Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-p51dtip-il-50000 Airfoil,p51dtip-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,22.6428 Max Cl/Cd alpha,6.75 Url,http://airfoiltools.com/polar/csv?polar=xf-p51dtip-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.4622,0.11232,0.10595,-0.0148,1.0000,0.3004 -9.750,-0.4622,0.10949,0.10318,-0.0152,1.0000,0.3187 -9.500,-0.4677,0.10696,0.10075,-0.0156,1.0000,0.3356 -9.250,-0.4445,0.10268,0.09644,-0.0145,1.0000,0.3607 -9.000,-0.4343,0.09951,0.09329,-0.0135,1.0000,0.3896 -8.750,-0.4194,0.09586,0.08966,-0.0127,1.0000,0.4153 -8.250,-0.4147,0.09084,0.08472,-0.0108,1.0000,0.4645 -8.000,-0.3912,0.08649,0.08035,-0.0109,1.0000,0.4831 -7.750,-0.3778,0.08362,0.07749,-0.0097,1.0000,0.5118 -6.750,-0.5346,0.07772,0.07236,0.0003,1.0000,0.4232 -6.500,-0.5786,0.07672,0.07153,0.0052,1.0000,0.4219 -6.250,-0.6439,0.07138,0.06630,0.0013,1.0000,0.3772 -6.000,-0.6740,0.05597,0.04928,-0.0188,1.0000,0.1738 -5.750,-0.6615,0.05095,0.04346,-0.0184,1.0000,0.1466 -5.500,-0.6474,0.04732,0.03896,-0.0172,1.0000,0.1359 -5.250,-0.6309,0.04407,0.03532,-0.0160,1.0000,0.1350 -5.000,-0.6116,0.04093,0.03177,-0.0149,1.0000,0.1321 -4.750,-0.5897,0.03811,0.02841,-0.0138,1.0000,0.1292 -4.500,-0.5674,0.03592,0.02577,-0.0127,1.0000,0.1319 -4.250,-0.5441,0.03422,0.02347,-0.0115,1.0000,0.1365 -4.000,-0.5198,0.03215,0.02124,-0.0106,1.0000,0.1393 -3.750,-0.4953,0.03065,0.01960,-0.0094,1.0000,0.1445 -3.500,-0.4719,0.02951,0.01840,-0.0080,1.0000,0.1559 -3.250,-0.1706,0.02963,0.02083,-0.0320,1.0000,1.0000 -3.000,-0.1654,0.02950,0.02047,-0.0296,1.0000,1.0000 -2.750,-0.1597,0.02938,0.02014,-0.0273,1.0000,1.0000 -2.500,-0.1537,0.02927,0.01981,-0.0249,1.0000,1.0000 -2.250,-0.1475,0.02915,0.01952,-0.0226,1.0000,1.0000 -2.000,-0.1411,0.02905,0.01926,-0.0202,1.0000,1.0000 -1.750,-0.1345,0.02894,0.01901,-0.0179,1.0000,1.0000 -1.500,-0.1279,0.02884,0.01877,-0.0155,1.0000,1.0000 -1.250,-0.1213,0.02873,0.01854,-0.0132,1.0000,1.0000 -1.000,-0.1147,0.02862,0.01831,-0.0108,1.0000,1.0000 -0.750,-0.1082,0.02850,0.01806,-0.0084,1.0000,1.0000 -0.500,-0.1019,0.02837,0.01784,-0.0060,1.0000,1.0000 -0.250,-0.0957,0.02824,0.01762,-0.0035,1.0000,1.0000 0.000,-0.0899,0.02808,0.01740,-0.0010,1.0000,1.0000 0.250,-0.0843,0.02791,0.01716,0.0016,1.0000,1.0000 0.500,-0.0790,0.02772,0.01691,0.0042,1.0000,1.0000 0.750,-0.0738,0.02751,0.01663,0.0069,1.0000,1.0000 1.000,-0.0684,0.02729,0.01637,0.0094,1.0000,1.0000 1.250,-0.0622,0.02709,0.01612,0.0119,1.0000,1.0000 1.500,-0.0539,0.02695,0.01594,0.0139,1.0000,1.0000 1.750,-0.0420,0.02695,0.01589,0.0153,1.0000,1.0000 2.000,-0.0269,0.02707,0.01597,0.0161,1.0000,1.0000 2.250,-0.0095,0.02730,0.01617,0.0164,1.0000,1.0000 2.500,0.0093,0.02762,0.01647,0.0165,1.0000,1.0000 2.750,0.0291,0.02800,0.01684,0.0164,1.0000,1.0000 3.000,0.0494,0.02845,0.01730,0.0162,1.0000,1.0000 3.250,0.0701,0.02896,0.01783,0.0159,1.0000,1.0000 3.500,0.0909,0.02952,0.01844,0.0156,1.0000,1.0000 3.750,0.1117,0.03013,0.01911,0.0152,1.0000,1.0000 4.000,0.1323,0.03080,0.01984,0.0148,1.0000,1.0000 4.250,0.1527,0.03153,0.02065,0.0144,1.0000,1.0000 4.500,0.1727,0.03231,0.02156,0.0139,1.0000,1.0000 4.750,0.1923,0.03316,0.02252,0.0135,1.0000,1.0000 5.000,0.2114,0.03409,0.02359,0.0130,1.0000,1.0000 5.250,0.2297,0.03512,0.02476,0.0125,1.0000,1.0000 5.500,0.2472,0.03625,0.02606,0.0119,1.0000,1.0000 5.750,0.2636,0.03753,0.02756,0.0112,1.0000,1.0000 6.000,0.4576,0.04316,0.03446,-0.0159,0.8504,1.0000 6.250,0.6294,0.02970,0.02297,-0.0110,0.5732,1.0000 6.500,0.6668,0.03000,0.01940,-0.0008,0.1747,1.0000 6.750,0.7411,0.03273,0.02192,-0.0044,0.1340,1.0000 7.000,0.7875,0.03596,0.02510,-0.0061,0.1175,1.0000 7.250,0.8168,0.03870,0.02843,-0.0055,0.1107,1.0000 7.500,0.8440,0.04215,0.03195,-0.0055,0.1035,1.0000 7.750,0.8661,0.04574,0.03606,-0.0044,0.1029,1.0000 8.000,0.8859,0.04982,0.04053,-0.0034,0.1036,1.0000 8.250,0.9005,0.05393,0.04505,-0.0021,0.1039,1.0000 8.500,0.9113,0.05809,0.04959,-0.0007,0.1041,1.0000 8.750,0.9003,0.06147,0.05397,0.0027,0.1108,1.0000 9.000,0.8998,0.06601,0.05883,0.0041,0.1140,1.0000 9.250,0.8980,0.07066,0.06381,0.0054,0.1205,1.0000 9.500,0.8807,0.07586,0.06931,0.0065,0.1289,1.0000 9.750,0.8454,0.08042,0.07413,0.0075,0.1391,1.0000 10.000,0.8090,0.08672,0.08054,0.0056,0.1528,1.0000