Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-s9032-il-100000-n5 Airfoil,s9032-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,34.2125 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-s9032-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.500,-0.8009,0.08345,0.07836,-0.0040,1.0000,0.0359 -11.250,-0.8901,0.06185,0.05644,-0.0222,1.0000,0.0324 -11.000,-0.9174,0.05612,0.05047,-0.0249,1.0000,0.0323 -10.750,-0.9352,0.05238,0.04650,-0.0243,1.0000,0.0324 -10.500,-0.9415,0.04956,0.04348,-0.0232,1.0000,0.0332 -10.250,-0.9432,0.04669,0.04033,-0.0221,1.0000,0.0342 -10.000,-0.9418,0.04367,0.03698,-0.0210,1.0000,0.0353 -9.750,-0.9368,0.04060,0.03352,-0.0197,1.0000,0.0364 -9.500,-0.9277,0.03769,0.03018,-0.0185,1.0000,0.0374 -9.250,-0.9148,0.03514,0.02721,-0.0173,1.0000,0.0386 -9.000,-0.8991,0.03284,0.02459,-0.0162,1.0000,0.0397 -8.750,-0.8820,0.03109,0.02278,-0.0153,1.0000,0.0416 -8.500,-0.8631,0.02983,0.02138,-0.0145,1.0000,0.0443 -8.250,-0.8433,0.02838,0.01971,-0.0136,1.0000,0.0473 -8.000,-0.8226,0.02689,0.01792,-0.0126,1.0000,0.0500 -7.750,-0.8031,0.02539,0.01640,-0.0116,1.0000,0.0529 -7.500,-0.7822,0.02428,0.01522,-0.0107,1.0000,0.0569 -7.250,-0.7602,0.02329,0.01404,-0.0098,1.0000,0.0627 -7.000,-0.7394,0.02229,0.01304,-0.0090,1.0000,0.0690 -6.750,-0.7172,0.02137,0.01200,-0.0081,1.0000,0.0762 -6.500,-0.6951,0.02058,0.01119,-0.0073,1.0000,0.0854 -6.250,-0.6730,0.01977,0.01038,-0.0065,1.0000,0.0950 -6.000,-0.6504,0.01904,0.00964,-0.0056,1.0000,0.1069 -5.750,-0.6278,0.01835,0.00893,-0.0048,1.0000,0.1203 -5.500,-0.6049,0.01771,0.00831,-0.0040,1.0000,0.1361 -5.250,-0.5819,0.01710,0.00772,-0.0032,1.0000,0.1537 -5.000,-0.5588,0.01653,0.00718,-0.0024,1.0000,0.1724 -4.750,-0.5359,0.01598,0.00671,-0.0016,1.0000,0.1953 -4.500,-0.5129,0.01547,0.00627,-0.0008,1.0000,0.2213 -4.250,-0.4899,0.01499,0.00589,0.0001,1.0000,0.2503 -4.000,-0.4669,0.01455,0.00556,0.0010,1.0000,0.2824 -3.750,-0.4442,0.01412,0.00527,0.0019,1.0000,0.3182 -3.500,-0.4215,0.01372,0.00499,0.0029,1.0000,0.3556 -3.250,-0.3990,0.01334,0.00477,0.0039,1.0000,0.3935 -3.000,-0.3764,0.01301,0.00457,0.0050,1.0000,0.4325 -2.750,-0.3540,0.01269,0.00441,0.0061,1.0000,0.4726 -2.500,-0.3317,0.01240,0.00428,0.0074,1.0000,0.5144 -2.250,-0.3096,0.01213,0.00419,0.0086,1.0000,0.5580 -2.000,-0.2877,0.01190,0.00414,0.0100,1.0000,0.6020 -1.750,-0.2656,0.01170,0.00411,0.0114,1.0000,0.6450 -1.500,-0.2437,0.01154,0.00409,0.0128,1.0000,0.6865 -1.250,-0.2222,0.01141,0.00412,0.0143,1.0000,0.7283 -1.000,-0.1934,0.01133,0.00420,0.0144,0.9950,0.7732 -0.750,-0.1504,0.01131,0.00431,0.0118,0.9812,0.8221 -0.500,-0.1042,0.01131,0.00441,0.0087,0.9664,0.8660 -0.250,-0.0535,0.01133,0.00447,0.0047,0.9491,0.9010 0.000,0.0000,0.01133,0.00449,0.0000,0.9280,0.9280 0.250,0.0535,0.01133,0.00447,-0.0047,0.9010,0.9491 0.500,0.1042,0.01131,0.00441,-0.0087,0.8661,0.9663 0.750,0.1504,0.01131,0.00431,-0.0119,0.8223,0.9811 1.000,0.1934,0.01133,0.00420,-0.0144,0.7733,0.9949 1.250,0.2224,0.01141,0.00412,-0.0143,0.7280,1.0000 1.500,0.2439,0.01154,0.00409,-0.0128,0.6863,1.0000 1.750,0.2659,0.01170,0.00411,-0.0114,0.6449,1.0000 2.000,0.2879,0.01190,0.00414,-0.0101,0.6018,1.0000 2.250,0.3099,0.01213,0.00419,-0.0087,0.5580,1.0000 2.500,0.3320,0.01240,0.00428,-0.0074,0.5143,1.0000 2.750,0.3543,0.01269,0.00441,-0.0062,0.4723,1.0000 3.000,0.3768,0.01301,0.00457,-0.0051,0.4324,1.0000 3.250,0.3994,0.01334,0.00477,-0.0040,0.3935,1.0000 3.500,0.4219,0.01372,0.00499,-0.0030,0.3555,1.0000 3.750,0.4446,0.01412,0.00527,-0.0020,0.3180,1.0000 4.000,0.4673,0.01455,0.00556,-0.0010,0.2823,1.0000 4.250,0.4902,0.01500,0.00589,-0.0001,0.2500,1.0000 4.500,0.5132,0.01547,0.00627,0.0007,0.2212,1.0000 4.750,0.5361,0.01598,0.00672,0.0015,0.1953,1.0000 5.000,0.5590,0.01653,0.00718,0.0024,0.1722,1.0000 5.250,0.5821,0.01710,0.00772,0.0032,0.1536,1.0000 5.500,0.6051,0.01771,0.00831,0.0040,0.1361,1.0000 5.750,0.6278,0.01835,0.00893,0.0048,0.1202,1.0000 6.000,0.6505,0.01904,0.00964,0.0056,0.1069,1.0000 6.250,0.6730,0.01977,0.01038,0.0065,0.0950,1.0000 6.500,0.6951,0.02057,0.01118,0.0073,0.0853,1.0000 6.750,0.7171,0.02136,0.01200,0.0081,0.0761,1.0000 7.000,0.7392,0.02229,0.01304,0.0090,0.0690,1.0000 7.250,0.7600,0.02328,0.01403,0.0099,0.0627,1.0000 7.500,0.7819,0.02427,0.01521,0.0108,0.0569,1.0000 7.750,0.8028,0.02538,0.01640,0.0117,0.0529,1.0000 8.000,0.8222,0.02688,0.01791,0.0126,0.0500,1.0000 8.250,0.8429,0.02838,0.01970,0.0137,0.0473,1.0000 8.500,0.8626,0.02981,0.02136,0.0146,0.0443,1.0000 8.750,0.8815,0.03106,0.02275,0.0154,0.0416,1.0000 9.000,0.8986,0.03281,0.02457,0.0163,0.0398,1.0000 9.250,0.9141,0.03511,0.02718,0.0174,0.0385,1.0000 9.500,0.9271,0.03765,0.03014,0.0186,0.0374,1.0000 9.750,0.9362,0.04055,0.03346,0.0199,0.0364,1.0000 10.000,0.9411,0.04362,0.03692,0.0211,0.0354,1.0000 10.250,0.9424,0.04667,0.04032,0.0223,0.0343,1.0000 10.500,0.9406,0.04954,0.04346,0.0234,0.0332,1.0000 10.750,0.9332,0.05248,0.04661,0.0245,0.0325,1.0000 11.000,0.9169,0.05603,0.05037,0.0251,0.0323,1.0000 11.250,0.8884,0.06197,0.05656,0.0222,0.0325,1.0000 11.500,0.8011,0.08325,0.07816,0.0043,0.0359,1.0000