Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-nl722362-il-50000-n5 Airfoil,nl722362-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,28.5063 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-nl722362-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.4921,0.11030,0.10310,-0.0200,1.0000,0.1264 -9.500,-0.4916,0.10704,0.09990,-0.0210,1.0000,0.1309 -9.250,-0.5225,0.10495,0.09799,-0.0270,1.0000,0.1358 -9.000,-0.4070,0.08614,0.07948,-0.0313,1.0000,0.0699 -8.750,-0.4220,0.08029,0.07366,-0.0351,1.0000,0.0610 -8.250,-0.5264,0.08221,0.07526,-0.0348,1.0000,0.0607 -8.000,-0.5315,0.07872,0.07181,-0.0340,1.0000,0.0588 -7.750,-0.5403,0.07513,0.06822,-0.0330,1.0000,0.0566 -7.250,-0.5652,0.06781,0.06056,-0.0294,1.0000,0.0501 -7.000,-0.5664,0.06475,0.05744,-0.0270,1.0000,0.0492 -6.750,-0.5681,0.06179,0.05438,-0.0245,1.0000,0.0483 -6.500,-0.5691,0.05879,0.05122,-0.0218,1.0000,0.0473 -6.250,-0.5688,0.05570,0.04791,-0.0190,1.0000,0.0463 -6.000,-0.5665,0.05261,0.04455,-0.0161,1.0000,0.0454 -5.750,-0.5619,0.04960,0.04120,-0.0133,1.0000,0.0444 -5.500,-0.5551,0.04661,0.03782,-0.0104,1.0000,0.0436 -5.250,-0.5455,0.04377,0.03456,-0.0076,1.0000,0.0429 -5.000,-0.5334,0.04119,0.03155,-0.0050,1.0000,0.0425 -4.750,-0.5193,0.03881,0.02878,-0.0027,1.0000,0.0426 -4.500,-0.5036,0.03683,0.02650,-0.0008,1.0000,0.0442 -4.250,-0.4860,0.03494,0.02428,0.0011,1.0000,0.0459 -4.000,-0.4663,0.03307,0.02202,0.0030,1.0000,0.0474 -3.750,-0.4447,0.03129,0.01988,0.0045,1.0000,0.0483 -3.500,-0.4215,0.02968,0.01795,0.0059,1.0000,0.0492 -3.250,-0.3968,0.02824,0.01618,0.0071,1.0000,0.0507 -3.000,-0.3727,0.02684,0.01478,0.0080,1.0000,0.0546 -2.750,-0.3479,0.02586,0.01365,0.0089,1.0000,0.0594 -2.500,-0.3221,0.02486,0.01245,0.0097,1.0000,0.0644 -2.000,-0.1198,0.01952,0.01040,-0.0161,1.0000,1.0000 -1.750,-0.1074,0.01947,0.01004,-0.0136,1.0000,1.0000 -1.500,-0.0941,0.01945,0.00974,-0.0113,1.0000,1.0000 -1.250,-0.0801,0.01945,0.00951,-0.0090,1.0000,1.0000 -1.000,-0.0655,0.01948,0.00930,-0.0069,1.0000,1.0000 -0.750,-0.0504,0.01953,0.00916,-0.0048,1.0000,1.0000 -0.500,-0.0349,0.01961,0.00907,-0.0029,1.0000,1.0000 -0.250,-0.0191,0.01971,0.00902,-0.0010,1.0000,1.0000 0.000,-0.0030,0.01983,0.00901,0.0009,1.0000,1.0000 0.250,0.0132,0.01997,0.00904,0.0026,1.0000,1.0000 0.500,0.0297,0.02014,0.00911,0.0043,1.0000,1.0000 0.750,0.0461,0.02033,0.00924,0.0060,1.0000,1.0000 1.000,0.0627,0.02056,0.00940,0.0076,1.0000,1.0000 1.250,0.1013,0.02097,0.00979,0.0046,0.9918,1.0000 1.500,0.1674,0.02151,0.01035,-0.0036,0.9725,1.0000 1.750,0.2503,0.02160,0.01053,-0.0142,0.9404,1.0000 2.000,0.3229,0.02134,0.01040,-0.0222,0.9114,1.0000 2.250,0.3786,0.02100,0.01023,-0.0268,0.8867,1.0000 2.500,0.4154,0.02066,0.01002,-0.0276,0.8590,1.0000 2.750,0.4446,0.02032,0.00981,-0.0269,0.8269,1.0000 3.000,0.4580,0.02017,0.00981,-0.0234,0.7839,1.0000 3.250,0.4681,0.02002,0.00976,-0.0192,0.7160,1.0000 3.500,0.5439,0.01908,0.00800,-0.0241,0.5335,1.0000 3.750,0.5603,0.01996,0.00828,-0.0214,0.4391,1.0000 4.000,0.5766,0.02084,0.00878,-0.0192,0.3836,1.0000 4.250,0.5955,0.02165,0.00935,-0.0176,0.3470,1.0000 4.500,0.6159,0.02242,0.00996,-0.0164,0.3209,1.0000 4.750,0.6384,0.02315,0.01061,-0.0154,0.3008,1.0000 5.000,0.6625,0.02387,0.01135,-0.0147,0.2848,1.0000 5.250,0.6875,0.02459,0.01208,-0.0142,0.2705,1.0000 5.500,0.7133,0.02533,0.01285,-0.0138,0.2573,1.0000 5.750,0.7385,0.02607,0.01372,-0.0134,0.2446,1.0000 6.000,0.7632,0.02686,0.01465,-0.0128,0.2325,1.0000 6.250,0.7868,0.02770,0.01562,-0.0121,0.2205,1.0000 6.500,0.8096,0.02860,0.01661,-0.0112,0.2090,1.0000 6.750,0.8315,0.02952,0.01762,-0.0103,0.1975,1.0000 7.000,0.8511,0.03045,0.01878,-0.0090,0.1844,1.0000 7.250,0.8696,0.03144,0.01998,-0.0075,0.1709,1.0000 7.500,0.8867,0.03246,0.02122,-0.0059,0.1569,1.0000 7.750,0.9010,0.03333,0.02224,-0.0039,0.1417,1.0000 8.000,0.9136,0.03411,0.02316,-0.0016,0.1264,1.0000 8.250,0.9253,0.03494,0.02411,0.0007,0.1119,1.0000 8.500,0.9369,0.03603,0.02540,0.0030,0.0982,1.0000 8.750,0.9484,0.03723,0.02676,0.0053,0.0872,1.0000 9.000,0.9591,0.03856,0.02819,0.0076,0.0785,1.0000 9.250,0.9694,0.04076,0.03069,0.0098,0.0714,1.0000 9.500,0.9780,0.04213,0.03197,0.0121,0.0665,1.0000 9.750,0.9833,0.04498,0.03535,0.0147,0.0619,1.0000 10.000,0.9875,0.04744,0.03807,0.0172,0.0591,1.0000 10.250,0.9916,0.04953,0.04027,0.0195,0.0569,1.0000 10.500,0.9894,0.05238,0.04334,0.0222,0.0553,1.0000 10.750,0.9762,0.05579,0.04716,0.0257,0.0541,1.0000 11.000,0.9588,0.05927,0.05093,0.0289,0.0534,1.0000 11.250,0.9382,0.06320,0.05511,0.0310,0.0530,1.0000 11.500,0.9139,0.06796,0.06009,0.0317,0.0530,1.0000 11.750,0.8864,0.07391,0.06622,0.0304,0.0535,1.0000 12.000,0.8570,0.08142,0.07381,0.0266,0.0543,1.0000 12.250,0.8296,0.09046,0.08290,0.0211,0.0552,1.0000