Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-nlr7301-il-100000 Airfoil,nlr7301-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,21.501 Max Cl/Cd alpha,6.5 Url,http://airfoiltools.com/polar/csv?polar=xf-nlr7301-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.000,-0.7978,0.06937,0.06245,-0.0695,1.0000,0.1013 -11.750,-0.8143,0.06582,0.05882,-0.0683,1.0000,0.1010 -11.500,-0.8382,0.06327,0.05621,-0.0651,1.0000,0.1007 -11.250,-0.8672,0.06151,0.05441,-0.0600,1.0000,0.1004 -11.000,-0.8932,0.05949,0.05229,-0.0553,1.0000,0.1002 -10.750,-0.9158,0.05731,0.04995,-0.0509,1.0000,0.0999 -10.500,-0.9339,0.05494,0.04738,-0.0469,1.0000,0.0998 -10.250,-0.9468,0.05245,0.04462,-0.0435,1.0000,0.0998 -10.000,-0.9538,0.04997,0.04186,-0.0405,1.0000,0.1001 -9.750,-0.9579,0.04758,0.03911,-0.0378,1.0000,0.1008 -9.500,-0.9553,0.04528,0.03650,-0.0357,1.0000,0.1018 -9.250,-0.9385,0.04380,0.03516,-0.0345,1.0000,0.1035 -9.000,-0.9257,0.04234,0.03364,-0.0331,1.0000,0.1052 -8.750,-0.9136,0.04067,0.03178,-0.0316,1.0000,0.1069 -8.500,-0.9004,0.03894,0.02978,-0.0303,1.0000,0.1086 -8.250,-0.8860,0.03734,0.02782,-0.0291,1.0000,0.1105 -8.000,-0.8674,0.03587,0.02638,-0.0282,1.0000,0.1130 -7.750,-0.8482,0.03486,0.02539,-0.0272,1.0000,0.1159 -7.500,-0.8290,0.03376,0.02413,-0.0263,1.0000,0.1191 -7.250,-0.8091,0.03257,0.02275,-0.0255,1.0000,0.1222 -7.000,-0.7887,0.03157,0.02190,-0.0246,1.0000,0.1258 -6.750,-0.7681,0.03075,0.02102,-0.0237,1.0000,0.1304 -6.500,-0.7473,0.02978,0.02005,-0.0228,1.0000,0.1350 -6.250,-0.7266,0.02901,0.01939,-0.0219,1.0000,0.1402 -6.000,-0.7052,0.02826,0.01857,-0.0212,1.0000,0.1466 -5.750,-0.6847,0.02749,0.01801,-0.0202,1.0000,0.1535 -5.500,-0.6633,0.02678,0.01734,-0.0195,1.0000,0.1619 -5.250,-0.6417,0.02614,0.01682,-0.0189,1.0000,0.1722 -5.000,-0.6202,0.02541,0.01631,-0.0183,1.0000,0.1844 -4.750,-0.5976,0.02472,0.01583,-0.0180,1.0000,0.2010 -4.500,-0.5736,0.02397,0.01533,-0.0181,1.0000,0.2264 -4.250,-0.5448,0.02257,0.01462,-0.0200,1.0000,0.2879 -4.000,-0.5219,0.02203,0.01583,-0.0192,1.0000,0.5276 -3.750,-0.5027,0.02315,0.01693,-0.0168,1.0000,0.5842 -3.500,-0.4886,0.02443,0.01822,-0.0129,1.0000,0.6077 -3.250,-0.4729,0.02557,0.01933,-0.0096,1.0000,0.6267 -3.000,-0.4591,0.02673,0.02049,-0.0058,1.0000,0.6414 -2.750,-0.4473,0.02784,0.02162,-0.0014,1.0000,0.6524 -2.500,-0.4251,0.02869,0.02241,-0.0001,0.9990,0.6685 -2.250,-0.4038,0.03026,0.02402,0.0035,0.9941,0.6774 -2.000,-0.3719,0.03119,0.02488,0.0030,0.9886,0.6924 -1.750,-0.3497,0.03239,0.02611,0.0059,0.9827,0.7018 -1.500,-0.3178,0.03314,0.02681,0.0052,0.9767,0.7156 -1.250,-0.2970,0.03400,0.02769,0.0080,0.9698,0.7265 -1.000,-0.2736,0.03501,0.02871,0.0105,0.9630,0.7425 -0.750,-0.2546,0.03566,0.02939,0.0135,0.9549,0.7605 -0.500,-0.2247,0.03642,0.03013,0.0138,0.9473,0.7779 -0.250,-0.2062,0.03643,0.03017,0.0164,0.9381,0.7859 0.000,-0.1633,0.03672,0.03042,0.0126,0.9296,0.7942 0.250,-0.1377,0.03651,0.03021,0.0126,0.9188,0.7997 0.500,-0.1010,0.03661,0.03032,0.0109,0.9087,0.8048 0.750,-0.0624,0.03652,0.03023,0.0083,0.8962,0.8102 1.000,0.0273,0.03587,0.02954,-0.0006,0.8702,0.8142 1.250,0.0735,0.03440,0.02808,-0.0014,0.8426,0.8175 1.500,0.1335,0.03318,0.02690,-0.0046,0.8278,0.8206 1.750,0.1632,0.03239,0.02615,-0.0044,0.8115,0.8239 2.000,0.2278,0.03090,0.02473,-0.0086,0.7992,0.8273 2.250,0.2865,0.02905,0.02294,-0.0116,0.7838,0.8304 2.500,0.3284,0.02733,0.02128,-0.0123,0.7629,0.8328 2.750,0.3578,0.02557,0.01959,-0.0100,0.7337,0.8355 3.000,0.3752,0.02411,0.01815,-0.0060,0.6781,0.8390 3.250,0.3920,0.02425,0.01617,-0.0010,0.3261,0.8417 3.500,0.3988,0.02532,0.01649,0.0015,0.2469,0.8446 3.750,0.4189,0.02595,0.01680,0.0019,0.2144,0.8474 4.000,0.4421,0.02653,0.01712,0.0019,0.1945,0.8507 4.250,0.4635,0.02689,0.01735,0.0029,0.1801,0.8540 4.500,0.4896,0.02744,0.01776,0.0030,0.1682,0.8571 4.750,0.5195,0.02817,0.01829,0.0021,0.1583,0.8600 5.000,0.5506,0.02880,0.01885,0.0011,0.1501,0.8630 5.250,0.5858,0.02978,0.01970,-0.0008,0.1433,0.8660 5.500,0.6118,0.03028,0.02021,-0.0006,0.1375,0.8693 5.750,0.6426,0.03127,0.02102,-0.0013,0.1328,0.8731 6.000,0.6709,0.03203,0.02194,-0.0015,0.1290,0.8770 6.250,0.7027,0.03304,0.02297,-0.0027,0.1258,0.8804 6.500,0.7334,0.03411,0.02401,-0.0037,0.1233,0.8836 6.750,0.7610,0.03550,0.02540,-0.0039,0.1213,0.8870 7.000,0.7836,0.03657,0.02677,-0.0033,0.1196,0.8911 7.250,0.8075,0.03787,0.02831,-0.0032,0.1176,0.8958 7.500,0.8288,0.03911,0.02974,-0.0026,0.1159,0.9003 7.750,0.8490,0.04045,0.03124,-0.0018,0.1146,0.9051 8.000,0.8706,0.04218,0.03316,-0.0015,0.1139,0.9097 8.250,0.8900,0.04413,0.03535,-0.0011,0.1136,0.9141 8.500,0.9028,0.04627,0.03782,0.0004,0.1137,0.9190 8.750,0.9109,0.04914,0.04111,0.0019,0.1145,0.9242 9.000,0.9127,0.05248,0.04491,0.0040,0.1159,0.9296 9.250,0.9097,0.05589,0.04870,0.0063,0.1175,0.9361 9.500,0.9079,0.05934,0.05244,0.0079,0.1188,0.9428 9.750,0.9067,0.06266,0.05598,0.0095,0.1199,0.9504 10.000,0.9124,0.06614,0.05958,0.0100,0.1209,0.9582