Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-sc1095r8-il-50000-n5 Airfoil,sc1095r8-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,27.0495 Max Cl/Cd alpha,6.75 Url,http://airfoiltools.com/polar/csv?polar=xf-sc1095r8-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.000,-0.4887,0.11213,0.10503,0.0001,1.0000,0.1265 -7.750,-0.4880,0.10886,0.10182,-0.0019,1.0000,0.1304 -7.500,-0.5150,0.10671,0.09982,-0.0108,1.0000,0.1345 -7.250,-0.5050,0.10192,0.09508,-0.0106,1.0000,0.1358 -7.000,-0.4884,0.09777,0.09095,-0.0086,1.0000,0.1377 -6.750,-0.4811,0.09413,0.08735,-0.0091,1.0000,0.1398 -6.250,-0.4832,0.07866,0.07163,-0.0248,1.0000,0.0732 -5.750,-0.4764,0.06783,0.06040,-0.0308,1.0000,0.0635 -5.500,-0.4660,0.06415,0.05664,-0.0312,1.0000,0.0631 -5.250,-0.4551,0.06044,0.05278,-0.0316,1.0000,0.0629 -5.000,-0.4430,0.05685,0.04900,-0.0318,1.0000,0.0628 -4.750,-0.4294,0.05343,0.04538,-0.0317,1.0000,0.0626 -4.500,-0.4146,0.05020,0.04194,-0.0313,1.0000,0.0622 -4.250,-0.3988,0.04712,0.03862,-0.0307,1.0000,0.0615 -4.000,-0.3821,0.04419,0.03543,-0.0299,1.0000,0.0610 -3.750,-0.3644,0.04145,0.03239,-0.0289,1.0000,0.0607 -3.500,-0.3457,0.03891,0.02953,-0.0278,1.0000,0.0605 -3.250,-0.3261,0.03663,0.02691,-0.0266,1.0000,0.0611 -3.000,-0.3053,0.03459,0.02446,-0.0253,1.0000,0.0626 -2.750,-0.2837,0.03278,0.02221,-0.0239,1.0000,0.0640 -2.500,-0.2628,0.03106,0.02043,-0.0228,1.0000,0.0654 -2.250,-0.2411,0.02957,0.01882,-0.0215,1.0000,0.0665 -2.000,-0.2188,0.02825,0.01735,-0.0203,1.0000,0.0678 -1.750,-0.1964,0.02714,0.01612,-0.0190,1.0000,0.0707 -1.500,-0.1734,0.02616,0.01494,-0.0176,1.0000,0.0743 -1.250,-0.1507,0.02515,0.01393,-0.0164,1.0000,0.0773 -1.000,-0.1279,0.02433,0.01312,-0.0151,1.0000,0.0807 -0.750,-0.1051,0.02372,0.01242,-0.0138,1.0000,0.0865 -0.500,-0.0829,0.02309,0.01184,-0.0128,1.0000,0.0930 -0.250,-0.0558,0.02255,0.01123,-0.0125,0.9973,0.1021 0.000,-0.0062,0.02169,0.01051,-0.0164,0.9827,0.1256 0.250,0.0403,0.02019,0.00971,-0.0200,0.9680,0.2250 0.500,0.0996,0.01782,0.00970,-0.0221,0.9585,1.0000 0.750,0.1482,0.01786,0.00944,-0.0254,0.9373,1.0000 1.000,0.1918,0.01784,0.00921,-0.0274,0.9130,1.0000 1.250,0.2328,0.01774,0.00894,-0.0287,0.8845,1.0000 1.500,0.2657,0.01762,0.00867,-0.0282,0.8483,1.0000 1.750,0.2944,0.01751,0.00840,-0.0268,0.8067,1.0000 2.000,0.3204,0.01744,0.00813,-0.0249,0.7613,1.0000 2.250,0.3444,0.01745,0.00790,-0.0226,0.7117,1.0000 2.500,0.3673,0.01755,0.00771,-0.0203,0.6575,1.0000 2.750,0.3895,0.01778,0.00757,-0.0179,0.6003,1.0000 3.000,0.4111,0.01814,0.00753,-0.0158,0.5434,1.0000 3.250,0.4328,0.01861,0.00761,-0.0139,0.4904,1.0000 3.500,0.4546,0.01916,0.00778,-0.0123,0.4435,1.0000 3.750,0.4769,0.01974,0.00804,-0.0109,0.4018,1.0000 4.000,0.4997,0.02037,0.00838,-0.0097,0.3662,1.0000 4.250,0.5233,0.02101,0.00878,-0.0087,0.3347,1.0000 4.500,0.5471,0.02168,0.00921,-0.0078,0.3088,1.0000 4.750,0.5715,0.02235,0.00972,-0.0069,0.2858,1.0000 5.000,0.5960,0.02303,0.01025,-0.0061,0.2669,1.0000 5.250,0.6208,0.02372,0.01083,-0.0053,0.2513,1.0000 5.500,0.6457,0.02443,0.01144,-0.0045,0.2377,1.0000 5.750,0.6704,0.02516,0.01207,-0.0037,0.2262,1.0000 6.000,0.6953,0.02592,0.01277,-0.0030,0.2165,1.0000 6.250,0.7206,0.02675,0.01360,-0.0022,0.2082,1.0000 6.500,0.7453,0.02756,0.01434,-0.0015,0.2005,1.0000 6.750,0.7701,0.02847,0.01530,-0.0007,0.1933,1.0000 7.000,0.7945,0.02938,0.01621,0.0000,0.1867,1.0000 7.250,0.8193,0.03037,0.01708,0.0007,0.1824,1.0000 7.500,0.8436,0.03158,0.01855,0.0014,0.1774,1.0000 7.750,0.8673,0.03272,0.01979,0.0022,0.1727,1.0000 8.000,0.8910,0.03377,0.02079,0.0029,0.1686,1.0000 8.250,0.9135,0.03513,0.02230,0.0036,0.1646,1.0000 8.500,0.9348,0.03665,0.02411,0.0044,0.1605,1.0000 8.750,0.9561,0.03821,0.02584,0.0052,0.1576,1.0000 9.000,0.9773,0.03974,0.02749,0.0059,0.1551,1.0000 9.250,0.9990,0.04123,0.02901,0.0067,0.1528,1.0000 9.500,1.0160,0.04332,0.03139,0.0075,0.1504,1.0000 9.750,1.0283,0.04585,0.03435,0.0084,0.1475,1.0000 10.000,1.0403,0.04829,0.03711,0.0093,0.1447,1.0000 10.250,1.0522,0.05066,0.03973,0.0102,0.1424,1.0000 10.500,1.0626,0.05325,0.04256,0.0110,0.1408,1.0000 10.750,1.0715,0.05593,0.04544,0.0118,0.1395,1.0000 11.000,1.0795,0.05868,0.04837,0.0126,0.1383,1.0000 11.250,1.0887,0.06137,0.05117,0.0133,0.1372,1.0000 11.500,1.0630,0.06710,0.05732,0.0135,0.1364,1.0000 11.750,1.0170,0.07440,0.06494,0.0123,0.1360,1.0000 12.000,0.9362,0.08968,0.08043,0.0015,0.1360,1.0000