Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-b707b-il-100000-n5 Airfoil,b707b-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,31.1614 Max Cl/Cd alpha,6.25 Url,http://airfoiltools.com/polar/csv?polar=xf-b707b-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.000,-0.7178,0.09050,0.08565,-0.0135,1.0000,0.0408 -11.750,-0.7423,0.08269,0.07776,-0.0184,1.0000,0.0399 -11.500,-0.7713,0.07591,0.07086,-0.0221,1.0000,0.0398 -11.250,-0.7968,0.07051,0.06532,-0.0237,1.0000,0.0392 -11.000,-0.8194,0.06621,0.06085,-0.0236,1.0000,0.0390 -10.750,-0.8375,0.06276,0.05724,-0.0222,1.0000,0.0391 -10.500,-0.8524,0.05973,0.05403,-0.0197,1.0000,0.0392 -10.250,-0.8633,0.05688,0.05098,-0.0170,1.0000,0.0393 -10.000,-0.8679,0.05394,0.04781,-0.0148,1.0000,0.0394 -9.500,-0.8578,0.04764,0.04072,-0.0124,0.8577,0.0387 -9.250,-0.8504,0.04496,0.03757,-0.0104,0.8323,0.0383 -9.000,-0.8406,0.04240,0.03457,-0.0085,0.8175,0.0379 -8.750,-0.8277,0.03999,0.03173,-0.0068,0.8073,0.0375 -8.500,-0.8114,0.03772,0.02907,-0.0054,0.7992,0.0372 -8.250,-0.7921,0.03571,0.02670,-0.0044,0.7930,0.0369 -8.000,-0.7702,0.03386,0.02455,-0.0037,0.7878,0.0366 -7.750,-0.7463,0.03217,0.02261,-0.0033,0.7833,0.0364 -7.500,-0.7214,0.03066,0.02090,-0.0030,0.7794,0.0363 -7.250,-0.6958,0.02931,0.01936,-0.0027,0.7762,0.0362 -7.000,-0.6699,0.02809,0.01799,-0.0025,0.7734,0.0361 -6.750,-0.6444,0.02698,0.01679,-0.0023,0.7703,0.0361 -6.500,-0.6197,0.02598,0.01571,-0.0019,0.7671,0.0361 -6.250,-0.5963,0.02506,0.01473,-0.0013,0.7641,0.0362 -6.000,-0.5741,0.02425,0.01386,-0.0005,0.7611,0.0362 -5.750,-0.5529,0.02351,0.01306,0.0006,0.7585,0.0365 -5.500,-0.5322,0.02284,0.01232,0.0016,0.7558,0.0367 -5.250,-0.5115,0.02222,0.01164,0.0027,0.7528,0.0369 -5.000,-0.4907,0.02166,0.01101,0.0038,0.7500,0.0374 -4.750,-0.4694,0.02116,0.01043,0.0049,0.7474,0.0378 -4.500,-0.4476,0.02071,0.00988,0.0059,0.7450,0.0385 -4.250,-0.4253,0.02030,0.00939,0.0068,0.7430,0.0393 -4.000,-0.4024,0.01994,0.00894,0.0077,0.7412,0.0405 -3.750,-0.3787,0.01961,0.00854,0.0084,0.7394,0.0421 -3.500,-0.3547,0.01927,0.00822,0.0090,0.7373,0.0457 -3.250,-0.3303,0.01896,0.00792,0.0095,0.7348,0.0537 -3.000,-0.3057,0.01869,0.00762,0.0101,0.7322,0.0736 -2.750,-0.2854,0.01793,0.00722,0.0112,0.7298,0.1435 -2.500,-0.2729,0.01649,0.00680,0.0133,0.7276,0.3776 -2.250,-0.2519,0.01603,0.00663,0.0145,0.7254,0.4456 -2.000,-0.2316,0.01561,0.00666,0.0161,0.7227,0.5264 -1.750,-0.2078,0.01546,0.00669,0.0171,0.7193,0.5882 -1.500,-0.1847,0.01533,0.00679,0.0184,0.7153,0.6493 -1.250,-0.1606,0.01528,0.00690,0.0198,0.7113,0.6972 -1.000,-0.1345,0.01527,0.00691,0.0207,0.7063,0.7236 -0.750,-0.1083,0.01525,0.00694,0.0214,0.6983,0.7466 -0.500,-0.0823,0.01527,0.00698,0.0227,0.6905,0.7770 -0.250,-0.0546,0.01533,0.00712,0.0235,0.6808,0.8063 0.000,-0.0239,0.01548,0.00730,0.0240,0.6726,0.8329 0.250,0.0051,0.01554,0.00738,0.0244,0.6643,0.8500 0.500,0.0371,0.01554,0.00735,0.0240,0.6540,0.8592 0.750,0.0673,0.01549,0.00723,0.0240,0.6412,0.8691 1.000,0.0962,0.01540,0.00711,0.0242,0.6257,0.8792 1.250,0.1275,0.01533,0.00705,0.0238,0.6077,0.8880 1.500,0.1605,0.01529,0.00709,0.0229,0.5861,0.8960 1.750,0.1927,0.01535,0.00740,0.0217,0.4812,0.9051 2.000,0.2148,0.01550,0.00653,0.0235,0.3903,0.9147 2.250,0.2480,0.01595,0.00684,0.0222,0.3548,0.9218 2.500,0.2799,0.01630,0.00710,0.0211,0.3269,0.9302 2.750,0.3104,0.01666,0.00735,0.0202,0.2992,0.9391 3.000,0.3461,0.01706,0.00759,0.0182,0.2747,0.9451 3.250,0.3790,0.01737,0.00784,0.0168,0.2544,0.9532 3.500,0.4121,0.01763,0.00808,0.0154,0.2281,0.9619 3.750,0.4485,0.01794,0.00823,0.0133,0.1752,0.9684 4.000,0.4817,0.01844,0.00846,0.0116,0.1443,0.9760 4.250,0.5148,0.01884,0.00878,0.0101,0.1273,0.9834 4.500,0.5498,0.01922,0.00909,0.0082,0.1180,0.9893 4.750,0.5838,0.01959,0.00945,0.0064,0.1124,0.9953 5.000,0.6151,0.02003,0.00981,0.0051,0.1075,1.0000 5.250,0.6316,0.02039,0.01018,0.0067,0.1036,1.0000 5.500,0.6474,0.02083,0.01060,0.0084,0.0990,1.0000 5.750,0.6625,0.02138,0.01107,0.0102,0.0953,1.0000 6.000,0.6788,0.02182,0.01155,0.0118,0.0927,1.0000 6.250,0.6949,0.02230,0.01207,0.0136,0.0905,1.0000 6.500,0.7107,0.02281,0.01262,0.0153,0.0893,1.0000 6.750,0.7265,0.02336,0.01323,0.0171,0.0884,1.0000 7.000,0.7422,0.02395,0.01384,0.0188,0.0874,1.0000 7.250,0.7577,0.02458,0.01450,0.0206,0.0861,1.0000 7.500,0.7726,0.02537,0.01524,0.0223,0.0843,1.0000 7.750,0.7891,0.02604,0.01595,0.0239,0.0831,1.0000 8.000,0.8062,0.02665,0.01668,0.0254,0.0823,1.0000 8.250,0.8235,0.02729,0.01742,0.0269,0.0815,1.0000 8.500,0.8407,0.02797,0.01821,0.0283,0.0807,1.0000 8.750,0.8577,0.02868,0.01903,0.0297,0.0797,1.0000 9.000,0.8744,0.02942,0.01988,0.0311,0.0785,1.0000 9.250,0.8904,0.03017,0.02073,0.0326,0.0771,1.0000 9.500,0.9061,0.03097,0.02160,0.0340,0.0757,1.0000 9.750,0.9214,0.03184,0.02250,0.0353,0.0739,1.0000 10.000,0.9375,0.03292,0.02356,0.0365,0.0722,1.0000 10.250,0.9500,0.03363,0.02454,0.0382,0.0710,1.0000 10.500,0.9629,0.03449,0.02561,0.0399,0.0700,1.0000 10.750,0.9746,0.03541,0.02675,0.0415,0.0688,1.0000 11.000,0.9852,0.03640,0.02795,0.0433,0.0675,1.0000 11.250,0.9937,0.03744,0.02919,0.0452,0.0663,1.0000 11.500,0.9998,0.03849,0.03041,0.0473,0.0650,1.0000 11.750,1.0049,0.03955,0.03159,0.0492,0.0634,1.0000 12.000,1.0099,0.04060,0.03263,0.0508,0.0615,1.0000 12.250,1.0068,0.04225,0.03470,0.0523,0.0591,1.0000 12.500,1.0061,0.04407,0.03681,0.0533,0.0565,1.0000 12.750,1.0058,0.04591,0.03887,0.0539,0.0540,1.0000 13.000,1.0062,0.04769,0.04079,0.0543,0.0520,1.0000 13.250,0.9978,0.05109,0.04458,0.0543,0.0489,1.0000 13.500,0.9874,0.05472,0.04849,0.0538,0.0465,1.0000 13.750,0.9749,0.05872,0.05271,0.0528,0.0446,1.0000 14.000,0.9570,0.06373,0.05791,0.0508,0.0432,1.0000 14.250,0.9296,0.07080,0.06517,0.0471,0.0435,1.0000 14.500,0.8441,0.09105,0.08564,0.0341,0.0492,1.0000