00559,0.0000,1.0000,1.0000 0.250,0.0040,0.01291,0.00563,0.0036,1.0000,1.0000 0.500,0.0085,0.01303,0.00575,0.0071,1.0000,1.0000 0.750,0.0138,0.01323,0.00594,0.0103,1.0000,1.0000 1.000,0.0197,0.01352,0.00623,0.0132,1.0000,1.0000 1.250,0.0628,0.01387,0.00665,0.0090,0.9911,1.0000 1.500,0.1342,0.01406,0.00699,-0.0001,0.9730,1.0000 1.750,0.2086,0.01399,0.00710,-0.0093,0.9546,1.0000 2.000,0.2783,0.01363,0.00698,-0.0170,0.9314,1.0000 2.250,0.3459,0.01306,0.00661,-0.0235,0.8995,1.0000 2.500,0.3960,0.01253,0.00614,-0.0261,0.8439,1.0000 2.750,0.4275,0.01237,0.00591,-0.0252,0.7775,1.0000 3.000,0.4510,0.01247,0.00583,-0.0231,0.7118,1.0000 3.250,0.4705,0.01273,0.00586,-0.0206,0.6438,1.0000 3.500,0.4883,0.01309,0.00595,-0.0179,0.5719,1.0000 3.750,0.5049,0.01356,0.00614,-0.0152,0.4935,1.0000 4.000,0.5197,0.01424,0.00638,-0.0124,0.3979,1.0000 4.250,0.5315,0.01541,0.00681,-0.0095,0.2749,1.0000 4.500,0.5458,0.01676,0.00758,-0.0070,0.2010,1.0000 4.750,0.5638,0.01787,0.00846,-0.0051,0.1704,1.0000 5.000,0.5835,0.01890,0.00933,-0.0035,0.1518,1.0000 5.250,0.6041,0.01990,0.01026,-0.0021,0.1372,1.0000 5.500,0.6264,0.02104,0.01145,-0.0008,0.1274,1.0000 5.750,0.6495,0.02250,0.01282,0.0002,0.1202,1.0000 6.000,0.6719,0.02364,0.01416,0.0015,0.1124,1.0000 6.250,0.6938,0.02517,0.01574,0.0025,0.1054,1.0000 6.500,0.7158,0.02676,0.01761,0.0040,0.1004,1.0000 6.750,0.7371,0.02863,0.01959,0.0051,0.0958,1.0000 7.000,0.7540,0.03063,0.02205,0.0071,0.0905,1.0000 7.250,0.7711,0.03274,0.02453,0.0091,0.0862,1.0000 7.500,0.7891,0.03528,0.02705,0.0102,0.0817,1.0000 7.750,0.7971,0.03798,0.03044,0.0132,0.0777,1.0000 8.000,0.8036,0.04149,0.03451,0.0160,0.0756,1.0000 8.250,0.8073,0.04527,0.03876,0.0187,0.0741,1.0000 8.500,0.8242,0.04805,0.04120,0.0189,0.0677,1.0000 8.750,0.8197,0.05156,0.04531,0.0220,0.0667,1.0000 9.000,0.8155,0.05629,0.05037,0.0242,0.0669,1.0000 9.250,0.8169,0.06167,0.05590,0.0254,0.0680,1.0000 9.500,0.6962,0.09159,0.08675,0.0152,0.1627,1.0000 9.750,0.6376,0.09795,0.09289,0.0041,0.1607,1.0000