Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-b737d-il-200000-n5 Airfoil,b737d-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,62.2832 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-b737d-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.000,-0.5229,0.08769,0.08429,-0.0208,1.0000,0.0227 -8.750,-0.5273,0.08185,0.07848,-0.0266,1.0000,0.0228 -8.500,-0.5358,0.07678,0.07340,-0.0310,1.0000,0.0227 -8.250,-0.5427,0.07267,0.06923,-0.0328,1.0000,0.0228 -8.000,-0.5445,0.06866,0.06515,-0.0341,1.0000,0.0231 -7.750,-0.5436,0.06486,0.06125,-0.0348,1.0000,0.0234 -7.500,-0.5406,0.06124,0.05752,-0.0350,1.0000,0.0237 -7.250,-0.5363,0.05784,0.05399,-0.0345,1.0000,0.0241 -7.000,-0.5277,0.05438,0.05037,-0.0344,0.9951,0.0247 -6.500,-0.4846,0.04419,0.03945,-0.0372,0.9651,0.0188 -6.250,-0.4631,0.04035,0.03531,-0.0380,0.9525,0.0178 -6.000,-0.4400,0.03702,0.03164,-0.0382,0.9406,0.0179 -5.750,-0.4160,0.03415,0.02837,-0.0378,0.9293,0.0189 -5.500,-0.3933,0.03135,0.02524,-0.0373,0.9186,0.0186 -5.000,-0.3469,0.02630,0.01952,-0.0357,0.8990,0.0173 -4.750,-0.3222,0.02406,0.01694,-0.0348,0.8905,0.0168 -4.500,-0.2969,0.02206,0.01461,-0.0339,0.8821,0.0165 -4.250,-0.2711,0.02036,0.01262,-0.0331,0.8744,0.0164 -4.000,-0.2452,0.01896,0.01099,-0.0324,0.8671,0.0165 -3.750,-0.2194,0.01777,0.00965,-0.0318,0.8599,0.0167 -3.500,-0.1941,0.01676,0.00851,-0.0311,0.8530,0.0172 -3.250,-0.1692,0.01587,0.00753,-0.0304,0.8462,0.0179 -3.000,-0.1447,0.01509,0.00666,-0.0297,0.8396,0.0189 -2.750,-0.1200,0.01449,0.00597,-0.0291,0.8334,0.0202 -2.500,-0.0958,0.01385,0.00535,-0.0286,0.8267,0.0237 -2.250,-0.0705,0.01345,0.00485,-0.0281,0.8214,0.0274 -2.000,-0.0450,0.01301,0.00438,-0.0278,0.8143,0.0334 -1.750,-0.0189,0.01271,0.00396,-0.0274,0.8083,0.0391 -1.500,0.0070,0.01233,0.00361,-0.0272,0.8016,0.0593 -1.250,0.0195,0.01009,0.00323,-0.0253,0.7948,0.5804 -1.000,0.0428,0.00986,0.00325,-0.0241,0.7883,0.6773 -0.750,0.0655,0.00972,0.00333,-0.0226,0.7813,0.7470 -0.500,0.0892,0.00967,0.00337,-0.0212,0.7752,0.7877 -0.250,0.1150,0.00965,0.00336,-0.0205,0.7678,0.8077 0.000,0.1418,0.00964,0.00328,-0.0202,0.7615,0.8201 0.250,0.1691,0.00963,0.00325,-0.0200,0.7538,0.8291 0.500,0.1962,0.00963,0.00320,-0.0197,0.7477,0.8393 0.750,0.2235,0.00963,0.00320,-0.0196,0.7397,0.8507 1.000,0.2508,0.00964,0.00319,-0.0194,0.7341,0.8622 1.250,0.2783,0.00965,0.00323,-0.0193,0.7275,0.8742 1.500,0.3061,0.00967,0.00325,-0.0192,0.7205,0.8870 1.750,0.3344,0.00969,0.00328,-0.0192,0.7116,0.9002 2.000,0.3633,0.00970,0.00328,-0.0193,0.7012,0.9137 2.250,0.3932,0.00971,0.00327,-0.0196,0.6875,0.9270 2.500,0.4245,0.00972,0.00328,-0.0203,0.6716,0.9399 2.750,0.4569,0.00975,0.00331,-0.0213,0.6572,0.9523 3.000,0.4904,0.00980,0.00336,-0.0225,0.6436,0.9639 3.250,0.5245,0.00985,0.00344,-0.0240,0.6270,0.9748 3.500,0.5591,0.00992,0.00352,-0.0256,0.6077,0.9851 3.750,0.5939,0.01002,0.00358,-0.0273,0.5829,0.9946 4.000,0.6249,0.01015,0.00365,-0.0282,0.5497,1.0000 4.250,0.6465,0.01038,0.00376,-0.0271,0.5093,1.0000 4.500,0.6667,0.01077,0.00390,-0.0258,0.4556,1.0000 4.750,0.6864,0.01128,0.00415,-0.0246,0.4015,1.0000 5.000,0.7062,0.01185,0.00448,-0.0235,0.3471,1.0000 5.250,0.7267,0.01241,0.00487,-0.0225,0.3125,1.0000 5.500,0.7486,0.01289,0.00527,-0.0218,0.2858,1.0000 5.750,0.7711,0.01333,0.00565,-0.0211,0.2556,1.0000 6.000,0.7922,0.01390,0.00605,-0.0203,0.2161,1.0000 6.250,0.8127,0.01456,0.00653,-0.0195,0.1802,1.0000 6.500,0.8342,0.01515,0.00702,-0.0189,0.1543,1.0000 6.750,0.8559,0.01571,0.00751,-0.0182,0.1318,1.0000 7.000,0.8779,0.01627,0.00802,-0.0176,0.1088,1.0000 7.250,0.8986,0.01694,0.00860,-0.0169,0.0845,1.0000 7.500,0.9183,0.01774,0.00932,-0.0160,0.0626,1.0000 7.750,0.9378,0.01858,0.01009,-0.0151,0.0474,1.0000 8.000,0.9574,0.01939,0.01094,-0.0141,0.0395,1.0000 8.250,0.9761,0.02028,0.01186,-0.0131,0.0344,1.0000 8.500,0.9944,0.02118,0.01285,-0.0120,0.0314,1.0000 8.750,1.0130,0.02201,0.01381,-0.0109,0.0285,1.0000 9.000,1.0300,0.02296,0.01484,-0.0098,0.0262,1.0000 9.250,1.0426,0.02431,0.01627,-0.0081,0.0244,1.0000 9.500,1.0580,0.02538,0.01747,-0.0067,0.0234,1.0000 9.750,1.0734,0.02642,0.01865,-0.0054,0.0219,1.0000 10.000,1.0871,0.02747,0.01982,-0.0039,0.0204,1.0000 10.250,1.0986,0.02865,0.02110,-0.0022,0.0193,1.0000 10.500,1.1084,0.03003,0.02260,-0.0005,0.0184,1.0000 10.750,1.1147,0.03190,0.02455,0.0014,0.0175,1.0000 11.000,1.1240,0.03354,0.02635,0.0029,0.0167,1.0000 11.250,1.1338,0.03502,0.02804,0.0043,0.0158,1.0000 11.500,1.1417,0.03669,0.02991,0.0056,0.0149,1.0000 11.750,1.1477,0.03862,0.03202,0.0068,0.0143,1.0000 12.000,1.1521,0.04071,0.03427,0.0080,0.0138,1.0000 12.250,1.1550,0.04294,0.03666,0.0089,0.0134,1.0000 12.500,1.1563,0.04536,0.03925,0.0097,0.0130,1.0000 12.750,1.1555,0.04807,0.04211,0.0103,0.0127,1.0000 13.000,1.1523,0.05118,0.04538,0.0107,0.0124,1.0000 13.250,1.1455,0.05485,0.04924,0.0108,0.0122,1.0000 13.500,1.1344,0.05924,0.05385,0.0106,0.0120,1.0000 13.750,1.1234,0.06372,0.05858,0.0096,0.0119,1.0000 14.000,1.1110,0.06863,0.06373,0.0081,0.0118,1.0000 14.250,1.0967,0.07412,0.06945,0.0058,0.0117,1.0000 14.500,1.0805,0.08032,0.07586,0.0028,0.0117,1.0000 14.750,1.0631,0.08729,0.08304,-0.0010,0.0117,1.0000 15.000,1.0444,0.09510,0.09100,-0.0056,0.0117,1.0000 15.250,1.0245,0.10378,0.09986,-0.0108,0.0118,1.0000 15.500,1.0036,0.11318,0.10941,-0.0165,0.0119,1.0000 15.750,0.9816,0.12327,0.11962,-0.0225,0.0120,1.0000 16.000,0.6852,0.13329,0.13007,-0.0133,0.0157,1.0000