Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca632a015-il-100000 Airfoil,naca632a015-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,45.8103 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-naca632a015-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.4574,0.09832,0.09332,-0.0351,1.0000,0.1273 -10.250,-0.4807,0.09221,0.08729,-0.0401,1.0000,0.1318 -10.000,-0.5319,0.08460,0.07972,-0.0469,1.0000,0.1331 -9.750,-0.5032,0.08214,0.07735,-0.0437,1.0000,0.1406 -9.500,-0.5249,0.07740,0.07264,-0.0454,1.0000,0.1444 -9.250,-0.5612,0.07315,0.06840,-0.0456,1.0000,0.1456 -9.000,-0.5948,0.07049,0.06574,-0.0423,1.0000,0.1463 -8.750,-0.6356,0.06858,0.06374,-0.0373,1.0000,0.1485 -6.000,-0.6458,0.04034,0.03246,-0.0036,0.9802,0.0858 -5.750,-0.6092,0.03789,0.02916,-0.0039,0.9725,0.0752 -5.500,-0.5725,0.03449,0.02563,-0.0057,0.9662,0.0730 -5.250,-0.5334,0.03232,0.02313,-0.0074,0.9595,0.0735 -5.000,-0.4947,0.03018,0.02077,-0.0094,0.9531,0.0768 -4.750,-0.4543,0.02832,0.01893,-0.0116,0.9464,0.0799 -4.500,-0.4060,0.02708,0.01752,-0.0151,0.9416,0.0874 -4.250,-0.3739,0.02539,0.01607,-0.0160,0.9333,0.0948 -4.000,-0.3332,0.02405,0.01486,-0.0185,0.9275,0.1070 -3.750,-0.3070,0.02332,0.01413,-0.0183,0.9180,0.1181 -3.500,-0.2756,0.02218,0.01303,-0.0193,0.9110,0.1320 -3.000,-0.2491,0.01879,0.01162,-0.0150,0.8933,0.5095 -2.750,-0.2448,0.01911,0.01250,-0.0086,0.8816,0.6611 -2.500,-0.2096,0.01986,0.01330,-0.0071,0.8762,0.7289 -2.250,-0.1898,0.02042,0.01383,-0.0043,0.8659,0.7563 -2.000,-0.1495,0.02094,0.01429,-0.0046,0.8605,0.7850 -1.750,-0.0850,0.02223,0.01556,-0.0074,0.8581,0.8168 -1.500,-0.0493,0.02303,0.01630,-0.0071,0.8485,0.8352 -1.250,-0.0002,0.02290,0.01604,-0.0107,0.8430,0.8420 -1.000,0.0328,0.02298,0.01604,-0.0118,0.8338,0.8492 -0.750,0.0661,0.02276,0.01572,-0.0128,0.8265,0.8578 -0.500,0.1083,0.02287,0.01575,-0.0154,0.8179,0.8633 -0.250,0.1333,0.02269,0.01550,-0.0150,0.8096,0.8737 0.000,0.1809,0.02278,0.01553,-0.0186,0.8010,0.8782 0.250,0.2245,0.02261,0.01529,-0.0213,0.7924,0.8847 0.500,0.2544,0.02257,0.01521,-0.0217,0.7811,0.8930 0.750,0.3070,0.02222,0.01477,-0.0256,0.7708,0.8975 1.000,0.3296,0.02204,0.01454,-0.0245,0.7581,0.9079 1.250,0.3759,0.02188,0.01435,-0.0278,0.7449,0.9129 1.500,0.4051,0.02175,0.01418,-0.0279,0.7342,0.9226 1.750,0.4498,0.02151,0.01389,-0.0309,0.7233,0.9283 2.000,0.4816,0.02148,0.01388,-0.0320,0.7108,0.9374 2.250,0.5207,0.02129,0.01367,-0.0341,0.6988,0.9446 2.500,0.5601,0.02099,0.01331,-0.0361,0.6881,0.9527 2.750,0.5973,0.02081,0.01316,-0.0381,0.6738,0.9606 3.000,0.6307,0.02065,0.01302,-0.0394,0.6598,0.9701 3.250,0.6738,0.02030,0.01267,-0.0425,0.6445,0.9772 3.500,0.7126,0.01997,0.01233,-0.0448,0.6284,0.9855 3.750,0.7528,0.01961,0.01197,-0.0475,0.6110,0.9936 4.000,0.7911,0.01918,0.01152,-0.0497,0.5919,1.0000 4.250,0.8060,0.01904,0.01134,-0.0476,0.5746,1.0000 4.500,0.8208,0.01889,0.01115,-0.0454,0.5564,1.0000 4.750,0.8338,0.01883,0.01106,-0.0429,0.5360,1.0000 5.000,0.8456,0.01883,0.01101,-0.0402,0.5137,1.0000 5.250,0.8584,0.01884,0.01091,-0.0376,0.4916,1.0000 5.500,0.8689,0.01898,0.01099,-0.0348,0.4686,1.0000 5.750,0.8791,0.01919,0.01111,-0.0318,0.4467,1.0000 6.000,0.8902,0.01945,0.01123,-0.0290,0.4270,1.0000 6.250,0.9017,0.01978,0.01141,-0.0263,0.4090,1.0000 6.500,0.9123,0.02017,0.01174,-0.0234,0.3917,1.0000 6.750,0.9248,0.02061,0.01208,-0.0209,0.3763,1.0000 7.000,0.9382,0.02110,0.01250,-0.0185,0.3621,1.0000 7.250,0.9516,0.02164,0.01302,-0.0161,0.3489,1.0000 7.500,0.9663,0.02224,0.01361,-0.0140,0.3368,1.0000 7.750,0.9828,0.02287,0.01418,-0.0123,0.3254,1.0000 8.000,1.0017,0.02352,0.01468,-0.0109,0.3138,1.0000 8.250,1.0136,0.02412,0.01537,-0.0084,0.3018,1.0000 8.500,1.0273,0.02478,0.01605,-0.0062,0.2901,1.0000 8.750,1.0434,0.02546,0.01667,-0.0045,0.2787,1.0000 9.000,1.0591,0.02612,0.01729,-0.0027,0.2676,1.0000 9.250,1.0705,0.02687,0.01818,-0.0003,0.2573,1.0000 9.500,1.0865,0.02767,0.01894,0.0014,0.2469,1.0000 9.750,1.1015,0.02840,0.01964,0.0032,0.2362,1.0000 10.000,1.1098,0.02924,0.02064,0.0060,0.2259,1.0000 10.250,1.1242,0.03015,0.02154,0.0078,0.2156,1.0000 10.500,1.1379,0.03096,0.02230,0.0097,0.2047,1.0000 10.750,1.1409,0.03193,0.02346,0.0131,0.1947,1.0000 11.000,1.1499,0.03286,0.02437,0.0155,0.1845,1.0000 11.250,1.1594,0.03360,0.02503,0.0178,0.1743,1.0000 11.500,1.1535,0.03462,0.02628,0.0223,0.1661,1.0000 11.750,1.1611,0.03547,0.02700,0.0247,0.1575,1.0000 12.000,1.1552,0.03655,0.02827,0.0287,0.1501,1.0000 12.250,1.1622,0.03769,0.02936,0.0307,0.1428,1.0000 12.500,1.1604,0.03907,0.03090,0.0334,0.1365,1.0000 12.750,1.1714,0.04038,0.03213,0.0347,0.1301,1.0000 13.000,1.1664,0.04221,0.03422,0.0372,0.1250,1.0000 13.250,1.1871,0.04332,0.03509,0.0375,0.1186,1.0000 13.500,1.1754,0.04565,0.03778,0.0400,0.1153,1.0000 13.750,1.1727,0.04770,0.04000,0.0415,0.1112,1.0000 14.000,1.1946,0.04907,0.04116,0.0417,0.1060,1.0000 14.250,1.1806,0.05205,0.04449,0.0434,0.1039,1.0000 14.500,1.1692,0.05519,0.04789,0.0445,0.1015,1.0000 14.750,1.1621,0.05816,0.05105,0.0451,0.0991,1.0000 15.000,1.1927,0.05933,0.05199,0.0453,0.0945,1.0000 15.250,1.1683,0.06349,0.05647,0.0458,0.0938,1.0000 15.500,1.1420,0.06837,0.06164,0.0455,0.0932,1.0000 15.750,1.1106,0.07425,0.06781,0.0442,0.0928,1.0000 16.000,1.0730,0.08150,0.07532,0.0417,0.0929,1.0000 16.250,1.0261,0.09097,0.08502,0.0374,0.0935,1.0000 16.500,0.9724,0.10312,0.09734,0.0313,0.0945,1.0000