Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n13-il-100000-n5 Airfoil,n13-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,37.1827 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-n13-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -14.000,-0.7458,0.10147,0.09602,-0.0276,1.0000,0.0267 -13.750,-0.8421,0.07702,0.07109,-0.0435,1.0000,0.0243 -13.500,-0.8700,0.06933,0.06313,-0.0477,1.0000,0.0241 -13.250,-0.8886,0.06384,0.05742,-0.0499,1.0000,0.0240 -13.000,-0.9008,0.05970,0.05313,-0.0509,1.0000,0.0243 -12.750,-0.9115,0.05603,0.04929,-0.0512,1.0000,0.0245 -12.500,-0.9194,0.05303,0.04615,-0.0509,1.0000,0.0250 -12.250,-0.9272,0.05003,0.04297,-0.0499,1.0000,0.0252 -12.000,-0.9322,0.04778,0.04057,-0.0485,1.0000,0.0261 -11.750,-0.9368,0.04556,0.03816,-0.0465,1.0000,0.0270 -11.500,-0.9399,0.04339,0.03576,-0.0441,1.0000,0.0278 -11.250,-0.9416,0.04125,0.03334,-0.0414,1.0000,0.0290 -11.000,-0.9408,0.03932,0.03118,-0.0385,1.0000,0.0302 -10.750,-0.9387,0.03790,0.02972,-0.0356,1.0000,0.0312 -10.500,-0.9359,0.03655,0.02829,-0.0325,1.0000,0.0325 -10.250,-0.9313,0.03515,0.02674,-0.0294,1.0000,0.0341 -10.000,-0.9237,0.03375,0.02509,-0.0265,1.0000,0.0367 -9.750,-0.9171,0.03238,0.02364,-0.0237,1.0000,0.0392 -9.500,-0.9091,0.03117,0.02235,-0.0210,1.0000,0.0426 -9.250,-0.8980,0.02995,0.02087,-0.0184,1.0000,0.0466 -9.000,-0.8917,0.02846,0.01943,-0.0153,1.0000,0.0506 -8.750,-0.8816,0.02739,0.01825,-0.0126,1.0000,0.0562 -8.500,-0.8720,0.02629,0.01712,-0.0098,1.0000,0.0612 -8.250,-0.8606,0.02546,0.01629,-0.0073,1.0000,0.0668 -8.000,-0.8479,0.02477,0.01561,-0.0049,1.0000,0.0728 -7.750,-0.8327,0.02432,0.01509,-0.0028,1.0000,0.0814 -7.500,-0.8173,0.02389,0.01457,-0.0007,1.0000,0.0906 -7.250,-0.8033,0.02330,0.01395,0.0016,1.0000,0.0985 -7.000,-0.7884,0.02267,0.01319,0.0039,1.0000,0.1067 -6.750,-0.7764,0.02189,0.01244,0.0066,1.0000,0.1141 -6.500,-0.7625,0.02127,0.01174,0.0090,1.0000,0.1231 -6.250,-0.7494,0.02064,0.01110,0.0116,1.0000,0.1334 -6.000,-0.7356,0.02008,0.01057,0.0139,1.0000,0.1447 -5.750,-0.7207,0.01960,0.01009,0.0162,1.0000,0.1566 -5.500,-0.7051,0.01916,0.00964,0.0183,1.0000,0.1690 -5.250,-0.6891,0.01874,0.00923,0.0203,1.0000,0.1839 -5.000,-0.6730,0.01832,0.00881,0.0224,1.0000,0.2011 -4.750,-0.6570,0.01789,0.00843,0.0244,1.0000,0.2221 -4.500,-0.6416,0.01741,0.00808,0.0265,1.0000,0.2501 -4.250,-0.6270,0.01689,0.00779,0.0286,1.0000,0.2921 -4.000,-0.6128,0.01639,0.00757,0.0309,1.0000,0.3527 -3.750,-0.5953,0.01602,0.00737,0.0327,0.9995,0.4058 -3.500,-0.5634,0.01576,0.00729,0.0315,0.9944,0.4572 -3.250,-0.5331,0.01548,0.00724,0.0308,0.9888,0.5136 -3.000,-0.5012,0.01534,0.00725,0.0299,0.9835,0.5648 -2.750,-0.4699,0.01522,0.00723,0.0292,0.9774,0.6079 -2.500,-0.4376,0.01513,0.00722,0.0283,0.9715,0.6451 -2.250,-0.4044,0.01505,0.00719,0.0272,0.9654,0.6784 -2.000,-0.3713,0.01499,0.00719,0.0263,0.9592,0.7094 -1.750,-0.3351,0.01495,0.00723,0.0248,0.9535,0.7410 -1.500,-0.2957,0.01498,0.00735,0.0227,0.9488,0.7738 -1.250,-0.2560,0.01507,0.00752,0.0207,0.9432,0.8036 -1.000,-0.2104,0.01522,0.00770,0.0174,0.9392,0.8278 -0.750,-0.1642,0.01534,0.00783,0.0139,0.9333,0.8458 -0.500,-0.1139,0.01540,0.00790,0.0098,0.9263,0.8619 -0.250,-0.0633,0.01541,0.00790,0.0056,0.9184,0.8763 0.000,-0.0133,0.01540,0.00788,0.0015,0.9113,0.8884 0.250,0.0308,0.01542,0.00791,-0.0016,0.9031,0.9003 0.500,0.0837,0.01540,0.00791,-0.0065,0.8964,0.9060 0.750,0.1240,0.01538,0.00791,-0.0088,0.8849,0.9159 1.000,0.1719,0.01535,0.00791,-0.0127,0.8730,0.9214 1.250,0.2104,0.01532,0.00792,-0.0145,0.8566,0.9314 1.500,0.2567,0.01524,0.00789,-0.0179,0.8361,0.9377 1.750,0.2922,0.01519,0.00787,-0.0191,0.8083,0.9478 2.000,0.3363,0.01504,0.00773,-0.0220,0.7763,0.9539 2.250,0.3772,0.01493,0.00757,-0.0242,0.7439,0.9605 2.500,0.4223,0.01487,0.00741,-0.0273,0.7087,0.9642 2.750,0.4600,0.01495,0.00739,-0.0291,0.6703,0.9703 3.000,0.4943,0.01508,0.00742,-0.0303,0.6184,0.9766 3.250,0.5253,0.01529,0.00742,-0.0309,0.5491,0.9840 3.500,0.5569,0.01562,0.00735,-0.0317,0.4631,0.9901 3.750,0.5880,0.01607,0.00747,-0.0328,0.3986,0.9967 4.000,0.6123,0.01649,0.00767,-0.0325,0.3482,1.0000 4.250,0.6269,0.01686,0.00790,-0.0302,0.3080,1.0000 4.500,0.6411,0.01728,0.00818,-0.0279,0.2690,1.0000 4.750,0.6556,0.01773,0.00848,-0.0256,0.2334,1.0000 5.000,0.6702,0.01822,0.00883,-0.0233,0.2034,1.0000 5.250,0.6847,0.01874,0.00924,-0.0210,0.1777,1.0000 5.500,0.6995,0.01927,0.00969,-0.0187,0.1555,1.0000 5.750,0.7141,0.01983,0.01022,-0.0164,0.1390,1.0000 6.000,0.7288,0.02041,0.01077,-0.0141,0.1259,1.0000 6.250,0.7433,0.02101,0.01136,-0.0117,0.1152,1.0000 6.750,0.7718,0.02229,0.01266,-0.0070,0.0998,1.0000 7.000,0.7854,0.02300,0.01340,-0.0045,0.0947,1.0000 7.250,0.7996,0.02378,0.01423,-0.0021,0.0898,1.0000 7.500,0.8143,0.02449,0.01501,0.0002,0.0843,1.0000 7.750,0.8270,0.02538,0.01586,0.0026,0.0798,1.0000 8.000,0.8427,0.02621,0.01685,0.0047,0.0757,1.0000 8.250,0.8570,0.02700,0.01774,0.0069,0.0709,1.0000 8.500,0.8690,0.02796,0.01864,0.0093,0.0666,1.0000 8.750,0.8833,0.02885,0.01979,0.0115,0.0623,1.0000 9.000,0.8954,0.02969,0.02075,0.0139,0.0579,1.0000 9.250,0.9059,0.03070,0.02174,0.0164,0.0546,1.0000 9.500,0.9173,0.03186,0.02315,0.0190,0.0508,1.0000 9.750,0.9272,0.03296,0.02442,0.0216,0.0474,1.0000 10.000,0.9351,0.03395,0.02544,0.0244,0.0447,1.0000 10.250,0.9420,0.03537,0.02695,0.0271,0.0424,1.0000 10.500,0.9470,0.03684,0.02873,0.0303,0.0397,1.0000 10.750,0.9487,0.03819,0.03027,0.0338,0.0376,1.0000 11.000,0.9497,0.03943,0.03160,0.0373,0.0361,1.0000 11.250,0.9506,0.04068,0.03286,0.0403,0.0348,1.0000 11.500,0.9476,0.04266,0.03505,0.0436,0.0336,1.0000 11.750,0.9404,0.04501,0.03773,0.0467,0.0324,1.0000 12.000,0.9320,0.04738,0.04036,0.0493,0.0312,1.0000 12.250,0.9226,0.04994,0.04314,0.0514,0.0302,1.0000 12.500,0.9119,0.05282,0.04621,0.0528,0.0296,1.0000 12.750,0.8984,0.05629,0.04989,0.0534,0.0293,1.0000 13.000,0.8832,0.06023,0.05400,0.0530,0.0289,1.0000 13.250,0.8603,0.06575,0.05976,0.0513,0.0290,1.0000 13.500,0.8347,0.07233,0.06655,0.0479,0.0289,1.0000 13.750,0.7768,0.08659,0.08113,0.0384,0.0303,1.0000 14.000,0.6990,0.10907,0.10366,0.0250,0.0329,1.0000