Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-lwk80080-il-200000-n5 Airfoil,lwk80080-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,35.7029 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-lwk80080-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.750,-0.6717,0.08298,0.07953,-0.0114,1.0000,0.0114 -9.500,-0.6847,0.07412,0.07069,-0.0195,1.0000,0.0113 -9.250,-0.7005,0.06780,0.06430,-0.0237,1.0000,0.0111 -9.000,-0.7160,0.06306,0.05946,-0.0243,1.0000,0.0110 -8.750,-0.7290,0.05807,0.05432,-0.0238,1.0000,0.0109 -8.500,-0.7381,0.05284,0.04886,-0.0227,1.0000,0.0109 -8.250,-0.7423,0.04793,0.04368,-0.0211,1.0000,0.0108 -8.000,-0.7443,0.04288,0.03826,-0.0190,1.0000,0.0106 -7.750,-0.7432,0.03791,0.03285,-0.0164,1.0000,0.0108 -7.500,-0.7371,0.03372,0.02818,-0.0139,1.0000,0.0109 -7.250,-0.7269,0.03011,0.02407,-0.0115,1.0000,0.0111 -7.000,-0.7127,0.02706,0.02051,-0.0093,1.0000,0.0119 -6.750,-0.6929,0.02584,0.01896,-0.0079,1.0000,0.0130 -6.500,-0.6768,0.02305,0.01581,-0.0061,1.0000,0.0138 -6.250,-0.6578,0.02140,0.01398,-0.0048,1.0000,0.0148 -6.000,-0.6378,0.01993,0.01233,-0.0033,1.0000,0.0155 -5.750,-0.6178,0.01869,0.01096,-0.0019,1.0000,0.0163 -5.500,-0.5987,0.01759,0.00970,-0.0003,1.0000,0.0174 -5.250,-0.5807,0.01664,0.00866,0.0015,1.0000,0.0186 -5.000,-0.5642,0.01585,0.00777,0.0035,1.0000,0.0201 -4.750,-0.5395,0.01486,0.00673,0.0037,0.9916,0.0249 -4.500,-0.5078,0.01433,0.00612,0.0026,0.9842,0.0318 -4.250,-0.4769,0.01366,0.00544,0.0015,0.9771,0.0424 -4.000,-0.4450,0.01310,0.00485,0.0003,0.9707,0.0573 -3.750,-0.4136,0.01251,0.00433,-0.0009,0.9646,0.0846 -3.500,-0.3826,0.01189,0.00390,-0.0021,0.9585,0.1310 -3.250,-0.3535,0.01108,0.00350,-0.0031,0.9525,0.2309 -3.000,-0.3310,0.00992,0.00312,-0.0028,0.9449,0.4147 -2.750,-0.3118,0.00896,0.00306,-0.0011,0.9379,0.6268 -2.500,-0.2844,0.00884,0.00313,-0.0007,0.9319,0.7091 -2.250,-0.2534,0.00884,0.00313,-0.0011,0.9275,0.7488 -2.000,-0.2264,0.00887,0.00314,-0.0007,0.9212,0.7758 -1.750,-0.1979,0.00892,0.00318,-0.0004,0.9160,0.8023 -1.500,-0.1694,0.00898,0.00324,-0.0001,0.9114,0.8253 -1.250,-0.1432,0.00902,0.00327,0.0005,0.9055,0.8422 -1.000,-0.1135,0.00904,0.00327,0.0003,0.9010,0.8540 -0.750,-0.0854,0.00904,0.00325,0.0004,0.8957,0.8622 -0.500,-0.0576,0.00904,0.00322,0.0004,0.8902,0.8693 -0.250,-0.0275,0.00903,0.00319,-0.0001,0.8860,0.8747 0.000,0.0000,0.00903,0.00319,0.0000,0.8801,0.8801 0.250,0.0275,0.00903,0.00319,0.0001,0.8747,0.8860 0.500,0.0577,0.00904,0.00322,-0.0004,0.8694,0.8902 0.750,0.0854,0.00904,0.00325,-0.0004,0.8621,0.8957 1.000,0.1134,0.00904,0.00327,-0.0003,0.8538,0.9009 1.250,0.1431,0.00902,0.00327,-0.0005,0.8419,0.9055 1.500,0.1694,0.00898,0.00324,0.0001,0.8253,0.9113 1.750,0.1979,0.00891,0.00318,0.0005,0.8015,0.9161 2.000,0.2263,0.00886,0.00314,0.0007,0.7748,0.9213 2.250,0.2534,0.00884,0.00313,0.0011,0.7486,0.9275 2.500,0.2846,0.00884,0.00315,0.0006,0.7118,0.9318 2.750,0.3122,0.00895,0.00311,0.0010,0.6329,0.9378 3.000,0.3304,0.00997,0.00313,0.0029,0.4063,0.9450 3.250,0.3529,0.01116,0.00351,0.0031,0.2179,0.9528 3.500,0.3826,0.01190,0.00390,0.0020,0.1293,0.9586 3.750,0.4137,0.01250,0.00433,0.0009,0.0853,0.9647 4.000,0.4451,0.01309,0.00486,-0.0003,0.0579,0.9707 4.250,0.4770,0.01363,0.00540,-0.0015,0.0407,0.9770 4.500,0.5080,0.01425,0.00604,-0.0026,0.0299,0.9840 4.750,0.5384,0.01508,0.00689,-0.0036,0.0218,0.9918 5.000,0.5641,0.01588,0.00781,-0.0035,0.0194,1.0000 5.250,0.5805,0.01669,0.00871,-0.0014,0.0181,1.0000 5.500,0.5985,0.01764,0.00975,0.0004,0.0165,1.0000 5.750,0.6177,0.01873,0.01100,0.0019,0.0160,1.0000 6.000,0.6375,0.01997,0.01236,0.0034,0.0150,1.0000 6.250,0.6576,0.02146,0.01403,0.0048,0.0146,1.0000 6.500,0.6765,0.02324,0.01601,0.0062,0.0138,1.0000 6.750,0.6938,0.02554,0.01867,0.0078,0.0127,1.0000 7.000,0.7121,0.02734,0.02082,0.0094,0.0119,1.0000 7.250,0.7265,0.03022,0.02418,0.0115,0.0113,1.0000 7.500,0.7368,0.03381,0.02827,0.0139,0.0110,1.0000 7.750,0.7436,0.03778,0.03270,0.0163,0.0111,1.0000 8.000,0.7465,0.04224,0.03757,0.0187,0.0110,1.0000 8.250,0.7442,0.04744,0.04315,0.0209,0.0110,1.0000 8.500,0.7375,0.05298,0.04901,0.0227,0.0109,1.0000 8.750,0.7308,0.05769,0.05392,0.0237,0.0111,1.0000 9.000,0.7188,0.06260,0.05899,0.0242,0.0111,1.0000 9.250,0.7026,0.06739,0.06388,0.0237,0.0113,1.0000 9.500,0.6866,0.07364,0.07021,0.0198,0.0115,1.0000 9.750,0.6755,0.08168,0.07825,0.0124,0.0117,1.0000 10.000,0.6664,0.08937,0.08589,0.0067,0.0117,1.0000