Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-b737a-il-50000-n5 Airfoil,b737a-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,19.4184 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-b737a-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.750,-0.7059,0.10545,0.09660,0.0039,1.0000,0.1675 -12.500,-0.6884,0.10497,0.09609,0.0049,1.0000,0.1726 -12.250,-0.7164,0.09618,0.08727,-0.0004,1.0000,0.1764 -12.000,-0.7088,0.09375,0.08482,-0.0008,1.0000,0.1797 -11.750,-0.6973,0.09202,0.08308,-0.0007,1.0000,0.1835 -11.500,-0.7410,0.07995,0.07095,-0.0086,1.0000,0.1863 -11.250,-0.8631,0.05980,0.05053,-0.0210,1.0000,0.1849 -11.000,-0.8949,0.05434,0.04481,-0.0210,1.0000,0.1864 -10.750,-0.9107,0.05018,0.04029,-0.0205,1.0000,0.1888 -10.500,-0.9010,0.04848,0.03848,-0.0196,1.0000,0.1917 -10.250,-0.8789,0.04817,0.03822,-0.0187,1.0000,0.1954 -10.000,-0.8686,0.04650,0.03640,-0.0178,1.0000,0.1991 -9.750,-0.8632,0.04414,0.03373,-0.0169,1.0000,0.2026 -9.500,-0.8501,0.04241,0.03182,-0.0160,1.0000,0.2055 -9.250,-0.8285,0.04149,0.03092,-0.0153,1.0000,0.2078 -9.000,-0.8095,0.04022,0.02958,-0.0145,1.0000,0.2099 -8.750,-0.7912,0.03879,0.02802,-0.0137,1.0000,0.2120 -8.500,-0.7728,0.03734,0.02642,-0.0130,1.0000,0.2143 -8.250,-0.7543,0.03590,0.02479,-0.0122,1.0000,0.2169 -8.000,-0.7358,0.03445,0.02311,-0.0114,1.0000,0.2199 -7.750,-0.7133,0.03345,0.02213,-0.0106,1.0000,0.2222 -7.500,-0.6907,0.03256,0.02128,-0.0098,1.0000,0.2249 -7.250,-0.6687,0.03164,0.02035,-0.0090,1.0000,0.2282 -7.000,-0.6473,0.03069,0.01933,-0.0081,1.0000,0.2325 -6.750,-0.6267,0.02970,0.01817,-0.0072,1.0000,0.2377 -6.500,-0.6043,0.02899,0.01762,-0.0063,1.0000,0.2417 -6.250,-0.5832,0.02830,0.01698,-0.0052,1.0000,0.2471 -6.000,-0.5632,0.02761,0.01622,-0.0040,1.0000,0.2540 -5.750,-0.5433,0.02700,0.01571,-0.0028,1.0000,0.2600 -5.500,-0.5245,0.02649,0.01529,-0.0015,1.0000,0.2668 -5.250,-0.5069,0.02602,0.01475,-0.0001,1.0000,0.2748 -5.000,-0.4900,0.02561,0.01448,0.0014,1.0000,0.2814 -4.750,-0.4739,0.02527,0.01419,0.0030,1.0000,0.2892 -4.500,-0.4575,0.02498,0.01387,0.0044,1.0000,0.2973 -4.250,-0.4316,0.02467,0.01370,0.0041,0.9951,0.3059 -4.000,-0.3900,0.02439,0.01342,0.0011,0.9820,0.3187 -3.750,-0.3421,0.02403,0.01322,-0.0029,0.9650,0.3337 -3.500,-0.2889,0.02355,0.01290,-0.0073,0.9395,0.3492 -3.250,-0.2357,0.02299,0.01245,-0.0111,0.9079,0.3661 -2.750,-0.1557,0.02211,0.01178,-0.0136,0.8509,0.3991 -2.500,-0.1262,0.02180,0.01161,-0.0131,0.8262,0.4190 -2.250,-0.0998,0.02153,0.01150,-0.0119,0.8007,0.4440 -2.000,-0.0757,0.02129,0.01147,-0.0101,0.7743,0.4756 -1.750,-0.0539,0.02112,0.01155,-0.0078,0.7460,0.5155 -1.500,-0.0328,0.02105,0.01173,-0.0051,0.7144,0.5609 -1.250,-0.0117,0.02106,0.01183,-0.0023,0.6795,0.6068 -1.000,0.0087,0.02110,0.01187,0.0004,0.6376,0.6486 -0.750,0.0290,0.02118,0.01189,0.0034,0.5859,0.6824 -0.500,0.0488,0.02134,0.01178,0.0062,0.5233,0.7130 -0.250,0.0685,0.02162,0.01172,0.0089,0.4607,0.7389 0.000,0.0889,0.02202,0.01176,0.0112,0.4155,0.7616 0.250,0.1104,0.02244,0.01190,0.0130,0.3847,0.7825 0.500,0.1331,0.02284,0.01210,0.0146,0.3623,0.8025 1.000,0.1846,0.02362,0.01265,0.0166,0.3303,0.8395 1.250,0.2132,0.02404,0.01297,0.0171,0.3181,0.8576 1.500,0.2447,0.02448,0.01336,0.0172,0.3067,0.8786 1.750,0.2810,0.02502,0.01383,0.0164,0.2966,0.9020 2.000,0.3230,0.02560,0.01437,0.0144,0.2858,0.9268 2.250,0.3737,0.02631,0.01498,0.0107,0.2764,0.9488 2.500,0.4271,0.02695,0.01563,0.0060,0.2661,0.9673 2.750,0.4746,0.02763,0.01609,0.0022,0.2586,0.9826 3.000,0.5168,0.02824,0.01687,-0.0010,0.2504,0.9958 3.250,0.5412,0.02876,0.01738,-0.0012,0.2445,1.0000 3.500,0.5575,0.02930,0.01779,0.0003,0.2404,1.0000 3.750,0.5722,0.02994,0.01849,0.0018,0.2360,1.0000 4.000,0.5860,0.03061,0.01927,0.0036,0.2311,1.0000 4.250,0.6013,0.03129,0.01997,0.0051,0.2267,1.0000 4.500,0.6187,0.03198,0.02058,0.0064,0.2229,1.0000 4.750,0.6377,0.03284,0.02134,0.0075,0.2193,1.0000 5.000,0.6545,0.03395,0.02266,0.0086,0.2148,1.0000 5.250,0.6735,0.03504,0.02386,0.0094,0.2106,1.0000 5.500,0.6942,0.03605,0.02486,0.0101,0.2069,1.0000 5.750,0.7166,0.03701,0.02573,0.0106,0.2039,1.0000 6.000,0.7351,0.03846,0.02732,0.0112,0.2007,1.0000 6.250,0.7500,0.04028,0.02942,0.0120,0.1972,1.0000 6.500,0.7662,0.04197,0.03127,0.0126,0.1939,1.0000 6.750,0.7838,0.04348,0.03287,0.0132,0.1910,1.0000 7.000,0.8033,0.04482,0.03422,0.0137,0.1885,1.0000 7.250,0.8249,0.04610,0.03544,0.0140,0.1864,1.0000 7.500,0.8257,0.04936,0.03912,0.0148,0.1840,1.0000 7.750,0.8215,0.05308,0.04320,0.0154,0.1817,1.0000 8.000,0.8120,0.05719,0.04760,0.0157,0.1794,1.0000 8.250,0.7948,0.06192,0.05254,0.0154,0.1774,1.0000 8.500,0.7610,0.06813,0.05893,0.0140,0.1756,1.0000 8.750,0.7225,0.07663,0.06754,0.0092,0.1737,1.0000 9.000,0.7191,0.08119,0.07211,0.0071,0.1722,1.0000 9.250,0.6852,0.09196,0.08293,0.0002,0.1708,1.0000 9.500,0.6479,0.10306,0.09407,-0.0070,0.1696,1.0000