Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-e171-il-200000-n5 Airfoil,e171-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,47.8106 Max Cl/Cd alpha,5 Url,http://www.airfoiltools.com/polar/csv?polar=xf-e171-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -14.000,-0.8164,0.09117,0.08733,-0.0142,1.0000,0.0088 -13.750,-0.8477,0.08043,0.07634,-0.0210,1.0000,0.0086 -13.500,-0.8678,0.07315,0.06889,-0.0254,1.0000,0.0086 -13.250,-0.8865,0.06674,0.06226,-0.0289,1.0000,0.0086 -13.000,-0.9007,0.06153,0.05686,-0.0314,1.0000,0.0087 -12.750,-0.9145,0.05667,0.05179,-0.0333,1.0000,0.0087 -12.500,-0.9247,0.05259,0.04751,-0.0344,1.0000,0.0087 -12.250,-0.9329,0.04899,0.04371,-0.0349,1.0000,0.0088 -12.000,-0.9388,0.04584,0.04038,-0.0350,1.0000,0.0090 -11.750,-0.9421,0.04307,0.03742,-0.0345,1.0000,0.0091 -11.500,-0.9440,0.04058,0.03475,-0.0337,1.0000,0.0094 -11.250,-0.9438,0.03820,0.03215,-0.0326,1.0000,0.0094 -11.000,-0.9416,0.03615,0.02988,-0.0311,1.0000,0.0098 -10.750,-0.9375,0.03423,0.02778,-0.0294,1.0000,0.0101 -10.500,-0.9315,0.03249,0.02585,-0.0276,1.0000,0.0104 -10.250,-0.9242,0.03084,0.02403,-0.0256,1.0000,0.0108 -10.000,-0.9154,0.02945,0.02247,-0.0235,1.0000,0.0115 -9.750,-0.9031,0.02858,0.02141,-0.0216,1.0000,0.0123 -9.500,-0.8956,0.02684,0.01960,-0.0194,1.0000,0.0131 -9.250,-0.8837,0.02569,0.01841,-0.0177,1.0000,0.0141 -9.000,-0.8706,0.02455,0.01718,-0.0159,1.0000,0.0149 -8.750,-0.8569,0.02345,0.01597,-0.0141,1.0000,0.0160 -8.500,-0.8424,0.02243,0.01483,-0.0123,1.0000,0.0172 -8.250,-0.8295,0.02130,0.01358,-0.0103,1.0000,0.0186 -8.000,-0.8141,0.02042,0.01268,-0.0088,1.0000,0.0211 -7.750,-0.7964,0.01974,0.01192,-0.0073,1.0000,0.0241 -7.500,-0.7810,0.01885,0.01097,-0.0055,1.0000,0.0270 -7.250,-0.7640,0.01814,0.01024,-0.0040,1.0000,0.0316 -7.000,-0.7465,0.01747,0.00951,-0.0023,1.0000,0.0365 -6.750,-0.7298,0.01676,0.00881,-0.0006,1.0000,0.0438 -6.500,-0.7130,0.01609,0.00815,0.0011,1.0000,0.0562 -6.250,-0.6964,0.01542,0.00758,0.0028,1.0000,0.0747 -6.000,-0.6741,0.01478,0.00703,0.0032,0.9965,0.0992 -5.750,-0.6410,0.01406,0.00645,0.0014,0.9837,0.1358 -5.500,-0.6101,0.01326,0.00589,-0.0001,0.9673,0.1889 -5.250,-0.5809,0.01232,0.00534,-0.0013,0.9477,0.2695 -5.000,-0.5502,0.01152,0.00487,-0.0026,0.9290,0.3526 -4.750,-0.5181,0.01106,0.00460,-0.0037,0.9105,0.4157 -4.500,-0.4873,0.01081,0.00441,-0.0044,0.8915,0.4607 -4.250,-0.4582,0.01067,0.00427,-0.0046,0.8729,0.4960 -4.000,-0.4302,0.01060,0.00414,-0.0044,0.8556,0.5201 -3.750,-0.4032,0.01055,0.00399,-0.0041,0.8393,0.5389 -3.500,-0.3767,0.01053,0.00387,-0.0037,0.8243,0.5553 -3.250,-0.3502,0.01050,0.00376,-0.0033,0.8106,0.5697 -3.000,-0.3238,0.01049,0.00367,-0.0029,0.7981,0.5822 -2.750,-0.2973,0.01047,0.00356,-0.0025,0.7862,0.5940 -2.500,-0.2707,0.01045,0.00348,-0.0021,0.7749,0.6051 -2.250,-0.2440,0.01044,0.00340,-0.0018,0.7646,0.6157 -2.000,-0.2172,0.01043,0.00331,-0.0015,0.7551,0.6253 -1.750,-0.1903,0.01041,0.00326,-0.0012,0.7455,0.6341 -1.500,-0.1633,0.01040,0.00319,-0.0010,0.7366,0.6435 -1.250,-0.1363,0.01039,0.00315,-0.0008,0.7285,0.6520 -1.000,-0.1091,0.01037,0.00311,-0.0006,0.7198,0.6600 -0.750,-0.0820,0.01037,0.00307,-0.0004,0.7125,0.6679 -0.500,-0.0546,0.01036,0.00305,-0.0003,0.7042,0.6749 -0.250,-0.0273,0.01036,0.00303,-0.0001,0.6973,0.6825 0.000,0.0000,0.01035,0.00303,0.0000,0.6894,0.6894 0.250,0.0273,0.01036,0.00303,0.0001,0.6825,0.6972 0.500,0.0546,0.01036,0.00305,0.0003,0.6749,0.7042 0.750,0.0819,0.01037,0.00307,0.0004,0.6679,0.7125 1.000,0.1091,0.01037,0.00311,0.0006,0.6600,0.7198 1.250,0.1363,0.01039,0.00315,0.0008,0.6520,0.7285 1.500,0.1633,0.01040,0.00319,0.0010,0.6435,0.7366 1.750,0.1903,0.01041,0.00326,0.0012,0.6341,0.7454 2.000,0.2172,0.01043,0.00332,0.0015,0.6253,0.7551 2.250,0.2440,0.01044,0.00340,0.0018,0.6157,0.7646 2.500,0.2708,0.01045,0.00348,0.0021,0.6052,0.7749 2.750,0.2973,0.01047,0.00356,0.0025,0.5940,0.7862 3.000,0.3238,0.01049,0.00367,0.0029,0.5824,0.7981 3.250,0.3502,0.01050,0.00376,0.0033,0.5697,0.8106 3.500,0.3767,0.01053,0.00387,0.0037,0.5554,0.8243 3.750,0.4033,0.01055,0.00399,0.0041,0.5389,0.8393 4.000,0.4302,0.01060,0.00414,0.0044,0.5199,0.8556 4.250,0.4582,0.01067,0.00427,0.0046,0.4959,0.8729 4.500,0.4873,0.01081,0.00441,0.0044,0.4607,0.8914 4.750,0.5181,0.01106,0.00460,0.0037,0.4155,0.9106 5.000,0.5503,0.01151,0.00487,0.0026,0.3534,0.9291 5.250,0.5809,0.01232,0.00534,0.0013,0.2694,0.9479 5.500,0.6101,0.01326,0.00589,0.0001,0.1892,0.9675 5.750,0.6411,0.01406,0.00645,-0.0014,0.1358,0.9839 6.000,0.6743,0.01478,0.00703,-0.0033,0.0993,0.9967 6.250,0.6961,0.01543,0.00758,-0.0027,0.0744,1.0000 6.500,0.7128,0.01609,0.00815,-0.0010,0.0566,1.0000 6.750,0.7297,0.01676,0.00880,0.0006,0.0439,1.0000 7.000,0.7465,0.01747,0.00951,0.0024,0.0365,1.0000 7.250,0.7640,0.01813,0.01024,0.0040,0.0315,1.0000 7.500,0.7811,0.01885,0.01097,0.0055,0.0269,1.0000 7.750,0.7966,0.01973,0.01191,0.0073,0.0240,1.0000 8.000,0.8143,0.02042,0.01268,0.0087,0.0212,1.0000 8.250,0.8300,0.02128,0.01356,0.0103,0.0186,1.0000 8.500,0.8428,0.02243,0.01483,0.0123,0.0172,1.0000 8.750,0.8573,0.02345,0.01598,0.0140,0.0160,1.0000 9.000,0.8711,0.02455,0.01718,0.0158,0.0148,1.0000 9.250,0.8842,0.02570,0.01841,0.0176,0.0140,1.0000 9.500,0.8963,0.02685,0.01963,0.0193,0.0131,1.0000 9.750,0.9040,0.02855,0.02139,0.0215,0.0123,1.0000 10.000,0.9153,0.02970,0.02270,0.0234,0.0118,1.0000 10.250,0.9251,0.03085,0.02404,0.0254,0.0108,1.0000 10.500,0.9324,0.03249,0.02586,0.0274,0.0104,1.0000 10.750,0.9384,0.03429,0.02784,0.0293,0.0101,1.0000 11.000,0.9425,0.03618,0.02992,0.0309,0.0097,1.0000 11.250,0.9445,0.03829,0.03226,0.0324,0.0095,1.0000 11.500,0.9450,0.04053,0.03468,0.0336,0.0092,1.0000 11.750,0.9433,0.04311,0.03747,0.0344,0.0091,1.0000 12.000,0.9393,0.04590,0.04044,0.0348,0.0089,1.0000 12.250,0.9341,0.04897,0.04368,0.0347,0.0088,1.0000 12.500,0.9265,0.05248,0.04738,0.0341,0.0086,1.0000 12.750,0.9145,0.05689,0.05203,0.0330,0.0087,1.0000 13.000,0.9028,0.06143,0.05676,0.0312,0.0087,1.0000 13.250,0.8877,0.06677,0.06228,0.0287,0.0086,1.0000 13.500,0.8686,0.07330,0.06903,0.0251,0.0086,1.0000 13.750,0.8432,0.08171,0.07769,0.0200,0.0088,1.0000 14.000,0.8111,0.09285,0.08906,0.0129,0.0090,1.0000