Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-b707d-il-200000-n5 Airfoil,b707d-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,52.2535 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-b707d-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.4636,0.09244,0.08895,-0.0329,1.0000,0.0256 -9.000,-0.4668,0.08791,0.08448,-0.0370,1.0000,0.0256 -7.250,-0.4951,0.06003,0.05626,-0.0380,1.0000,0.0268 -7.000,-0.4945,0.05726,0.05353,-0.0362,1.0000,0.0277 -6.750,-0.4775,0.05371,0.04989,-0.0379,0.9943,0.0287 -6.500,-0.4542,0.04993,0.04591,-0.0407,0.9866,0.0299 -6.250,-0.4291,0.04668,0.04244,-0.0430,0.9789,0.0328 -6.000,-0.3944,0.04539,0.04063,-0.0444,0.9714,0.0371 -5.750,-0.3656,0.04313,0.03802,-0.0458,0.9645,0.0375 -5.500,-0.3392,0.04047,0.03505,-0.0468,0.9565,0.0376 -5.250,-0.3131,0.03788,0.03215,-0.0475,0.9484,0.0377 -5.000,-0.2931,0.03183,0.02583,-0.0487,0.9407,0.0392 -4.750,-0.2668,0.02930,0.02316,-0.0495,0.9330,0.0403 -4.500,-0.2384,0.02719,0.02084,-0.0496,0.9251,0.0340 -4.250,-0.2096,0.02539,0.01875,-0.0499,0.9181,0.0341 -4.000,-0.1833,0.02329,0.01634,-0.0495,0.9092,0.0308 -3.750,-0.1517,0.02235,0.01490,-0.0488,0.9021,0.0264 -3.500,-0.1249,0.02111,0.01356,-0.0487,0.8937,0.0252 -3.250,-0.0981,0.01949,0.01177,-0.0485,0.8863,0.0245 -3.000,-0.0715,0.01828,0.01040,-0.0482,0.8783,0.0240 -2.750,-0.0447,0.01725,0.00921,-0.0479,0.8707,0.0235 -2.500,-0.0178,0.01635,0.00820,-0.0476,0.8635,0.0230 -2.250,0.0084,0.01556,0.00733,-0.0471,0.8561,0.0226 -2.000,0.0346,0.01485,0.00656,-0.0467,0.8490,0.0222 -1.750,0.0600,0.01423,0.00590,-0.0461,0.8414,0.0219 -1.500,0.0853,0.01367,0.00529,-0.0456,0.8349,0.0216 -1.250,0.1100,0.01318,0.00479,-0.0449,0.8276,0.0214 -1.000,0.1350,0.01276,0.00433,-0.0443,0.8210,0.0213 -0.750,0.1598,0.01240,0.00396,-0.0438,0.8140,0.0212 -0.500,0.1852,0.01212,0.00362,-0.0433,0.8075,0.0212 -0.250,0.2109,0.01191,0.00334,-0.0429,0.8009,0.0213 0.000,0.2370,0.01175,0.00312,-0.0426,0.7941,0.0216 0.250,0.2634,0.01164,0.00293,-0.0422,0.7880,0.0222 0.500,0.2895,0.01155,0.00279,-0.0419,0.7801,0.0232 0.750,0.3153,0.01147,0.00264,-0.0413,0.7678,0.0251 1.000,0.3391,0.01133,0.00238,-0.0400,0.7402,0.0346 1.250,0.3516,0.00978,0.00218,-0.0373,0.7061,0.5890 1.500,0.3679,0.00920,0.00218,-0.0343,0.6701,0.7705 1.750,0.4161,0.00903,0.00229,-0.0378,0.6342,0.9356 2.000,0.4471,0.00915,0.00227,-0.0385,0.6039,0.9488 2.250,0.4783,0.00932,0.00228,-0.0393,0.5640,0.9636 2.500,0.5066,0.00970,0.00230,-0.0396,0.4856,0.9767 2.750,0.5332,0.01043,0.00251,-0.0399,0.3775,0.9893 3.000,0.5613,0.01104,0.00279,-0.0406,0.3078,1.0000 3.250,0.5816,0.01145,0.00302,-0.0394,0.2705,1.0000 3.500,0.6027,0.01181,0.00327,-0.0383,0.2422,1.0000 3.750,0.6244,0.01211,0.00353,-0.0373,0.2212,1.0000 4.000,0.6465,0.01240,0.00382,-0.0364,0.2046,1.0000 4.250,0.6678,0.01278,0.00413,-0.0353,0.1792,1.0000 4.500,0.6857,0.01348,0.00453,-0.0339,0.1217,1.0000 4.750,0.7019,0.01441,0.00509,-0.0322,0.0575,1.0000 5.000,0.7236,0.01482,0.00558,-0.0312,0.0483,1.0000 5.250,0.7458,0.01519,0.00603,-0.0303,0.0382,1.0000 5.500,0.7672,0.01567,0.00652,-0.0292,0.0277,1.0000 5.750,0.7877,0.01626,0.00711,-0.0280,0.0227,1.0000 6.000,0.8078,0.01693,0.00792,-0.0268,0.0200,1.0000 6.250,0.8262,0.01780,0.00894,-0.0252,0.0176,1.0000 6.500,0.8412,0.01898,0.01028,-0.0232,0.0150,1.0000 6.750,0.8603,0.01970,0.01112,-0.0219,0.0134,1.0000 7.000,0.8771,0.02068,0.01221,-0.0202,0.0125,1.0000 7.250,0.8932,0.02180,0.01342,-0.0185,0.0115,1.0000 7.500,0.9095,0.02298,0.01467,-0.0169,0.0110,1.0000 7.750,0.9255,0.02434,0.01613,-0.0153,0.0105,1.0000 8.000,0.9415,0.02607,0.01790,-0.0139,0.0101,1.0000 8.250,0.9598,0.02796,0.01992,-0.0127,0.0098,1.0000 8.500,0.9785,0.02972,0.02190,-0.0115,0.0096,1.0000 8.750,0.9958,0.03150,0.02401,-0.0100,0.0092,1.0000 9.000,1.0109,0.03325,0.02608,-0.0084,0.0085,1.0000 9.250,1.0239,0.03462,0.02767,-0.0067,0.0076,1.0000 9.500,1.0346,0.03631,0.02957,-0.0049,0.0073,1.0000 9.750,1.0417,0.03842,0.03194,-0.0028,0.0071,1.0000 10.000,1.0451,0.04047,0.03422,-0.0003,0.0069,1.0000 10.250,1.0434,0.04269,0.03665,0.0027,0.0068,1.0000 10.500,1.0385,0.04521,0.03941,0.0056,0.0067,1.0000 10.750,1.0306,0.04797,0.04240,0.0081,0.0067,1.0000 11.000,1.0198,0.05109,0.04577,0.0102,0.0066,1.0000 11.250,1.0064,0.05463,0.04953,0.0115,0.0066,1.0000 11.500,0.9936,0.05828,0.05341,0.0120,0.0066,1.0000 11.750,0.9776,0.06267,0.05801,0.0117,0.0066,1.0000 12.000,0.9615,0.06753,0.06308,0.0103,0.0066,1.0000 12.250,0.9431,0.07326,0.06899,0.0078,0.0066,1.0000 12.500,0.9244,0.07997,0.07591,0.0040,0.0067,1.0000 12.750,0.9033,0.08836,0.08450,-0.0015,0.0068,1.0000 13.000,0.8595,0.10602,0.10242,-0.0132,0.0072,1.0000