Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-raf30md-il-100000-n5 Airfoil,raf30md-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,31.0384 Max Cl/Cd alpha,3 Url,http://www.airfoiltools.com/polar/csv?polar=xf-raf30md-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.6800,0.08518,0.08035,-0.0040,1.0000,0.0212 -9.250,-0.6904,0.07722,0.07244,-0.0104,1.0000,0.0209 -9.000,-0.7057,0.07052,0.06571,-0.0157,1.0000,0.0205 -8.750,-0.7223,0.06545,0.06054,-0.0171,1.0000,0.0202 -8.500,-0.7333,0.06036,0.05528,-0.0179,1.0000,0.0200 -8.250,-0.7398,0.05539,0.05005,-0.0180,1.0000,0.0200 -8.000,-0.7417,0.05059,0.04492,-0.0174,1.0000,0.0199 -7.750,-0.7391,0.04607,0.04000,-0.0164,1.0000,0.0202 -7.500,-0.7319,0.04211,0.03559,-0.0152,1.0000,0.0213 -7.250,-0.7212,0.03844,0.03139,-0.0138,1.0000,0.0227 -7.000,-0.7072,0.03497,0.02736,-0.0122,1.0000,0.0236 -6.750,-0.6903,0.03181,0.02363,-0.0107,1.0000,0.0244 -6.500,-0.6703,0.02923,0.02054,-0.0093,1.0000,0.0254 -6.250,-0.6503,0.02676,0.01779,-0.0082,1.0000,0.0276 -6.000,-0.6290,0.02514,0.01599,-0.0074,1.0000,0.0309 -5.750,-0.6063,0.02334,0.01396,-0.0063,1.0000,0.0336 -5.500,-0.5837,0.02186,0.01227,-0.0051,1.0000,0.0377 -5.250,-0.5631,0.02045,0.01087,-0.0041,1.0000,0.0429 -5.000,-0.5410,0.01943,0.00968,-0.0029,1.0000,0.0484 -4.750,-0.5210,0.01829,0.00856,-0.0017,1.0000,0.0560 -4.500,-0.4991,0.01752,0.00761,-0.0005,1.0000,0.0628 -4.250,-0.4777,0.01671,0.00679,0.0006,1.0000,0.0733 -4.000,-0.4561,0.01592,0.00600,0.0018,1.0000,0.0874 -3.750,-0.4356,0.01494,0.00527,0.0030,1.0000,0.1364 -3.500,-0.4168,0.01383,0.00470,0.0042,1.0000,0.2524 -3.250,-0.3977,0.01297,0.00434,0.0056,1.0000,0.3723 -3.000,-0.3795,0.01222,0.00416,0.0075,1.0000,0.5024 -2.750,-0.3606,0.01173,0.00410,0.0096,1.0000,0.6126 -2.500,-0.3408,0.01141,0.00411,0.0120,1.0000,0.7049 -2.250,-0.3193,0.01123,0.00407,0.0141,1.0000,0.7713 -2.000,-0.2952,0.01113,0.00405,0.0156,1.0000,0.8219 -1.750,-0.2655,0.01111,0.00404,0.0159,1.0000,0.8649 -1.500,-0.2312,0.01111,0.00396,0.0149,1.0000,0.8945 -1.250,-0.1920,0.01114,0.00391,0.0127,1.0000,0.9196 -1.000,-0.1505,0.01117,0.00386,0.0099,1.0000,0.9420 -0.750,-0.1077,0.01118,0.00380,0.0067,1.0000,0.9623 -0.500,-0.0627,0.01117,0.00374,0.0029,1.0000,0.9799 -0.250,-0.0169,0.01114,0.00367,-0.0013,1.0000,0.9966 0.000,0.0000,0.01111,0.00364,0.0000,1.0000,1.0000 0.250,0.0169,0.01114,0.00367,0.0013,0.9966,1.0000 0.500,0.0628,0.01117,0.00374,-0.0029,0.9799,1.0000 0.750,0.1076,0.01118,0.00380,-0.0067,0.9623,1.0000 1.000,0.1506,0.01117,0.00386,-0.0099,0.9419,1.0000 1.250,0.1920,0.01114,0.00391,-0.0128,0.9196,1.0000 1.500,0.2313,0.01111,0.00396,-0.0149,0.8945,1.0000 1.750,0.2656,0.01111,0.00404,-0.0160,0.8650,1.0000 2.000,0.2953,0.01113,0.00405,-0.0156,0.8217,1.0000 2.250,0.3194,0.01123,0.00407,-0.0141,0.7709,1.0000 2.500,0.3410,0.01141,0.00411,-0.0120,0.7051,1.0000 2.750,0.3608,0.01173,0.00411,-0.0097,0.6134,1.0000 3.000,0.3796,0.01223,0.00416,-0.0075,0.5008,1.0000 3.250,0.3978,0.01297,0.00434,-0.0056,0.3730,1.0000 3.500,0.4169,0.01384,0.00470,-0.0042,0.2521,1.0000 3.750,0.4357,0.01494,0.00528,-0.0030,0.1364,1.0000 4.000,0.4562,0.01592,0.00600,-0.0018,0.0873,1.0000 4.250,0.4778,0.01671,0.00679,-0.0006,0.0733,1.0000 4.500,0.4991,0.01752,0.00761,0.0005,0.0626,1.0000 4.750,0.5210,0.01829,0.00857,0.0017,0.0559,1.0000 5.000,0.5411,0.01942,0.00967,0.0029,0.0484,1.0000 5.250,0.5631,0.02045,0.01087,0.0041,0.0429,1.0000 5.500,0.5838,0.02184,0.01225,0.0051,0.0378,1.0000 5.750,0.6063,0.02335,0.01397,0.0063,0.0336,1.0000 6.000,0.6290,0.02514,0.01599,0.0074,0.0309,1.0000 6.250,0.6502,0.02675,0.01778,0.0082,0.0276,1.0000 6.500,0.6703,0.02923,0.02053,0.0093,0.0254,1.0000 6.750,0.6901,0.03182,0.02365,0.0107,0.0244,1.0000 7.000,0.7071,0.03495,0.02733,0.0123,0.0236,1.0000 7.250,0.7210,0.03843,0.03138,0.0138,0.0226,1.0000 7.500,0.7316,0.04211,0.03559,0.0153,0.0213,1.0000 7.750,0.7389,0.04606,0.03999,0.0165,0.0203,1.0000 8.000,0.7415,0.05055,0.04488,0.0175,0.0199,1.0000 8.250,0.7397,0.05533,0.04999,0.0180,0.0200,1.0000 8.500,0.7331,0.06032,0.05524,0.0180,0.0200,1.0000 8.750,0.7222,0.06540,0.06049,0.0172,0.0203,1.0000 9.000,0.7059,0.07043,0.06561,0.0158,0.0205,1.0000 9.250,0.6901,0.07729,0.07251,0.0104,0.0209,1.0000 9.500,0.6802,0.08510,0.08027,0.0040,0.0213,1.0000