Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-s9032-il-100000 Airfoil,s9032-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,32.7393 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-s9032-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.7379,0.08392,0.07899,-0.0071,1.0000,0.0901 -9.750,-0.7529,0.07538,0.07045,-0.0125,1.0000,0.0842 -9.500,-0.8555,0.06105,0.05541,-0.0199,1.0000,0.0748 -9.250,-0.8579,0.05567,0.04983,-0.0196,1.0000,0.0742 -9.000,-0.8591,0.05062,0.04445,-0.0190,1.0000,0.0736 -8.750,-0.8575,0.04590,0.03928,-0.0180,1.0000,0.0734 -8.500,-0.8514,0.04166,0.03450,-0.0167,1.0000,0.0738 -8.250,-0.8410,0.03816,0.03039,-0.0152,1.0000,0.0747 -8.000,-0.8256,0.03489,0.02696,-0.0144,1.0000,0.0779 -7.750,-0.8055,0.03308,0.02504,-0.0136,1.0000,0.0821 -7.500,-0.7867,0.03060,0.02208,-0.0123,1.0000,0.0858 -7.250,-0.7662,0.02806,0.01914,-0.0112,1.0000,0.0899 -7.000,-0.7437,0.02648,0.01751,-0.0104,1.0000,0.0967 -6.750,-0.7215,0.02488,0.01578,-0.0095,1.0000,0.1058 -6.500,-0.6985,0.02349,0.01415,-0.0085,1.0000,0.1163 -6.250,-0.6756,0.02239,0.01299,-0.0076,1.0000,0.1294 -6.000,-0.6525,0.02120,0.01183,-0.0068,1.0000,0.1437 -5.750,-0.6296,0.02013,0.01086,-0.0060,1.0000,0.1602 -5.500,-0.6067,0.01917,0.00999,-0.0051,1.0000,0.1792 -5.250,-0.5840,0.01825,0.00913,-0.0041,1.0000,0.2025 -5.000,-0.5613,0.01738,0.00835,-0.0031,1.0000,0.2292 -4.750,-0.5392,0.01655,0.00772,-0.0020,1.0000,0.2600 -4.500,-0.5173,0.01583,0.00716,-0.0009,1.0000,0.2971 -4.250,-0.4957,0.01515,0.00670,0.0003,1.0000,0.3378 -4.000,-0.4742,0.01455,0.00632,0.0016,1.0000,0.3829 -3.750,-0.4529,0.01401,0.00600,0.0030,1.0000,0.4319 -3.500,-0.4319,0.01352,0.00575,0.0046,1.0000,0.4812 -3.250,-0.4110,0.01310,0.00554,0.0063,1.0000,0.5328 -3.000,-0.3903,0.01272,0.00540,0.0081,1.0000,0.5824 -2.750,-0.3697,0.01240,0.00527,0.0100,1.0000,0.6334 -2.500,-0.3495,0.01212,0.00518,0.0122,1.0000,0.6823 -2.250,-0.3298,0.01189,0.00514,0.0146,1.0000,0.7320 -2.000,-0.3100,0.01171,0.00512,0.0172,1.0000,0.7819 -1.750,-0.2881,0.01162,0.00517,0.0195,1.0000,0.8315 -1.500,-0.2593,0.01165,0.00526,0.0205,1.0000,0.8814 -1.250,-0.2108,0.01186,0.00543,0.0175,1.0000,0.9251 -1.000,-0.1442,0.01210,0.00556,0.0106,1.0000,0.9568 -0.750,-0.0690,0.01215,0.00550,0.0015,1.0000,0.9810 -0.500,0.0037,0.01193,0.00520,-0.0078,1.0000,1.0000 -0.250,0.0028,0.01167,0.00498,-0.0042,1.0000,1.0000 0.000,0.0000,0.01158,0.00490,0.0000,1.0000,1.0000 0.250,-0.0028,0.01167,0.00498,0.0042,1.0000,1.0000 0.500,-0.0037,0.01193,0.00520,0.0078,1.0000,1.0000 0.750,0.0690,0.01215,0.00550,-0.0015,0.9810,1.0000 1.000,0.1443,0.01210,0.00556,-0.0106,0.9567,1.0000 1.250,0.2109,0.01186,0.00543,-0.0175,0.9249,1.0000 1.500,0.2595,0.01165,0.00526,-0.0205,0.8814,1.0000 1.750,0.2883,0.01162,0.00517,-0.0195,0.8314,1.0000 2.000,0.3103,0.01171,0.00513,-0.0172,0.7818,1.0000 2.250,0.3301,0.01189,0.00514,-0.0147,0.7320,1.0000 2.500,0.3498,0.01212,0.00518,-0.0123,0.6822,1.0000 2.750,0.3700,0.01240,0.00527,-0.0101,0.6331,1.0000 3.000,0.3906,0.01272,0.00540,-0.0082,0.5822,1.0000 3.250,0.4114,0.01310,0.00554,-0.0063,0.5327,1.0000 3.500,0.4323,0.01352,0.00575,-0.0047,0.4810,1.0000 3.750,0.4533,0.01401,0.00601,-0.0031,0.4316,1.0000 4.000,0.4745,0.01455,0.00632,-0.0017,0.3827,1.0000 4.250,0.4960,0.01515,0.00671,-0.0004,0.3375,1.0000 4.500,0.5176,0.01583,0.00717,0.0008,0.2969,1.0000 4.750,0.5395,0.01655,0.00772,0.0020,0.2599,1.0000 5.000,0.5615,0.01738,0.00836,0.0030,0.2291,1.0000 5.250,0.5842,0.01826,0.00914,0.0041,0.2024,1.0000 5.500,0.6069,0.01917,0.00999,0.0050,0.1792,1.0000 5.750,0.6297,0.02013,0.01086,0.0059,0.1602,1.0000 6.000,0.6525,0.02121,0.01184,0.0068,0.1437,1.0000 6.250,0.6756,0.02240,0.01300,0.0076,0.1294,1.0000 6.500,0.6984,0.02348,0.01414,0.0085,0.1163,1.0000 6.750,0.7214,0.02487,0.01577,0.0095,0.1058,1.0000 7.000,0.7436,0.02649,0.01752,0.0104,0.0967,1.0000 7.250,0.7661,0.02805,0.01914,0.0112,0.0899,1.0000 7.500,0.7865,0.03059,0.02207,0.0124,0.0858,1.0000 7.750,0.8052,0.03308,0.02504,0.0137,0.0822,1.0000 8.000,0.8252,0.03490,0.02697,0.0145,0.0779,1.0000 8.250,0.8407,0.03815,0.03037,0.0153,0.0748,1.0000 8.500,0.8510,0.04161,0.03446,0.0168,0.0738,1.0000 8.750,0.8569,0.04586,0.03924,0.0181,0.0734,1.0000 9.000,0.8587,0.05055,0.04437,0.0191,0.0736,1.0000 9.250,0.8569,0.05562,0.04978,0.0198,0.0741,1.0000 9.500,0.8553,0.06097,0.05532,0.0200,0.0748,1.0000 9.750,0.6296,0.07871,0.07396,0.0047,0.0930,1.0000 10.000,0.6419,0.08048,0.07577,0.0061,0.0902,1.0000