Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ssca09-il-200000-n5 Airfoil,ssca09-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,52.7375 Max Cl/Cd alpha,7.5 Url,http://airfoiltools.com/polar/csv?polar=xf-ssca09-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.4645,0.11499,0.11181,0.0029,1.0000,0.0246 -10.500,-0.4646,0.11094,0.10777,0.0015,1.0000,0.0250 -10.000,-0.6069,0.11187,0.10856,0.0131,1.0000,0.0230 -9.000,-0.4888,0.07942,0.07633,-0.0118,1.0000,0.0205 -8.750,-0.4944,0.07410,0.07103,-0.0142,1.0000,0.0197 -8.250,-0.6288,0.06555,0.06207,-0.0223,1.0000,0.0164 -8.000,-0.6215,0.06225,0.05869,-0.0234,1.0000,0.0157 -7.750,-0.6169,0.05774,0.05402,-0.0248,1.0000,0.0155 -7.500,-0.6101,0.05298,0.04904,-0.0259,1.0000,0.0153 -7.250,-0.6014,0.04679,0.04231,-0.0261,1.0000,0.0161 -6.750,-0.5738,0.03884,0.03370,-0.0261,0.9917,0.0160 -6.500,-0.5518,0.03500,0.02951,-0.0271,0.9864,0.0157 -6.250,-0.5287,0.03157,0.02568,-0.0276,0.9812,0.0155 -6.000,-0.5042,0.02854,0.02223,-0.0278,0.9766,0.0154 -5.750,-0.4783,0.02593,0.01919,-0.0278,0.9726,0.0153 -5.500,-0.4528,0.02376,0.01664,-0.0275,0.9676,0.0154 -5.250,-0.4259,0.02195,0.01448,-0.0273,0.9635,0.0156 -5.000,-0.3992,0.02049,0.01274,-0.0270,0.9596,0.0159 -4.750,-0.3733,0.01913,0.01119,-0.0266,0.9551,0.0163 -4.500,-0.3476,0.01796,0.00996,-0.0263,0.9510,0.0170 -4.250,-0.3218,0.01719,0.00914,-0.0261,0.9471,0.0179 -4.000,-0.2959,0.01661,0.00851,-0.0258,0.9426,0.0198 -3.750,-0.2702,0.01600,0.00782,-0.0253,0.9384,0.0213 -3.500,-0.2458,0.01518,0.00697,-0.0246,0.9347,0.0224 -3.250,-0.2202,0.01453,0.00631,-0.0244,0.9299,0.0243 -3.000,-0.1944,0.01410,0.00584,-0.0240,0.9255,0.0273 -2.750,-0.1693,0.01366,0.00535,-0.0234,0.9217,0.0322 -2.500,-0.1424,0.01328,0.00492,-0.0233,0.9170,0.0388 -2.250,-0.1165,0.01274,0.00453,-0.0230,0.9123,0.0700 -2.000,-0.0950,0.01136,0.00415,-0.0227,0.9082,0.3172 -1.750,-0.0764,0.00996,0.00411,-0.0212,0.9035,0.6510 -1.500,-0.0583,0.00970,0.00437,-0.0181,0.8983,0.7930 -1.250,-0.0431,0.00977,0.00462,-0.0138,0.8937,0.8628 -1.000,-0.0213,0.00985,0.00468,-0.0118,0.8884,0.8901 -0.750,0.0024,0.00980,0.00456,-0.0104,0.8809,0.9026 -0.500,0.0251,0.00968,0.00437,-0.0087,0.8693,0.9131 -0.250,0.0467,0.00948,0.00407,-0.0065,0.8533,0.9228 0.000,0.0696,0.00930,0.00379,-0.0047,0.8365,0.9330 0.250,0.0955,0.00919,0.00360,-0.0039,0.8222,0.9429 0.500,0.1246,0.00911,0.00347,-0.0038,0.8104,0.9510 0.750,0.1535,0.00904,0.00334,-0.0038,0.7979,0.9601 1.000,0.1851,0.00898,0.00323,-0.0044,0.7834,0.9673 1.250,0.2172,0.00892,0.00312,-0.0052,0.7660,0.9744 1.500,0.2503,0.00887,0.00300,-0.0061,0.7420,0.9808 1.750,0.2835,0.00883,0.00286,-0.0071,0.7039,0.9866 2.000,0.3158,0.00890,0.00266,-0.0078,0.6408,0.9923 2.250,0.3483,0.00927,0.00258,-0.0088,0.5487,0.9973 2.500,0.3767,0.00987,0.00268,-0.0094,0.4448,1.0000 2.750,0.4003,0.01044,0.00284,-0.0092,0.3659,1.0000 3.000,0.4242,0.01088,0.00302,-0.0089,0.3145,1.0000 3.250,0.4487,0.01124,0.00322,-0.0086,0.2810,1.0000 3.500,0.4738,0.01157,0.00343,-0.0084,0.2570,1.0000 3.750,0.4995,0.01188,0.00365,-0.0083,0.2381,1.0000 4.000,0.5254,0.01220,0.00390,-0.0083,0.2226,1.0000 4.250,0.5516,0.01250,0.00416,-0.0083,0.2096,1.0000 4.500,0.5780,0.01282,0.00444,-0.0083,0.1994,1.0000 4.750,0.6044,0.01316,0.00475,-0.0083,0.1911,1.0000 5.000,0.6310,0.01347,0.00509,-0.0083,0.1834,1.0000 5.250,0.6572,0.01384,0.00542,-0.0083,0.1751,1.0000 5.500,0.6840,0.01413,0.00575,-0.0083,0.1662,1.0000 5.750,0.7103,0.01449,0.00610,-0.0083,0.1584,1.0000 6.000,0.7368,0.01482,0.00649,-0.0083,0.1510,1.0000 6.250,0.7630,0.01519,0.00688,-0.0083,0.1443,1.0000 6.500,0.7895,0.01552,0.00727,-0.0083,0.1363,1.0000 6.750,0.8157,0.01587,0.00769,-0.0083,0.1284,1.0000 7.000,0.8416,0.01625,0.00808,-0.0083,0.1191,1.0000 7.250,0.8680,0.01657,0.00849,-0.0083,0.1083,1.0000 7.500,0.8939,0.01695,0.00891,-0.0083,0.0954,1.0000 7.750,0.9191,0.01744,0.00939,-0.0083,0.0807,1.0000 8.000,0.9436,0.01805,0.00999,-0.0081,0.0663,1.0000 8.250,0.9673,0.01881,0.01074,-0.0079,0.0554,1.0000 8.500,0.9901,0.01970,0.01163,-0.0076,0.0469,1.0000 8.750,1.0135,0.02047,0.01252,-0.0073,0.0413,1.0000 9.000,1.0350,0.02149,0.01360,-0.0069,0.0363,1.0000 9.250,1.0575,0.02231,0.01457,-0.0065,0.0325,1.0000 9.500,1.0782,0.02333,0.01567,-0.0060,0.0295,1.0000 9.750,1.0970,0.02455,0.01701,-0.0052,0.0275,1.0000 10.000,1.1164,0.02565,0.01829,-0.0045,0.0258,1.0000 10.250,1.1346,0.02684,0.01966,-0.0037,0.0243,1.0000 10.500,1.1516,0.02808,0.02103,-0.0029,0.0230,1.0000 10.750,1.1659,0.02952,0.02257,-0.0019,0.0218,1.0000 11.000,1.1777,0.03122,0.02441,-0.0006,0.0208,1.0000 11.250,1.1908,0.03269,0.02610,0.0005,0.0199,1.0000 11.500,1.2006,0.03439,0.02801,0.0019,0.0193,1.0000 11.750,1.2061,0.03616,0.02998,0.0037,0.0187,1.0000 12.000,1.2098,0.03812,0.03213,0.0054,0.0182,1.0000 12.250,1.2118,0.04027,0.03446,0.0068,0.0177,1.0000 12.500,1.2119,0.04265,0.03705,0.0079,0.0174,1.0000 12.750,1.2101,0.04531,0.03990,0.0086,0.0170,1.0000 13.000,1.2067,0.04828,0.04303,0.0089,0.0167,1.0000 13.250,1.2012,0.05168,0.04659,0.0086,0.0164,1.0000 13.500,1.1928,0.05572,0.05079,0.0076,0.0162,1.0000 13.750,1.1813,0.06061,0.05587,0.0057,0.0159,1.0000 14.000,1.1671,0.06647,0.06192,0.0026,0.0158,1.0000 15.000,1.0919,0.09926,0.09549,-0.0187,0.0159,1.0000 15.250,1.0535,0.11310,0.10956,-0.0273,0.0164,1.0000 15.500,0.8791,0.16823,0.16482,-0.0554,0.0184,1.0000