Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-v23010-il-100000-n5 Airfoil,v23010-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,41.2066 Max Cl/Cd alpha,9.5 Url,http://airfoiltools.com/polar/csv?polar=xf-v23010-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.5080,0.09222,0.08696,-0.0115,1.0000,0.0687 -8.750,-0.5156,0.08736,0.08215,-0.0158,1.0000,0.0702 -8.500,-0.5388,0.08168,0.07649,-0.0224,1.0000,0.0713 -8.250,-0.5728,0.07827,0.07284,-0.0250,1.0000,0.0723 -8.000,-0.5858,0.07562,0.06989,-0.0251,1.0000,0.0727 -7.750,-0.5704,0.06959,0.06407,-0.0253,1.0000,0.0736 -7.500,-0.5569,0.06601,0.06058,-0.0248,1.0000,0.0748 -7.250,-0.5472,0.06311,0.05769,-0.0242,1.0000,0.0766 -7.000,-0.5404,0.06029,0.05481,-0.0236,1.0000,0.0794 -6.750,-0.5483,0.05786,0.05183,-0.0228,1.0000,0.0867 -6.250,-0.5234,0.04763,0.04074,-0.0196,1.0000,0.0525 -6.000,-0.5070,0.04476,0.03798,-0.0187,1.0000,0.0497 -5.500,-0.4815,0.03906,0.03134,-0.0142,1.0000,0.0439 -5.250,-0.4657,0.03687,0.02905,-0.0128,1.0000,0.0435 -5.000,-0.4497,0.03488,0.02689,-0.0111,1.0000,0.0431 -4.750,-0.4334,0.03318,0.02490,-0.0092,1.0000,0.0435 -4.500,-0.4169,0.03170,0.02311,-0.0072,1.0000,0.0439 -4.250,-0.4001,0.03034,0.02147,-0.0052,1.0000,0.0441 -4.000,-0.3828,0.02885,0.01985,-0.0035,1.0000,0.0440 -3.750,-0.3654,0.02752,0.01840,-0.0019,1.0000,0.0438 -3.500,-0.3283,0.02592,0.01662,-0.0038,0.9920,0.0437 -3.250,-0.2858,0.02442,0.01492,-0.0067,0.9809,0.0437 -3.000,-0.2403,0.02301,0.01334,-0.0098,0.9659,0.0439 -2.750,-0.1942,0.02173,0.01194,-0.0129,0.9479,0.0442 -2.500,-0.1536,0.02043,0.01072,-0.0152,0.9278,0.0455 -2.250,-0.1186,0.01956,0.00990,-0.0164,0.9065,0.0474 -2.000,-0.0836,0.01875,0.00907,-0.0174,0.8869,0.0490 -1.750,-0.0505,0.01798,0.00830,-0.0179,0.8670,0.0500 -1.500,-0.0210,0.01736,0.00765,-0.0177,0.8449,0.0511 -1.250,0.0054,0.01685,0.00708,-0.0170,0.8190,0.0522 -1.000,0.0307,0.01633,0.00651,-0.0161,0.7920,0.0540 -0.750,0.0569,0.01598,0.00603,-0.0152,0.7661,0.0572 -0.500,0.0831,0.01575,0.00563,-0.0144,0.7403,0.0618 -0.250,0.1085,0.01546,0.00525,-0.0135,0.7138,0.0676 0.000,0.1338,0.01523,0.00491,-0.0125,0.6839,0.0769 0.250,0.1505,0.01327,0.00459,-0.0108,0.6525,0.5259 0.500,0.1796,0.01251,0.00492,-0.0085,0.6109,0.8679 0.750,0.2754,0.01305,0.00502,-0.0199,0.5331,0.9829 1.000,0.3195,0.01326,0.00484,-0.0233,0.4781,0.9964 1.250,0.3454,0.01348,0.00476,-0.0231,0.4395,1.0000 1.500,0.3649,0.01371,0.00474,-0.0217,0.4115,1.0000 1.750,0.3849,0.01396,0.00477,-0.0204,0.3893,1.0000 2.000,0.4055,0.01422,0.00485,-0.0191,0.3720,1.0000 2.250,0.4268,0.01447,0.00496,-0.0179,0.3585,1.0000 2.500,0.4484,0.01475,0.00511,-0.0168,0.3477,1.0000 2.750,0.4703,0.01503,0.00528,-0.0157,0.3375,1.0000 3.000,0.4926,0.01531,0.00546,-0.0146,0.3274,1.0000 3.250,0.5147,0.01562,0.00564,-0.0136,0.3178,1.0000 3.500,0.5375,0.01589,0.00587,-0.0126,0.3077,1.0000 3.750,0.5601,0.01621,0.00609,-0.0117,0.2989,1.0000 4.000,0.5830,0.01651,0.00635,-0.0107,0.2907,1.0000 4.250,0.6059,0.01687,0.00663,-0.0098,0.2842,1.0000 4.500,0.6293,0.01719,0.00697,-0.0090,0.2771,1.0000 4.750,0.6523,0.01758,0.00728,-0.0081,0.2710,1.0000 5.000,0.6759,0.01795,0.00767,-0.0073,0.2649,1.0000 5.250,0.6994,0.01833,0.00808,-0.0065,0.2589,1.0000 5.500,0.7227,0.01878,0.00846,-0.0057,0.2536,1.0000 5.750,0.7464,0.01918,0.00895,-0.0050,0.2472,1.0000 6.000,0.7698,0.01959,0.00940,-0.0042,0.2407,1.0000 6.250,0.7931,0.02007,0.00985,-0.0034,0.2349,1.0000 6.500,0.8165,0.02049,0.01041,-0.0027,0.2279,1.0000 6.750,0.8397,0.02096,0.01089,-0.0019,0.2221,1.0000 7.000,0.8630,0.02148,0.01150,-0.0012,0.2165,1.0000 7.250,0.8860,0.02200,0.01213,-0.0005,0.2102,1.0000 7.500,0.9090,0.02249,0.01261,0.0003,0.2050,1.0000 7.750,0.9315,0.02306,0.01337,0.0010,0.1987,1.0000 8.000,0.9540,0.02360,0.01400,0.0018,0.1929,1.0000 8.250,0.9766,0.02414,0.01453,0.0026,0.1887,1.0000 8.500,0.9982,0.02479,0.01544,0.0034,0.1822,1.0000 8.750,1.0195,0.02513,0.01583,0.0043,0.1757,1.0000 9.000,1.0397,0.02552,0.01638,0.0053,0.1672,1.0000 9.250,1.0595,0.02572,0.01659,0.0063,0.1592,1.0000 9.500,1.0792,0.02619,0.01726,0.0073,0.1505,1.0000 9.750,1.0982,0.02672,0.01786,0.0084,0.1439,1.0000 10.000,1.1168,0.02734,0.01862,0.0094,0.1367,1.0000 10.250,1.1340,0.02802,0.01940,0.0106,0.1301,1.0000 10.500,1.1501,0.02877,0.02027,0.0118,0.1227,1.0000 10.750,1.1647,0.02967,0.02128,0.0132,0.1154,1.0000 11.000,1.1768,0.03062,0.02230,0.0147,0.1079,1.0000 11.250,1.1882,0.03174,0.02363,0.0162,0.0994,1.0000 11.500,1.1957,0.03297,0.02495,0.0181,0.0918,1.0000 11.750,1.2002,0.03430,0.02642,0.0202,0.0843,1.0000 12.000,1.2011,0.03584,0.02808,0.0225,0.0780,1.0000 12.250,1.1987,0.03764,0.02995,0.0244,0.0733,1.0000 12.500,1.1947,0.03985,0.03227,0.0257,0.0692,1.0000 12.750,1.1882,0.04253,0.03507,0.0263,0.0659,1.0000 13.000,1.1783,0.04587,0.03849,0.0260,0.0637,1.0000 13.250,1.1668,0.04985,0.04257,0.0248,0.0619,1.0000 13.500,1.1544,0.05445,0.04734,0.0229,0.0602,1.0000 13.750,1.1397,0.05978,0.05283,0.0203,0.0589,1.0000 14.000,1.1233,0.06574,0.05893,0.0170,0.0578,1.0000 14.250,1.1061,0.07208,0.06540,0.0136,0.0568,1.0000 14.500,1.0905,0.07826,0.07166,0.0103,0.0559,1.0000 14.750,1.0774,0.08399,0.07743,0.0074,0.0548,1.0000 15.000,1.0651,0.08965,0.08314,0.0046,0.0536,1.0000 15.250,1.0487,0.09643,0.09009,0.0011,0.0526,1.0000 15.500,1.0302,0.10387,0.09767,-0.0028,0.0515,1.0000 15.750,1.0109,0.11174,0.10569,-0.0069,0.0507,1.0000 16.000,0.9854,0.12133,0.11542,-0.0121,0.0499,1.0000