Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-nl722362-il-500000-n5 Airfoil,nl722362-il Reynolds number,500000 Ncrit,5 Mach,0 Max Cl/Cd,70.7531 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-nl722362-il-500000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.5081,0.09133,0.08895,-0.0270,1.0000,0.0072 -9.750,-0.5069,0.08829,0.08593,-0.0283,1.0000,0.0071 -9.500,-0.5126,0.08322,0.08090,-0.0309,1.0000,0.0071 -9.250,-0.5188,0.07838,0.07609,-0.0338,1.0000,0.0071 -9.000,-0.5222,0.07489,0.07263,-0.0364,1.0000,0.0069 -8.750,-0.5442,0.06797,0.06571,-0.0415,0.9967,0.0070 -8.500,-0.5400,0.06234,0.05997,-0.0466,0.9752,0.0068 -8.250,-0.5382,0.05431,0.05172,-0.0515,0.9600,0.0069 -8.000,-0.5344,0.04813,0.04528,-0.0530,0.9485,0.0069 -7.750,-0.5403,0.03976,0.03645,-0.0511,0.9373,0.0072 -7.500,-0.5411,0.03354,0.02977,-0.0480,0.9298,0.0072 -7.250,-0.5441,0.02687,0.02242,-0.0436,0.9233,0.0074 -7.000,-0.5295,0.02496,0.02025,-0.0419,0.9197,0.0076 -6.750,-0.5090,0.02423,0.01940,-0.0410,0.9171,0.0078 -6.500,-0.4908,0.02244,0.01733,-0.0395,0.9146,0.0081 -6.250,-0.4704,0.02113,0.01582,-0.0384,0.9123,0.0085 -6.000,-0.4513,0.01872,0.01299,-0.0366,0.9099,0.0087 -5.750,-0.4291,0.01699,0.01096,-0.0354,0.9078,0.0089 -5.500,-0.4055,0.01573,0.00945,-0.0345,0.9060,0.0093 -5.250,-0.3811,0.01479,0.00833,-0.0337,0.9044,0.0096 -5.000,-0.3564,0.01407,0.00747,-0.0331,0.9029,0.0098 -4.750,-0.3328,0.01325,0.00657,-0.0323,0.9015,0.0101 -4.500,-0.3084,0.01270,0.00599,-0.0317,0.9001,0.0105 -4.250,-0.2834,0.01232,0.00559,-0.0311,0.8987,0.0111 -4.000,-0.2587,0.01194,0.00517,-0.0305,0.8971,0.0118 -3.750,-0.2342,0.01152,0.00471,-0.0298,0.8957,0.0123 -3.500,-0.2097,0.01114,0.00429,-0.0292,0.8943,0.0126 -3.250,-0.1853,0.01074,0.00386,-0.0284,0.8929,0.0131 -3.000,-0.1602,0.01043,0.00355,-0.0279,0.8916,0.0139 -2.750,-0.1347,0.01019,0.00329,-0.0274,0.8901,0.0149 -2.500,-0.1091,0.00998,0.00305,-0.0268,0.8874,0.0162 -2.250,-0.0836,0.00976,0.00280,-0.0262,0.8842,0.0185 -2.000,-0.0591,0.00954,0.00261,-0.0254,0.8795,0.0249 -1.750,-0.0353,0.00924,0.00237,-0.0244,0.8711,0.0476 -1.500,-0.0134,0.00884,0.00212,-0.0229,0.8571,0.1018 -1.250,0.0061,0.00816,0.00186,-0.0212,0.8414,0.2406 -1.000,0.0185,0.00697,0.00166,-0.0183,0.8298,0.5260 -0.750,0.0275,0.00603,0.00160,-0.0141,0.8230,0.7579 -0.500,0.1272,0.00617,0.00223,-0.0289,0.8137,0.9278 -0.250,0.1534,0.00626,0.00226,-0.0283,0.8040,0.9397 0.000,0.1779,0.00635,0.00229,-0.0273,0.7905,0.9496 0.250,0.2117,0.00646,0.00227,-0.0283,0.7369,0.9557 0.500,0.2293,0.00710,0.00226,-0.0259,0.6062,0.9637 0.750,0.2582,0.00764,0.00238,-0.0263,0.5111,0.9673 1.000,0.2844,0.00807,0.00249,-0.0262,0.4376,0.9719 1.250,0.3093,0.00846,0.00259,-0.0257,0.3757,0.9760 1.500,0.3407,0.00880,0.00266,-0.0268,0.3150,0.9779 1.750,0.3714,0.00908,0.00274,-0.0277,0.2704,0.9802 2.000,0.4007,0.00933,0.00282,-0.0282,0.2375,0.9828 2.250,0.4275,0.00955,0.00292,-0.0281,0.2151,0.9856 2.500,0.4587,0.00971,0.00299,-0.0290,0.1978,0.9870 2.750,0.4908,0.00985,0.00308,-0.0301,0.1854,0.9885 3.000,0.5226,0.00999,0.00317,-0.0312,0.1766,0.9903 3.250,0.5545,0.01017,0.00328,-0.0322,0.1674,0.9926 3.500,0.5861,0.01030,0.00341,-0.0332,0.1605,0.9948 3.750,0.6191,0.01045,0.00352,-0.0346,0.1542,0.9964 4.000,0.6507,0.01056,0.00364,-0.0356,0.1500,0.9980 4.250,0.6814,0.01069,0.00378,-0.0364,0.1451,0.9993 4.500,0.7085,0.01086,0.00394,-0.0364,0.1401,1.0000 4.750,0.7316,0.01103,0.00412,-0.0355,0.1367,1.0000 5.000,0.7547,0.01118,0.00428,-0.0347,0.1311,1.0000 5.250,0.7773,0.01138,0.00446,-0.0337,0.1228,1.0000 5.500,0.8003,0.01154,0.00464,-0.0329,0.1151,1.0000 5.750,0.8230,0.01174,0.00483,-0.0319,0.1078,1.0000 6.000,0.8455,0.01195,0.00503,-0.0310,0.0952,1.0000 6.250,0.8666,0.01230,0.00527,-0.0298,0.0773,1.0000 6.500,0.8873,0.01269,0.00560,-0.0286,0.0623,1.0000 6.750,0.9076,0.01314,0.00599,-0.0273,0.0487,1.0000 7.000,0.9274,0.01363,0.00643,-0.0260,0.0363,1.0000 7.250,0.9471,0.01413,0.00689,-0.0246,0.0270,1.0000 7.500,0.9669,0.01461,0.00737,-0.0232,0.0221,1.0000 7.750,0.9865,0.01511,0.00789,-0.0218,0.0193,1.0000 8.000,1.0065,0.01553,0.00839,-0.0204,0.0178,1.0000 8.250,1.0255,0.01606,0.00895,-0.0190,0.0162,1.0000 8.500,1.0441,0.01661,0.00956,-0.0174,0.0150,1.0000 8.750,1.0629,0.01710,0.01013,-0.0159,0.0142,1.0000 9.000,1.0811,0.01762,0.01072,-0.0143,0.0134,1.0000 9.250,1.0984,0.01821,0.01138,-0.0125,0.0128,1.0000 9.500,1.1141,0.01891,0.01215,-0.0106,0.0122,1.0000 9.750,1.1288,0.01965,0.01298,-0.0084,0.0118,1.0000 10.000,1.1438,0.02031,0.01374,-0.0064,0.0115,1.0000 10.250,1.1583,0.02096,0.01449,-0.0042,0.0112,1.0000 10.500,1.1710,0.02170,0.01533,-0.0018,0.0109,1.0000 10.750,1.1827,0.02246,0.01618,0.0007,0.0105,1.0000 11.000,1.1927,0.02327,0.01709,0.0035,0.0103,1.0000 11.250,1.2019,0.02407,0.01800,0.0063,0.0101,1.0000 11.500,1.2073,0.02487,0.01889,0.0099,0.0098,1.0000 11.750,1.2089,0.02569,0.01979,0.0140,0.0097,1.0000 12.000,1.2106,0.02659,0.02078,0.0179,0.0095,1.0000 12.250,1.2117,0.02763,0.02192,0.0215,0.0094,1.0000 12.500,1.2084,0.02905,0.02343,0.0253,0.0092,1.0000 12.750,1.2080,0.03042,0.02492,0.0285,0.0090,1.0000 13.000,1.2089,0.03179,0.02642,0.0312,0.0090,1.0000 13.250,1.2082,0.03340,0.02817,0.0337,0.0088,1.0000 13.500,1.2076,0.03508,0.03001,0.0359,0.0087,1.0000 13.750,1.2042,0.03711,0.03217,0.0380,0.0087,1.0000 14.000,1.2008,0.03929,0.03450,0.0395,0.0086,1.0000 14.250,1.1935,0.04205,0.03742,0.0407,0.0084,1.0000 14.500,1.1869,0.04505,0.04057,0.0411,0.0084,1.0000 14.750,1.1764,0.04893,0.04461,0.0405,0.0084,1.0000 15.000,1.1641,0.05369,0.04954,0.0386,0.0083,1.0000 15.250,1.1492,0.05960,0.05562,0.0355,0.0083,1.0000 15.500,1.1333,0.06637,0.06257,0.0314,0.0083,1.0000 15.750,1.1167,0.07351,0.06985,0.0272,0.0083,1.0000 16.000,1.0934,0.08187,0.07836,0.0226,0.0083,1.0000 16.250,1.0748,0.08937,0.08598,0.0186,0.0083,1.0000