Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-cp-180-050-gn-200000-n5 Airfoil,cp-180-050-gn Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,29.6306 Max Cl/Cd alpha,7 Url,http://airfoiltools.com/polar/csv?polar=xf-cp-180-050-gn-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -13.250,0.2101,0.14398,0.13953,-0.1725,0.8587,0.0194 -13.000,0.2143,0.14223,0.13777,-0.1723,0.8563,0.0196 -12.750,0.2228,0.13992,0.13544,-0.1735,0.8548,0.0197 -11.750,0.2252,0.13467,0.13022,-0.1687,0.8418,0.0201 -11.500,0.2325,0.13266,0.12820,-0.1693,0.8401,0.0204 -11.250,0.2423,0.13040,0.12592,-0.1706,0.8389,0.0207 -11.000,0.2534,0.12800,0.12349,-0.1722,0.8379,0.0211 -10.750,0.2658,0.12545,0.12092,-0.1742,0.8371,0.0215 -10.500,0.2612,0.12484,0.12032,-0.1713,0.8330,0.0218 -10.250,0.2859,0.12096,0.11638,-0.1767,0.8346,0.0223 -9.250,0.2335,0.12210,0.11768,-0.1567,0.8102,0.0228 -8.750,0.2422,0.10988,0.10574,-0.1417,0.7873,0.0231 -8.250,0.2256,0.11822,0.11385,-0.1489,0.7955,0.0230 -8.000,0.2309,0.11645,0.11207,-0.1487,0.7935,0.0233 -7.750,0.2385,0.11452,0.11012,-0.1490,0.7921,0.0236 -7.500,0.2473,0.11247,0.10806,-0.1497,0.7911,0.0239 -7.250,0.2150,0.11492,0.11060,-0.1402,0.7806,0.0240 -7.000,0.2179,0.11341,0.10908,-0.1394,0.7781,0.0243 -6.750,0.2238,0.11161,0.10727,-0.1394,0.7765,0.0247 -6.500,0.2305,0.10971,0.10535,-0.1395,0.7753,0.0253 -6.250,0.2378,0.10779,0.10341,-0.1398,0.7744,0.0256 -5.250,0.1667,0.11064,0.10645,-0.1177,0.7478,0.0257 -5.000,0.1717,0.10895,0.10475,-0.1176,0.7456,0.0258 -4.750,0.1808,0.10686,0.10264,-0.1185,0.7441,0.0258 -4.250,0.1884,0.10348,0.09925,-0.1174,0.7392,0.0260 -4.000,0.2133,0.09981,0.09553,-0.1213,0.7408,0.0264 -3.250,0.1684,0.10181,0.09768,-0.1078,0.7175,0.0268 -3.000,0.1769,0.10017,0.09604,-0.1084,0.7146,0.0275 -2.750,0.1924,0.09790,0.09374,-0.1104,0.7129,0.0282 -2.500,0.2114,0.09539,0.09120,-0.1132,0.7117,0.0285 -2.250,0.2339,0.09274,0.08850,-0.1167,0.7108,0.0287 -2.000,0.2136,0.09442,0.09025,-0.1116,0.7005,0.0287 -1.750,0.2339,0.09235,0.08815,-0.1148,0.6982,0.0288 -1.500,0.2611,0.08992,0.08567,-0.1195,0.6968,0.0289 -1.250,0.2905,0.08725,0.08297,-0.1245,0.6958,0.0289 -1.000,0.3113,0.08446,0.08014,-0.1268,0.6949,0.0292 -0.750,0.3395,0.08196,0.07760,-0.1308,0.6942,0.0299 -0.500,0.3734,0.07935,0.07494,-0.1362,0.6937,0.0307 -0.250,0.4125,0.07668,0.07221,-0.1427,0.6933,0.0314 0.250,0.4356,0.07684,0.07238,-0.1454,0.6798,0.0318 0.500,0.4896,0.07445,0.06990,-0.1552,0.6793,0.0319 0.750,0.5253,0.07178,0.06720,-0.1603,0.6786,0.0322 1.000,0.5618,0.06952,0.06489,-0.1653,0.6781,0.0328 1.250,0.6075,0.06739,0.06270,-0.1724,0.6777,0.0335 1.500,0.6576,0.06533,0.06057,-0.1804,0.6774,0.0344 1.750,0.7185,0.06345,0.05860,-0.1906,0.6771,0.0352 2.250,0.8124,0.05999,0.05504,-0.2044,0.6755,0.0362 2.500,0.8679,0.05796,0.05294,-0.2125,0.6760,0.0371 3.500,0.8589,0.06015,0.05547,-0.1975,0.6301,0.0394 4.000,1.0886,0.05666,0.05148,-0.2396,0.6575,0.0427 5.000,1.2295,0.05708,0.05184,-0.2538,0.6459,0.0482 5.250,1.2928,0.05685,0.05148,-0.2618,0.6454,0.0494 5.500,1.3265,0.05532,0.04999,-0.2641,0.6449,0.0504 6.000,1.4134,0.05320,0.04767,-0.2711,0.6290,0.0560 6.250,1.4189,0.05426,0.04877,-0.2689,0.6168,0.0571 6.500,1.4569,0.05309,0.04749,-0.2711,0.6023,0.0597 6.750,1.5036,0.05297,0.04711,-0.2747,0.5844,0.0630 7.000,1.5319,0.05170,0.04561,-0.2753,0.5506,0.0645 7.250,1.5329,0.05331,0.04664,-0.2718,0.4793,0.0657 7.500,1.5040,0.05818,0.05105,-0.2648,0.4094,0.0659 7.750,1.4724,0.06382,0.05629,-0.2582,0.3386,0.0659 8.000,1.4420,0.06971,0.06176,-0.2522,0.2550,0.0659 8.250,1.4124,0.07582,0.06741,-0.2468,0.1462,0.0659 8.500,1.3963,0.08084,0.07209,-0.2432,0.0389,0.0666 9.000,1.4291,0.08482,0.07601,-0.2430,0.0290,0.0740 9.250,1.4420,0.08661,0.07786,-0.2424,0.0278,0.0785 9.500,1.4627,0.08866,0.07984,-0.2427,0.0268,0.0835 9.750,1.4757,0.09051,0.08176,-0.2422,0.0260,0.0846 10.000,1.5034,0.09250,0.08354,-0.2435,0.0253,0.0543 10.250,1.5165,0.09468,0.08573,-0.2429,0.0248,0.0534 10.500,1.5293,0.09694,0.08797,-0.2423,0.0243,0.0530 10.750,1.5407,0.09941,0.09037,-0.2416,0.0240,0.0547 11.000,1.5484,0.10222,0.09318,-0.2406,0.0236,0.0548 11.250,1.5571,0.10479,0.09574,-0.2397,0.0232,0.0546 11.500,1.5655,0.10729,0.09824,-0.2387,0.0227,0.0545 11.750,1.5724,0.10986,0.10082,-0.2376,0.0222,0.0545 12.000,1.5784,0.11243,0.10342,-0.2364,0.0217,0.0546 12.250,1.5832,0.11512,0.10613,-0.2352,0.0214,0.0549 12.500,1.5877,0.11780,0.10884,-0.2339,0.0212,0.0553 12.750,1.5927,0.12038,0.11146,-0.2327,0.0209,0.0559 13.000,1.5977,0.12292,0.11406,-0.2316,0.0207,0.0568 13.250,1.6034,0.12535,0.11652,-0.2305,0.0205,0.0582 13.500,1.6098,0.12760,0.11882,-0.2294,0.0203,0.0609 13.750,1.6171,0.12968,0.12093,-0.2284,0.0200,0.0649 14.000,1.6252,0.13159,0.12286,-0.2275,0.0198,0.0694