Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-c5b-il-100000-n5 Airfoil,c5b-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,42.6446 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-c5b-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.7324,0.06422,0.05815,-0.0567,1.0000,0.0328 -10.000,-0.7551,0.06178,0.05561,-0.0523,1.0000,0.0328 -9.750,-0.7727,0.05896,0.05263,-0.0485,1.0000,0.0327 -9.500,-0.7864,0.05609,0.04955,-0.0448,1.0000,0.0327 -9.250,-0.7960,0.05318,0.04641,-0.0413,1.0000,0.0327 -9.000,-0.8019,0.05028,0.04323,-0.0379,1.0000,0.0327 -8.750,-0.8041,0.04744,0.04007,-0.0348,1.0000,0.0327 -8.500,-0.8027,0.04472,0.03700,-0.0319,1.0000,0.0327 -8.000,-0.7891,0.03969,0.03135,-0.0271,1.0000,0.0331 -7.750,-0.7777,0.03751,0.02892,-0.0252,1.0000,0.0334 -7.500,-0.7641,0.03560,0.02679,-0.0235,1.0000,0.0338 -7.250,-0.7488,0.03388,0.02486,-0.0219,1.0000,0.0343 -7.000,-0.7320,0.03231,0.02309,-0.0205,1.0000,0.0349 -6.750,-0.7141,0.03086,0.02144,-0.0191,1.0000,0.0356 -6.500,-0.6951,0.02955,0.01993,-0.0179,1.0000,0.0366 -6.250,-0.6752,0.02841,0.01861,-0.0167,1.0000,0.0382 -6.000,-0.6546,0.02740,0.01736,-0.0156,1.0000,0.0400 -5.750,-0.6342,0.02621,0.01612,-0.0146,1.0000,0.0416 -5.500,-0.6138,0.02524,0.01513,-0.0136,1.0000,0.0433 -5.250,-0.5931,0.02438,0.01423,-0.0126,1.0000,0.0453 -5.000,-0.5668,0.02364,0.01337,-0.0127,0.9986,0.0488 -4.750,-0.5381,0.02276,0.01250,-0.0135,0.9964,0.0527 -4.500,-0.5078,0.02209,0.01177,-0.0144,0.9942,0.0574 -4.250,-0.4792,0.02141,0.01109,-0.0151,0.9913,0.0646 -4.000,-0.4493,0.02080,0.01048,-0.0160,0.9885,0.0745 -3.750,-0.4182,0.02019,0.01001,-0.0172,0.9860,0.0976 -3.500,-0.3885,0.01951,0.00959,-0.0182,0.9833,0.1486 -3.250,-0.3603,0.01871,0.00924,-0.0191,0.9800,0.2339 -3.000,-0.3319,0.01772,0.00900,-0.0201,0.9772,0.3889 -2.750,-0.3047,0.01701,0.00922,-0.0200,0.9748,0.5817 -2.500,-0.2816,0.01693,0.00952,-0.0184,0.9703,0.6940 -2.250,-0.2543,0.01702,0.00968,-0.0177,0.9661,0.7467 -2.000,-0.2219,0.01715,0.00974,-0.0184,0.9629,0.7737 -1.750,-0.1964,0.01720,0.00974,-0.0178,0.9577,0.7958 -1.500,-0.1682,0.01730,0.00981,-0.0175,0.9532,0.8218 -1.250,-0.1374,0.01745,0.00994,-0.0177,0.9498,0.8496 -1.000,-0.1139,0.01757,0.01007,-0.0162,0.9442,0.8761 -0.750,-0.0840,0.01772,0.01019,-0.0161,0.9397,0.9012 -0.500,-0.0462,0.01786,0.01029,-0.0180,0.9366,0.9194 -0.250,-0.0078,0.01798,0.01035,-0.0202,0.9332,0.9337 0.000,0.0260,0.01806,0.01039,-0.0217,0.9275,0.9466 0.250,0.0683,0.01815,0.01045,-0.0250,0.9237,0.9560 0.500,0.1134,0.01821,0.01049,-0.0288,0.9208,0.9642 0.750,0.1517,0.01828,0.01055,-0.0314,0.9151,0.9740 1.000,0.1944,0.01830,0.01059,-0.0348,0.9097,0.9819 1.250,0.2423,0.01828,0.01059,-0.0392,0.9060,0.9876 1.500,0.2835,0.01827,0.01062,-0.0424,0.8992,0.9955 1.750,0.3239,0.01816,0.01056,-0.0452,0.8927,1.0000 2.000,0.3484,0.01798,0.01042,-0.0448,0.8826,1.0000 2.250,0.3983,0.01741,0.00992,-0.0486,0.8735,1.0000 2.500,0.4224,0.01688,0.00943,-0.0473,0.8546,1.0000 2.750,0.4512,0.01632,0.00891,-0.0467,0.8350,1.0000 3.000,0.4820,0.01582,0.00847,-0.0466,0.8156,1.0000 3.250,0.5054,0.01551,0.00821,-0.0452,0.7932,1.0000 3.500,0.5355,0.01514,0.00786,-0.0450,0.7651,1.0000 3.750,0.5713,0.01477,0.00747,-0.0457,0.7229,1.0000 4.000,0.6192,0.01452,0.00685,-0.0484,0.6269,1.0000 4.250,0.6408,0.01505,0.00673,-0.0467,0.5023,1.0000 4.500,0.6492,0.01591,0.00696,-0.0429,0.3886,1.0000 4.750,0.6587,0.01679,0.00733,-0.0397,0.2986,1.0000 5.000,0.6718,0.01759,0.00777,-0.0372,0.2337,1.0000 5.250,0.6867,0.01835,0.00824,-0.0351,0.1873,1.0000 5.500,0.7034,0.01904,0.00879,-0.0332,0.1564,1.0000 5.750,0.7205,0.01975,0.00935,-0.0314,0.1333,1.0000 6.000,0.7376,0.02047,0.00997,-0.0297,0.1171,1.0000 6.250,0.7557,0.02115,0.01065,-0.0281,0.1058,1.0000 6.500,0.7734,0.02191,0.01140,-0.0264,0.0980,1.0000 6.750,0.7920,0.02263,0.01214,-0.0249,0.0913,1.0000 7.000,0.8104,0.02343,0.01292,-0.0234,0.0861,1.0000 7.250,0.8304,0.02417,0.01374,-0.0221,0.0811,1.0000 7.500,0.8500,0.02499,0.01459,-0.0209,0.0775,1.0000 7.750,0.8701,0.02595,0.01554,-0.0198,0.0742,1.0000 8.000,0.8918,0.02681,0.01653,-0.0189,0.0702,1.0000 8.250,0.9125,0.02769,0.01745,-0.0180,0.0668,1.0000 8.500,0.9327,0.02880,0.01851,-0.0171,0.0638,1.0000 8.750,0.9549,0.02985,0.01979,-0.0163,0.0606,1.0000 9.000,0.9756,0.03094,0.02101,-0.0154,0.0575,1.0000 9.250,0.9950,0.03203,0.02213,-0.0145,0.0549,1.0000 9.500,1.0167,0.03367,0.02382,-0.0140,0.0528,1.0000 9.750,1.0370,0.03534,0.02582,-0.0130,0.0509,1.0000 10.000,1.0544,0.03702,0.02777,-0.0117,0.0487,1.0000 10.250,1.0694,0.03849,0.02944,-0.0102,0.0466,1.0000 10.500,1.0839,0.03996,0.03098,-0.0088,0.0449,1.0000 10.750,1.0990,0.04227,0.03339,-0.0077,0.0435,1.0000 11.000,1.1040,0.04464,0.03623,-0.0048,0.0425,1.0000 11.250,1.1042,0.04725,0.03928,-0.0016,0.0415,1.0000 11.500,1.0996,0.04993,0.04233,0.0021,0.0406,1.0000 11.750,1.0923,0.05258,0.04531,0.0056,0.0397,1.0000 12.000,1.0845,0.05512,0.04811,0.0088,0.0387,1.0000 12.250,1.0791,0.05739,0.05055,0.0112,0.0377,1.0000 12.500,1.0742,0.05961,0.05291,0.0133,0.0368,1.0000 12.750,1.0719,0.06174,0.05510,0.0148,0.0360,1.0000 13.000,1.0677,0.06449,0.05789,0.0159,0.0353,1.0000 13.250,1.0421,0.06920,0.06292,0.0170,0.0351,1.0000 13.500,1.0154,0.07469,0.06869,0.0166,0.0351,1.0000 13.750,0.9878,0.08111,0.07535,0.0145,0.0351,1.0000 14.000,0.9599,0.08863,0.08307,0.0107,0.0352,1.0000