Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ames01-il-200000-n5 Airfoil,ames01-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,55.3197 Max Cl/Cd alpha,8.75 Url,http://airfoiltools.com/polar/csv?polar=xf-ames01-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.7277,0.06507,0.06155,-0.0217,1.0000,0.0207 -9.500,-0.7634,0.05562,0.05177,-0.0234,1.0000,0.0207 -9.250,-0.8094,0.04179,0.03688,-0.0222,1.0000,0.0213 -9.000,-0.7946,0.04004,0.03502,-0.0219,1.0000,0.0218 -8.750,-0.7755,0.03898,0.03386,-0.0217,1.0000,0.0224 -8.500,-0.7595,0.03688,0.03152,-0.0212,1.0000,0.0230 -8.250,-0.7419,0.03493,0.02934,-0.0208,1.0000,0.0238 -8.000,-0.7262,0.03211,0.02612,-0.0199,1.0000,0.0250 -7.750,-0.7108,0.02896,0.02242,-0.0187,1.0000,0.0261 -7.500,-0.6902,0.02653,0.01949,-0.0180,0.9942,0.0270 -7.250,-0.6636,0.02489,0.01769,-0.0185,0.9876,0.0278 -7.000,-0.6345,0.02403,0.01674,-0.0193,0.9828,0.0288 -6.750,-0.6060,0.02327,0.01586,-0.0199,0.9780,0.0301 -6.500,-0.5769,0.02226,0.01465,-0.0204,0.9739,0.0318 -6.250,-0.5490,0.02114,0.01330,-0.0205,0.9693,0.0332 -6.000,-0.5213,0.02020,0.01217,-0.0206,0.9646,0.0343 -5.750,-0.4944,0.01925,0.01120,-0.0207,0.9605,0.0359 -5.500,-0.4678,0.01880,0.01073,-0.0206,0.9557,0.0378 -5.250,-0.4412,0.01826,0.01012,-0.0204,0.9510,0.0398 -5.000,-0.4149,0.01767,0.00942,-0.0200,0.9468,0.0417 -4.750,-0.3886,0.01723,0.00889,-0.0197,0.9422,0.0434 -4.500,-0.3641,0.01650,0.00820,-0.0191,0.9373,0.0461 -4.250,-0.3389,0.01609,0.00779,-0.0186,0.9331,0.0486 -4.000,-0.3132,0.01567,0.00732,-0.0181,0.9284,0.0512 -3.750,-0.2875,0.01534,0.00693,-0.0176,0.9234,0.0539 -3.500,-0.2642,0.01489,0.00649,-0.0166,0.9182,0.0574 -3.250,-0.2397,0.01455,0.00615,-0.0158,0.9104,0.0612 -3.000,-0.2174,0.01428,0.00583,-0.0143,0.9029,0.0650 -2.750,-0.1932,0.01395,0.00548,-0.0133,0.8930,0.0700 -2.500,-0.1697,0.01363,0.00517,-0.0121,0.8846,0.0767 -2.250,-0.1454,0.01335,0.00485,-0.0111,0.8757,0.0844 -2.000,-0.1204,0.01300,0.00457,-0.0103,0.8668,0.1006 -1.750,-0.0974,0.01244,0.00427,-0.0092,0.8586,0.1605 -1.500,-0.0762,0.01133,0.00399,-0.0083,0.8479,0.3660 -1.250,-0.0569,0.01038,0.00380,-0.0064,0.8368,0.5605 -1.000,-0.0383,0.00967,0.00373,-0.0038,0.8247,0.7198 -0.750,-0.0143,0.00932,0.00378,-0.0017,0.8127,0.8419 -0.500,0.0260,0.00936,0.00391,-0.0032,0.8007,0.9174 -0.250,0.0663,0.00947,0.00397,-0.0050,0.7866,0.9550 0.000,0.1129,0.00958,0.00398,-0.0084,0.7677,0.9769 0.250,0.1538,0.00961,0.00389,-0.0109,0.7431,0.9876 0.500,0.1909,0.00963,0.00374,-0.0126,0.7095,0.9949 0.750,0.2269,0.00970,0.00353,-0.0141,0.6532,1.0000 1.000,0.2514,0.00992,0.00333,-0.0133,0.5735,1.0000 1.250,0.2769,0.01035,0.00326,-0.0131,0.4788,1.0000 1.500,0.3025,0.01082,0.00330,-0.0131,0.3997,1.0000 1.750,0.3280,0.01118,0.00336,-0.0129,0.3521,1.0000 2.000,0.3534,0.01146,0.00345,-0.0127,0.3242,1.0000 2.250,0.3787,0.01168,0.00354,-0.0124,0.3060,1.0000 2.500,0.4040,0.01190,0.00365,-0.0121,0.2923,1.0000 2.750,0.4292,0.01211,0.00377,-0.0117,0.2806,1.0000 3.000,0.4544,0.01231,0.00391,-0.0113,0.2711,1.0000 3.500,0.5048,0.01274,0.00424,-0.0105,0.2566,1.0000 3.750,0.5298,0.01298,0.00442,-0.0100,0.2504,1.0000 4.000,0.5549,0.01322,0.00462,-0.0096,0.2446,1.0000 4.250,0.5802,0.01344,0.00484,-0.0092,0.2386,1.0000 4.500,0.6050,0.01372,0.00507,-0.0087,0.2335,1.0000 4.750,0.6302,0.01397,0.00533,-0.0083,0.2291,1.0000 5.000,0.6554,0.01421,0.00559,-0.0078,0.2240,1.0000 5.250,0.6803,0.01451,0.00586,-0.0074,0.2191,1.0000 5.500,0.7053,0.01481,0.00616,-0.0070,0.2148,1.0000 5.750,0.7306,0.01506,0.00647,-0.0066,0.2099,1.0000 6.000,0.7556,0.01535,0.00677,-0.0062,0.2050,1.0000 6.250,0.7805,0.01569,0.00710,-0.0058,0.2003,1.0000 6.500,0.8060,0.01593,0.00743,-0.0054,0.1948,1.0000 6.750,0.8311,0.01622,0.00775,-0.0050,0.1896,1.0000 7.000,0.8561,0.01653,0.00809,-0.0047,0.1841,1.0000 7.250,0.8815,0.01677,0.00842,-0.0043,0.1776,1.0000 7.500,0.9061,0.01710,0.00875,-0.0040,0.1718,1.0000 7.750,0.9315,0.01735,0.00912,-0.0037,0.1648,1.0000 8.000,0.9560,0.01765,0.00943,-0.0033,0.1578,1.0000 8.250,0.9810,0.01791,0.00979,-0.0030,0.1488,1.0000 8.500,1.0055,0.01824,0.01017,-0.0026,0.1395,1.0000 8.750,1.0295,0.01861,0.01056,-0.0023,0.1295,1.0000 9.000,1.0529,0.01905,0.01101,-0.0018,0.1185,1.0000 9.250,1.0761,0.01954,0.01153,-0.0014,0.1062,1.0000 9.500,1.0982,0.02015,0.01215,-0.0009,0.0929,1.0000 9.750,1.1194,0.02087,0.01285,-0.0002,0.0798,1.0000 10.000,1.1395,0.02171,0.01368,0.0005,0.0685,1.0000 10.500,1.1773,0.02353,0.01557,0.0022,0.0514,1.0000 10.750,1.1947,0.02451,0.01662,0.0032,0.0458,1.0000 11.000,1.2109,0.02555,0.01773,0.0043,0.0413,1.0000 11.250,1.2249,0.02671,0.01896,0.0056,0.0380,1.0000 11.500,1.2392,0.02775,0.02014,0.0069,0.0352,1.0000 11.750,1.2504,0.02896,0.02144,0.0085,0.0328,1.0000 12.000,1.2549,0.03042,0.02297,0.0107,0.0309,1.0000 12.250,1.2610,0.03173,0.02444,0.0128,0.0296,1.0000 12.500,1.2663,0.03321,0.02606,0.0145,0.0283,1.0000 12.750,1.2698,0.03491,0.02790,0.0161,0.0272,1.0000 13.000,1.2718,0.03684,0.02996,0.0174,0.0263,1.0000 13.250,1.2716,0.03908,0.03232,0.0184,0.0255,1.0000 13.500,1.2685,0.04177,0.03512,0.0191,0.0248,1.0000 13.750,1.2618,0.04505,0.03853,0.0192,0.0242,1.0000 14.000,1.2542,0.04873,0.04233,0.0187,0.0237,1.0000 14.250,1.2491,0.05249,0.04628,0.0177,0.0233,1.0000 14.500,1.2414,0.05690,0.05087,0.0159,0.0229,1.0000 14.750,1.2316,0.06203,0.05617,0.0135,0.0226,1.0000 15.000,1.2198,0.06779,0.06212,0.0104,0.0223,1.0000 15.250,1.2064,0.07406,0.06854,0.0071,0.0220,1.0000 15.500,1.1920,0.08057,0.07522,0.0036,0.0218,1.0000 15.750,1.1774,0.08714,0.08192,0.0003,0.0216,1.0000