Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-b737c-il-50000-n5 Airfoil,b737c-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,34.0968 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-b737c-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.750,-0.5570,0.09767,0.09121,-0.0169,1.0000,0.1318 -8.500,-0.5425,0.09408,0.08762,-0.0146,1.0000,0.1376 -8.250,-0.5681,0.08984,0.08350,-0.0206,1.0000,0.1464 -8.000,-0.5531,0.08620,0.07988,-0.0185,1.0000,0.1531 -7.500,-0.4928,0.06058,0.05413,-0.0325,1.0000,0.0576 -7.250,-0.5520,0.06778,0.06070,-0.0293,1.0000,0.0574 -7.000,-0.5462,0.06375,0.05656,-0.0289,1.0000,0.0540 -6.750,-0.5439,0.06078,0.05273,-0.0275,1.0000,0.0475 -6.500,-0.5320,0.05646,0.04848,-0.0268,1.0000,0.0463 -6.250,-0.5218,0.05302,0.04488,-0.0256,1.0000,0.0454 -6.000,-0.5105,0.04985,0.04141,-0.0242,1.0000,0.0445 -5.750,-0.4979,0.04686,0.03814,-0.0227,1.0000,0.0437 -5.500,-0.4838,0.04405,0.03501,-0.0210,1.0000,0.0430 -5.250,-0.4681,0.04142,0.03203,-0.0194,1.0000,0.0426 -5.000,-0.4509,0.03905,0.02930,-0.0178,1.0000,0.0431 -4.750,-0.4323,0.03693,0.02678,-0.0162,1.0000,0.0443 -4.500,-0.4122,0.03497,0.02443,-0.0146,1.0000,0.0455 -4.250,-0.3910,0.03308,0.02220,-0.0132,1.0000,0.0460 -4.000,-0.3688,0.03125,0.02010,-0.0118,1.0000,0.0463 -3.750,-0.3458,0.02963,0.01818,-0.0106,1.0000,0.0468 -3.500,-0.3224,0.02815,0.01655,-0.0094,1.0000,0.0479 -3.250,-0.3004,0.02673,0.01520,-0.0084,1.0000,0.0516 -3.000,-0.2787,0.02572,0.01411,-0.0071,1.0000,0.0552 -2.750,-0.2581,0.02483,0.01308,-0.0056,1.0000,0.0576 -2.500,-0.2394,0.02414,0.01219,-0.0041,1.0000,0.0600 -2.250,-0.2038,0.02299,0.01092,-0.0064,0.9908,0.0658 -2.000,-0.1655,0.02205,0.00979,-0.0091,0.9796,0.0779 -1.750,-0.1283,0.02068,0.00871,-0.0118,0.9687,0.1363 -1.500,-0.1091,0.01813,0.00924,-0.0077,0.9638,0.8186 -1.250,-0.0300,0.01850,0.00928,-0.0151,0.9678,0.9708 -1.000,0.0429,0.01845,0.00883,-0.0247,0.9649,1.0000 -0.750,0.0840,0.01845,0.00856,-0.0284,0.9506,1.0000 -0.500,0.1205,0.01847,0.00838,-0.0311,0.9355,1.0000 -0.250,0.1541,0.01852,0.00827,-0.0330,0.9210,1.0000 0.000,0.1857,0.01858,0.00819,-0.0345,0.9064,1.0000 0.250,0.2161,0.01865,0.00814,-0.0355,0.8928,1.0000 0.500,0.2457,0.01875,0.00814,-0.0364,0.8806,1.0000 0.750,0.2724,0.01888,0.00819,-0.0366,0.8678,1.0000 1.000,0.2993,0.01899,0.00825,-0.0367,0.8549,1.0000 1.250,0.3262,0.01909,0.00829,-0.0367,0.8420,1.0000 1.500,0.3530,0.01917,0.00834,-0.0365,0.8285,1.0000 1.750,0.3790,0.01926,0.00841,-0.0361,0.8153,1.0000 2.000,0.4043,0.01940,0.00856,-0.0356,0.8026,1.0000 2.250,0.4293,0.01955,0.00872,-0.0350,0.7902,1.0000 2.500,0.4540,0.01971,0.00889,-0.0343,0.7772,1.0000 2.750,0.4785,0.01985,0.00907,-0.0334,0.7630,1.0000 3.000,0.5028,0.01998,0.00927,-0.0323,0.7474,1.0000 3.250,0.5277,0.02010,0.00941,-0.0312,0.7307,1.0000 3.500,0.5516,0.02024,0.00960,-0.0299,0.7128,1.0000 3.750,0.5740,0.02045,0.00987,-0.0285,0.6932,1.0000 4.000,0.5975,0.02062,0.01011,-0.0271,0.6737,1.0000 4.250,0.6201,0.02083,0.01045,-0.0257,0.6529,1.0000 4.500,0.6421,0.02104,0.01076,-0.0241,0.6304,1.0000 4.750,0.6640,0.02125,0.01107,-0.0225,0.6065,1.0000 5.000,0.6862,0.02142,0.01133,-0.0209,0.5808,1.0000 5.250,0.7059,0.02167,0.01176,-0.0191,0.5489,1.0000 5.500,0.7221,0.02196,0.01236,-0.0171,0.5011,1.0000 5.750,0.7420,0.02187,0.01208,-0.0147,0.4579,1.0000 6.000,0.7607,0.02231,0.01233,-0.0126,0.4111,1.0000 6.250,0.7782,0.02304,0.01289,-0.0108,0.3630,1.0000 6.500,0.7949,0.02397,0.01370,-0.0090,0.3183,1.0000 6.750,0.8110,0.02502,0.01466,-0.0074,0.2771,1.0000 7.000,0.8265,0.02618,0.01572,-0.0059,0.2390,1.0000 7.250,0.8408,0.02746,0.01687,-0.0043,0.2047,1.0000 7.500,0.8549,0.02883,0.01814,-0.0028,0.1737,1.0000 7.750,0.8691,0.03027,0.01959,-0.0013,0.1470,1.0000 8.000,0.8831,0.03177,0.02111,0.0002,0.1227,1.0000 8.250,0.8970,0.03343,0.02274,0.0017,0.1058,1.0000 8.500,0.9108,0.03515,0.02444,0.0031,0.0912,1.0000 9.000,0.9452,0.03905,0.02880,0.0056,0.0710,1.0000 9.250,0.9592,0.04103,0.03077,0.0067,0.0640,1.0000 9.500,0.9755,0.04348,0.03367,0.0080,0.0583,1.0000 9.750,0.9900,0.04603,0.03644,0.0091,0.0549,1.0000 10.000,1.0037,0.04911,0.03962,0.0101,0.0523,1.0000 10.250,1.0079,0.05264,0.04378,0.0118,0.0504,1.0000 10.500,1.0055,0.05612,0.04773,0.0136,0.0482,1.0000 10.750,0.9986,0.05934,0.05127,0.0154,0.0463,1.0000 11.000,0.9895,0.06265,0.05483,0.0167,0.0448,1.0000 11.250,0.9779,0.06639,0.05879,0.0173,0.0439,1.0000 11.500,0.9626,0.07085,0.06349,0.0167,0.0435,1.0000 11.750,0.9420,0.07647,0.06933,0.0147,0.0436,1.0000 12.000,0.9124,0.08434,0.07745,0.0102,0.0449,1.0000 12.250,0.8776,0.09471,0.08792,0.0034,0.0475,1.0000