Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ah7476-il-50000 Airfoil,ah7476-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,48.0899 Max Cl/Cd alpha,6.5 Url,http://airfoiltools.com/polar/csv?polar=xf-ah7476-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.250,-0.3443,0.12114,0.11430,-0.0249,1.0000,0.1073 -8.000,-0.3586,0.12186,0.11517,-0.0234,1.0000,0.1082 -7.750,-0.3708,0.12277,0.11623,-0.0238,1.0000,0.1087 -7.500,-0.3458,0.11344,0.10680,-0.0206,1.0000,0.1142 -7.250,-0.3496,0.11175,0.10519,-0.0189,1.0000,0.1177 -7.000,-0.3554,0.11089,0.10444,-0.0187,1.0000,0.1210 -6.750,-0.3615,0.11152,0.10519,-0.0218,1.0000,0.1228 -6.500,-0.3560,0.10631,0.10002,-0.0185,1.0000,0.1255 -6.250,-0.3518,0.10314,0.09688,-0.0166,1.0000,0.1304 -6.000,-0.3499,0.10168,0.09549,-0.0184,1.0000,0.1358 -5.750,-0.3439,0.10005,0.09393,-0.0231,1.0000,0.1387 -5.500,-0.3409,0.09583,0.08974,-0.0180,1.0000,0.1446 -5.250,-0.3229,0.09516,0.08910,-0.0287,1.0000,0.1528 -5.000,-0.3252,0.09049,0.08448,-0.0209,1.0000,0.1577 -4.750,-0.3034,0.08853,0.08249,-0.0297,1.0000,0.1678 -4.500,-0.3021,0.08474,0.07876,-0.0245,1.0000,0.1734 -4.250,-0.2799,0.08191,0.07591,-0.0309,1.0000,0.1838 -4.000,-0.2536,0.07919,0.07315,-0.0374,1.0000,0.1974 -3.750,-0.2293,0.07631,0.07023,-0.0419,1.0000,0.2120 -3.500,-0.2095,0.07314,0.06705,-0.0441,1.0000,0.2271 -3.250,-0.1954,0.06984,0.06377,-0.0438,1.0000,0.2430 -2.750,-0.1548,0.06400,0.05792,-0.0468,1.0000,0.2886 -1.000,-0.0936,0.04710,0.04150,-0.0222,1.0000,0.6347 -0.750,-0.0904,0.04470,0.03919,-0.0166,1.0000,0.6925 -0.500,0.3113,0.03939,0.03070,-0.1214,1.0000,0.1940 -0.250,0.3556,0.03804,0.02889,-0.1254,1.0000,0.1775 0.000,0.3970,0.03710,0.02745,-0.1286,1.0000,0.1643 0.250,0.4336,0.03643,0.02645,-0.1309,1.0000,0.1571 0.500,0.4671,0.03630,0.02587,-0.1324,1.0000,0.1526 0.750,0.4977,0.03624,0.02560,-0.1337,1.0000,0.1521 1.000,0.5254,0.03638,0.02555,-0.1343,1.0000,0.1531 1.250,0.5526,0.03665,0.02576,-0.1350,1.0000,0.1577 1.500,0.5784,0.03723,0.02628,-0.1358,1.0000,0.1677 1.750,0.6053,0.03792,0.02704,-0.1370,1.0000,0.1829 2.000,0.6336,0.03877,0.02805,-0.1387,1.0000,0.2097 2.250,0.6791,0.03813,0.02884,-0.1431,0.9904,1.0000 2.500,0.7381,0.03932,0.02961,-0.1500,0.9711,1.0000 2.750,0.7829,0.04020,0.03036,-0.1544,0.9477,1.0000 3.000,0.8290,0.04090,0.03101,-0.1586,0.9259,1.0000 3.250,0.8758,0.04137,0.03146,-0.1626,0.9051,1.0000 3.500,0.9155,0.04178,0.03190,-0.1651,0.8832,1.0000 3.750,0.9600,0.04186,0.03208,-0.1679,0.8630,1.0000 4.000,1.0031,0.04171,0.03202,-0.1701,0.8428,1.0000 4.250,1.0446,0.04117,0.03160,-0.1713,0.8206,1.0000 4.500,1.1014,0.03934,0.03000,-0.1736,0.8022,1.0000 4.750,1.1354,0.03860,0.02943,-0.1729,0.7790,1.0000 5.000,1.1887,0.03659,0.02766,-0.1743,0.7605,1.0000 5.250,1.2382,0.03470,0.02607,-0.1750,0.7404,1.0000 5.500,1.2793,0.03331,0.02491,-0.1746,0.7160,1.0000 5.750,1.3209,0.03185,0.02372,-0.1741,0.6881,1.0000 6.000,1.3671,0.03021,0.02222,-0.1739,0.6550,1.0000 6.250,1.4001,0.02949,0.02148,-0.1718,0.6111,1.0000 6.500,1.4225,0.02958,0.02143,-0.1685,0.5597,1.0000 6.750,1.4428,0.03013,0.02178,-0.1652,0.5069,1.0000 7.000,1.4595,0.03129,0.02279,-0.1620,0.4559,1.0000 7.250,1.4732,0.03264,0.02393,-0.1584,0.4041,1.0000 7.500,1.4818,0.03405,0.02517,-0.1541,0.3529,1.0000 7.750,1.4827,0.03536,0.02628,-0.1487,0.3020,1.0000 8.000,1.4791,0.03690,0.02733,-0.1431,0.2533,1.0000 8.250,1.4770,0.03923,0.02936,-0.1382,0.2056,1.0000 8.500,1.4836,0.04243,0.03221,-0.1346,0.1615,1.0000 8.750,1.4975,0.04576,0.03536,-0.1320,0.1300,1.0000 9.000,1.5258,0.04946,0.03881,-0.1317,0.1110,1.0000 9.250,1.5436,0.05245,0.04207,-0.1298,0.1001,1.0000 9.500,1.5648,0.05677,0.04686,-0.1283,0.0946,1.0000 9.750,1.5782,0.06094,0.05154,-0.1259,0.0912,1.0000 10.000,1.5928,0.06490,0.05575,-0.1242,0.0875,1.0000 10.250,1.5981,0.06962,0.06075,-0.1216,0.0849,1.0000 10.500,1.5882,0.07363,0.06533,-0.1169,0.0841,1.0000 10.750,1.5750,0.07779,0.06996,-0.1124,0.0836,1.0000 11.000,1.5582,0.08194,0.07450,-0.1078,0.0835,1.0000 11.250,1.5377,0.08595,0.07883,-0.1033,0.0837,1.0000 11.500,1.5164,0.09035,0.08351,-0.0995,0.0840,1.0000 11.750,1.4943,0.09511,0.08852,-0.0967,0.0844,1.0000 12.000,1.4725,0.10031,0.09394,-0.0948,0.0848,1.0000 12.250,1.4523,0.10597,0.09979,-0.0940,0.0852,1.0000 12.500,1.3540,0.11957,0.11393,-0.1013,0.0945,1.0000