Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-b737c-il-100000-n5 Airfoil,b737c-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,47.0684 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-b737c-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.4221,0.08931,0.08480,-0.0204,1.0000,0.0532 -9.000,-0.4262,0.08479,0.08031,-0.0221,1.0000,0.0535 -8.750,-0.4317,0.08007,0.07563,-0.0241,1.0000,0.0537 -8.500,-0.4394,0.07507,0.07067,-0.0268,1.0000,0.0537 -8.250,-0.4519,0.06968,0.06530,-0.0305,1.0000,0.0538 -8.000,-0.4672,0.06509,0.06071,-0.0326,1.0000,0.0538 -7.750,-0.4807,0.06103,0.05662,-0.0328,1.0000,0.0537 -7.500,-0.4896,0.05681,0.05233,-0.0328,1.0000,0.0536 -7.250,-0.4956,0.05261,0.04803,-0.0322,1.0000,0.0532 -6.750,-0.5386,0.05497,0.04928,-0.0277,1.0000,0.0327 -6.500,-0.5321,0.05127,0.04547,-0.0264,1.0000,0.0312 -6.250,-0.5238,0.04794,0.04192,-0.0247,1.0000,0.0302 -6.000,-0.5133,0.04498,0.03870,-0.0228,1.0000,0.0304 -5.750,-0.5012,0.04219,0.03558,-0.0209,1.0000,0.0308 -5.500,-0.4881,0.03939,0.03249,-0.0189,1.0000,0.0305 -5.250,-0.4738,0.03654,0.02934,-0.0168,1.0000,0.0293 -5.000,-0.4577,0.03382,0.02627,-0.0148,1.0000,0.0282 -4.750,-0.4398,0.03126,0.02333,-0.0128,1.0000,0.0273 -4.500,-0.4175,0.02879,0.02046,-0.0115,0.9988,0.0266 -4.250,-0.3811,0.02624,0.01747,-0.0130,0.9923,0.0261 -4.000,-0.3435,0.02411,0.01501,-0.0147,0.9857,0.0261 -3.750,-0.3066,0.02229,0.01297,-0.0163,0.9779,0.0265 -3.500,-0.2697,0.02105,0.01161,-0.0182,0.9691,0.0287 -3.250,-0.2333,0.01988,0.01035,-0.0199,0.9595,0.0314 -3.000,-0.1996,0.01864,0.00905,-0.0209,0.9485,0.0327 -2.750,-0.1685,0.01764,0.00799,-0.0216,0.9352,0.0349 -2.500,-0.1389,0.01700,0.00732,-0.0221,0.9188,0.0401 -2.250,-0.1096,0.01638,0.00654,-0.0223,0.9010,0.0444 -2.000,-0.0799,0.01582,0.00583,-0.0225,0.8833,0.0520 -1.750,-0.0500,0.01532,0.00521,-0.0228,0.8663,0.0708 -1.500,-0.0301,0.01315,0.00474,-0.0222,0.8499,0.5074 -1.250,-0.0046,0.01266,0.00456,-0.0213,0.8352,0.6267 -1.000,0.0206,0.01231,0.00453,-0.0200,0.8224,0.7142 -0.750,0.0492,0.01222,0.00462,-0.0190,0.8114,0.7982 -0.500,0.0804,0.01232,0.00473,-0.0186,0.8009,0.8797 -0.250,0.1143,0.01241,0.00472,-0.0192,0.7909,0.9143 0.000,0.1509,0.01249,0.00468,-0.0207,0.7813,0.9401 0.250,0.2135,0.01259,0.00467,-0.0274,0.7729,0.9770 0.500,0.2609,0.01258,0.00454,-0.0316,0.7624,0.9903 0.750,0.3000,0.01258,0.00443,-0.0342,0.7511,0.9988 1.000,0.3263,0.01263,0.00439,-0.0341,0.7407,1.0000 1.250,0.3504,0.01271,0.00439,-0.0336,0.7307,1.0000 1.500,0.3746,0.01280,0.00444,-0.0331,0.7210,1.0000 1.750,0.3987,0.01291,0.00449,-0.0325,0.7115,1.0000 2.000,0.4226,0.01303,0.00458,-0.0317,0.7004,1.0000 2.250,0.4461,0.01316,0.00467,-0.0310,0.6874,1.0000 2.500,0.4694,0.01329,0.00478,-0.0301,0.6739,1.0000 2.750,0.4928,0.01343,0.00491,-0.0293,0.6605,1.0000 3.000,0.5162,0.01358,0.00510,-0.0285,0.6472,1.0000 3.250,0.5396,0.01373,0.00526,-0.0276,0.6339,1.0000 3.500,0.5630,0.01388,0.00544,-0.0267,0.6198,1.0000 3.750,0.5862,0.01404,0.00563,-0.0258,0.6049,1.0000 4.000,0.6092,0.01420,0.00585,-0.0248,0.5884,1.0000 4.250,0.6320,0.01439,0.00604,-0.0237,0.5695,1.0000 4.500,0.6539,0.01453,0.00628,-0.0226,0.5428,1.0000 4.750,0.6760,0.01458,0.00658,-0.0216,0.4902,1.0000 5.000,0.6952,0.01477,0.00637,-0.0196,0.4490,1.0000 5.250,0.7159,0.01521,0.00675,-0.0184,0.4065,1.0000 5.500,0.7356,0.01576,0.00715,-0.0170,0.3590,1.0000 5.750,0.7551,0.01639,0.00764,-0.0158,0.3177,1.0000 6.000,0.7746,0.01706,0.00819,-0.0146,0.2767,1.0000 6.250,0.7940,0.01777,0.00882,-0.0134,0.2389,1.0000 6.500,0.8127,0.01857,0.00947,-0.0122,0.2034,1.0000 6.750,0.8320,0.01935,0.01018,-0.0112,0.1712,1.0000 7.000,0.8513,0.02017,0.01093,-0.0101,0.1420,1.0000 7.250,0.8702,0.02105,0.01174,-0.0091,0.1152,1.0000 7.500,0.8882,0.02206,0.01268,-0.0080,0.0921,1.0000 7.750,0.9057,0.02314,0.01375,-0.0067,0.0743,1.0000 8.000,0.9227,0.02427,0.01492,-0.0055,0.0606,1.0000 8.250,0.9383,0.02555,0.01619,-0.0041,0.0519,1.0000 8.500,0.9546,0.02680,0.01765,-0.0026,0.0461,1.0000 8.750,0.9689,0.02824,0.01917,-0.0010,0.0421,1.0000 9.000,0.9826,0.02997,0.02101,0.0007,0.0394,1.0000 9.250,0.9987,0.03150,0.02278,0.0020,0.0361,1.0000 9.500,1.0132,0.03293,0.02437,0.0033,0.0326,1.0000 9.750,1.0256,0.03488,0.02644,0.0048,0.0305,1.0000 10.000,1.0375,0.03723,0.02902,0.0062,0.0283,1.0000 10.250,1.0487,0.03911,0.03124,0.0078,0.0257,1.0000 10.500,1.0569,0.04143,0.03385,0.0094,0.0241,1.0000 10.750,1.0609,0.04363,0.03628,0.0114,0.0227,1.0000 11.000,1.0621,0.04573,0.03852,0.0132,0.0215,1.0000 11.250,1.0588,0.04863,0.04155,0.0148,0.0204,1.0000 11.500,1.0515,0.05196,0.04518,0.0161,0.0196,1.0000 11.750,1.0431,0.05536,0.04891,0.0168,0.0191,1.0000 12.000,1.0317,0.05940,0.05327,0.0166,0.0186,1.0000 12.250,1.0178,0.06410,0.05825,0.0153,0.0184,1.0000 12.500,1.0016,0.06950,0.06390,0.0131,0.0183,1.0000 12.750,0.9834,0.07565,0.07028,0.0100,0.0183,1.0000 13.000,0.9636,0.08256,0.07738,0.0060,0.0185,1.0000 13.250,0.9424,0.09048,0.08545,0.0010,0.0187,1.0000 13.500,0.9209,0.09930,0.09439,-0.0047,0.0192,1.0000 13.750,0.8998,0.10869,0.10386,-0.0104,0.0196,1.0000