Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-rae102-il-200000-n5 Airfoil,rae102-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,41.4538 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-rae102-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.250,-0.7606,0.08610,0.08241,-0.0120,1.0000,0.0130 -12.000,-0.7867,0.07523,0.07143,-0.0200,1.0000,0.0129 -11.750,-0.8049,0.06810,0.06420,-0.0252,1.0000,0.0127 -11.500,-0.8264,0.06155,0.05748,-0.0295,1.0000,0.0126 -11.250,-0.8469,0.05619,0.05193,-0.0320,1.0000,0.0126 -11.000,-0.8670,0.05170,0.04723,-0.0327,1.0000,0.0126 -10.750,-0.8845,0.04809,0.04338,-0.0315,1.0000,0.0126 -10.500,-0.9014,0.04483,0.03983,-0.0286,1.0000,0.0127 -10.250,-0.9112,0.04174,0.03641,-0.0257,1.0000,0.0128 -10.000,-0.9135,0.03873,0.03303,-0.0232,1.0000,0.0129 -9.750,-0.9119,0.03570,0.02966,-0.0210,1.0000,0.0132 -9.500,-0.9034,0.03353,0.02730,-0.0193,1.0000,0.0136 -9.250,-0.8914,0.03162,0.02518,-0.0178,1.0000,0.0139 -9.000,-0.8762,0.03038,0.02376,-0.0165,1.0000,0.0146 -8.750,-0.8601,0.02906,0.02225,-0.0152,1.0000,0.0154 -8.500,-0.8431,0.02758,0.02052,-0.0139,1.0000,0.0164 -8.250,-0.8252,0.02594,0.01862,-0.0125,1.0000,0.0172 -8.000,-0.8062,0.02445,0.01690,-0.0112,1.0000,0.0178 -7.750,-0.7880,0.02282,0.01512,-0.0099,1.0000,0.0185 -7.500,-0.7697,0.02159,0.01384,-0.0086,1.0000,0.0196 -7.250,-0.7501,0.02071,0.01287,-0.0074,1.0000,0.0208 -7.000,-0.7299,0.01994,0.01202,-0.0062,1.0000,0.0226 -6.750,-0.7097,0.01916,0.01113,-0.0050,1.0000,0.0244 -6.500,-0.6920,0.01810,0.01001,-0.0033,1.0000,0.0259 -6.250,-0.6736,0.01728,0.00916,-0.0018,1.0000,0.0279 -6.000,-0.6537,0.01667,0.00848,-0.0005,1.0000,0.0309 -5.750,-0.6335,0.01612,0.00785,0.0008,1.0000,0.0341 -5.500,-0.6150,0.01538,0.00712,0.0024,1.0000,0.0385 -5.250,-0.5947,0.01489,0.00656,0.0037,1.0000,0.0437 -5.000,-0.5753,0.01432,0.00602,0.0051,1.0000,0.0522 -4.750,-0.5556,0.01382,0.00552,0.0065,1.0000,0.0632 -4.500,-0.5361,0.01334,0.00510,0.0079,1.0000,0.0814 -4.250,-0.5138,0.01276,0.00470,0.0085,0.9984,0.1149 -4.000,-0.4814,0.01196,0.00424,0.0068,0.9903,0.1868 -3.750,-0.4507,0.01100,0.00379,0.0053,0.9818,0.3039 -3.500,-0.4219,0.01018,0.00358,0.0045,0.9720,0.4431 -3.250,-0.3903,0.00986,0.00346,0.0036,0.9620,0.5107 -3.000,-0.3570,0.00966,0.00335,0.0024,0.9521,0.5535 -2.750,-0.3232,0.00950,0.00323,0.0013,0.9418,0.5878 -2.500,-0.2909,0.00936,0.00314,0.0004,0.9295,0.6164 -2.250,-0.2586,0.00924,0.00306,-0.0003,0.9165,0.6420 -2.000,-0.2267,0.00914,0.00296,-0.0010,0.9026,0.6649 -1.750,-0.1956,0.00905,0.00288,-0.0014,0.8876,0.6839 -1.500,-0.1655,0.00897,0.00280,-0.0017,0.8721,0.7003 -1.250,-0.1365,0.00891,0.00272,-0.0017,0.8566,0.7149 -1.000,-0.1083,0.00887,0.00265,-0.0015,0.8407,0.7284 -0.750,-0.0808,0.00884,0.00259,-0.0012,0.8250,0.7417 -0.500,-0.0537,0.00882,0.00255,-0.0008,0.8099,0.7547 -0.250,-0.0268,0.00880,0.00253,-0.0004,0.7957,0.7679 0.000,0.0000,0.00880,0.00252,0.0000,0.7816,0.7816 0.250,0.0268,0.00880,0.00253,0.0004,0.7679,0.7957 0.500,0.0537,0.00882,0.00255,0.0008,0.7547,0.8099 0.750,0.0808,0.00884,0.00259,0.0012,0.7417,0.8250 1.000,0.1083,0.00887,0.00265,0.0015,0.7285,0.8407 1.250,0.1365,0.00891,0.00272,0.0017,0.7150,0.8566 1.500,0.1655,0.00897,0.00280,0.0017,0.7004,0.8722 1.750,0.1956,0.00905,0.00288,0.0014,0.6838,0.8877 2.000,0.2266,0.00914,0.00296,0.0010,0.6649,0.9027 2.250,0.2586,0.00924,0.00306,0.0003,0.6420,0.9166 2.500,0.2909,0.00936,0.00314,-0.0004,0.6164,0.9295 2.750,0.3232,0.00950,0.00323,-0.0013,0.5878,0.9419 3.000,0.3570,0.00966,0.00335,-0.0024,0.5537,0.9523 3.250,0.3902,0.00986,0.00346,-0.0036,0.5102,0.9622 3.500,0.4220,0.01018,0.00357,-0.0045,0.4421,0.9722 3.750,0.4508,0.01098,0.00379,-0.0053,0.3062,0.9821 4.000,0.4816,0.01196,0.00424,-0.0068,0.1877,0.9905 4.250,0.5138,0.01276,0.00469,-0.0085,0.1147,0.9986 4.500,0.5356,0.01333,0.00510,-0.0078,0.0817,1.0000 4.750,0.5551,0.01381,0.00552,-0.0064,0.0633,1.0000 5.000,0.5749,0.01431,0.00602,-0.0050,0.0523,1.0000 5.250,0.5944,0.01488,0.00654,-0.0036,0.0437,1.0000 5.500,0.6147,0.01537,0.00711,-0.0023,0.0386,1.0000 5.750,0.6331,0.01612,0.00785,-0.0008,0.0340,1.0000 6.000,0.6534,0.01667,0.00848,0.0005,0.0309,1.0000 6.250,0.6734,0.01727,0.00915,0.0019,0.0279,1.0000 6.500,0.6919,0.01810,0.01000,0.0033,0.0258,1.0000 6.750,0.7097,0.01915,0.01111,0.0050,0.0243,1.0000 7.000,0.7299,0.01995,0.01203,0.0062,0.0226,1.0000 7.250,0.7502,0.02069,0.01285,0.0074,0.0207,1.0000 7.500,0.7699,0.02157,0.01381,0.0085,0.0195,1.0000 7.750,0.7882,0.02283,0.01513,0.0098,0.0185,1.0000 8.000,0.8065,0.02444,0.01688,0.0112,0.0178,1.0000 8.250,0.8255,0.02595,0.01863,0.0125,0.0172,1.0000 8.500,0.8435,0.02760,0.02054,0.0138,0.0165,1.0000 8.750,0.8607,0.02903,0.02221,0.0151,0.0154,1.0000 9.000,0.8768,0.03042,0.02381,0.0164,0.0146,1.0000 9.250,0.8920,0.03170,0.02527,0.0176,0.0139,1.0000 9.500,0.9046,0.03336,0.02709,0.0191,0.0135,1.0000 9.750,0.9130,0.03572,0.02970,0.0208,0.0132,1.0000 10.000,0.9148,0.03875,0.03303,0.0230,0.0130,1.0000 10.250,0.9127,0.04171,0.03637,0.0254,0.0128,1.0000 10.500,0.9032,0.04483,0.03982,0.0283,0.0127,1.0000 10.750,0.8871,0.04800,0.04327,0.0312,0.0127,1.0000 11.000,0.8670,0.05189,0.04743,0.0324,0.0126,1.0000 11.250,0.8490,0.05613,0.05187,0.0318,0.0126,1.0000 11.500,0.8302,0.06122,0.05713,0.0295,0.0127,1.0000 11.750,0.8066,0.06814,0.06423,0.0249,0.0127,1.0000 12.000,0.7850,0.07608,0.07230,0.0190,0.0128,1.0000 12.250,0.7477,0.09153,0.08792,0.0081,0.0132,1.0000