Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-pfcm-il-1000000 Airfoil,pfcm-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,88.3852 Max Cl/Cd alpha,2.5 Url,http://airfoiltools.com/polar/csv?polar=xf-pfcm-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.5944,0.08880,0.08725,-0.0088,1.0000,0.0079 -9.000,-0.5978,0.08327,0.08173,-0.0126,1.0000,0.0080 -8.750,-0.6011,0.07737,0.07586,-0.0175,1.0000,0.0080 -8.500,-0.6049,0.06902,0.06751,-0.0286,1.0000,0.0079 -8.250,-0.6062,0.06200,0.06040,-0.0343,1.0000,0.0080 -8.000,-0.6049,0.05590,0.05417,-0.0377,1.0000,0.0081 -7.750,-0.5988,0.05116,0.04929,-0.0395,1.0000,0.0082 -7.500,-0.5888,0.04749,0.04547,-0.0404,1.0000,0.0084 -7.250,-0.5769,0.04411,0.04195,-0.0408,1.0000,0.0087 -7.000,-0.5644,0.04104,0.03874,-0.0406,1.0000,0.0092 -6.750,-0.5525,0.03774,0.03526,-0.0395,1.0000,0.0102 -6.000,-0.4935,0.01875,0.01464,-0.0390,0.9953,0.0093 -5.750,-0.4616,0.01702,0.01269,-0.0402,0.9936,0.0101 -5.500,-0.4310,0.01472,0.01008,-0.0409,0.9910,0.0106 -5.250,-0.3986,0.01358,0.00876,-0.0420,0.9884,0.0113 -5.000,-0.3658,0.01300,0.00807,-0.0432,0.9855,0.0118 -4.750,-0.3343,0.01149,0.00640,-0.0442,0.9828,0.0122 -4.500,-0.3078,0.00998,0.00477,-0.0442,0.9762,0.0133 -4.250,-0.2782,0.00944,0.00419,-0.0447,0.9706,0.0144 -4.000,-0.2512,0.00899,0.00369,-0.0446,0.9629,0.0155 -3.750,-0.2245,0.00862,0.00325,-0.0443,0.9555,0.0165 -3.500,-0.1984,0.00829,0.00286,-0.0439,0.9468,0.0173 -3.250,-0.1722,0.00803,0.00255,-0.0435,0.9388,0.0180 -3.000,-0.1460,0.00762,0.00203,-0.0431,0.9300,0.0211 -2.750,-0.1191,0.00739,0.00176,-0.0428,0.9216,0.0265 -2.500,-0.0925,0.00710,0.00152,-0.0425,0.9132,0.0515 -2.250,-0.0659,0.00661,0.00133,-0.0426,0.9041,0.1438 -2.000,-0.0402,0.00579,0.00112,-0.0427,0.8953,0.3363 -1.750,-0.0146,0.00511,0.00101,-0.0426,0.8863,0.5240 -1.500,0.0125,0.00487,0.00098,-0.0426,0.8769,0.5975 -1.250,0.0398,0.00475,0.00096,-0.0425,0.8677,0.6448 -1.000,0.0674,0.00470,0.00093,-0.0424,0.8580,0.6707 -0.750,0.0948,0.00460,0.00094,-0.0423,0.8476,0.7149 -0.500,0.1221,0.00454,0.00094,-0.0421,0.8372,0.7495 -0.250,0.1498,0.00451,0.00093,-0.0420,0.8263,0.7700 0.000,0.1774,0.00449,0.00092,-0.0420,0.8148,0.7878 0.250,0.2051,0.00447,0.00091,-0.0419,0.8029,0.8035 0.500,0.2326,0.00444,0.00091,-0.0418,0.7903,0.8195 0.750,0.2597,0.00442,0.00092,-0.0416,0.7754,0.8401 1.000,0.2859,0.00439,0.00094,-0.0411,0.7577,0.8697 1.250,0.3098,0.00432,0.00097,-0.0401,0.7393,0.9181 1.500,0.3401,0.00433,0.00098,-0.0404,0.7143,0.9764 1.750,0.3740,0.00448,0.00098,-0.0419,0.6740,1.0000 2.000,0.4008,0.00467,0.00102,-0.0417,0.6349,1.0000 2.250,0.4276,0.00489,0.00110,-0.0416,0.5925,1.0000 2.500,0.4543,0.00514,0.00118,-0.0416,0.5450,1.0000 2.750,0.4802,0.00555,0.00131,-0.0414,0.4709,1.0000 3.000,0.5023,0.00668,0.00166,-0.0409,0.2771,1.0000 3.250,0.5255,0.00766,0.00203,-0.0406,0.1292,1.0000 3.500,0.5506,0.00830,0.00235,-0.0404,0.0536,1.0000 3.750,0.5765,0.00881,0.00273,-0.0402,0.0244,1.0000 4.000,0.6036,0.00906,0.00300,-0.0401,0.0218,1.0000 4.250,0.6303,0.00939,0.00333,-0.0400,0.0188,1.0000 4.500,0.6551,0.01010,0.00417,-0.0395,0.0160,1.0000 4.750,0.6815,0.01046,0.00456,-0.0393,0.0155,1.0000 5.000,0.7074,0.01090,0.00505,-0.0390,0.0149,1.0000 5.250,0.7328,0.01140,0.00560,-0.0387,0.0141,1.0000 5.500,0.7585,0.01184,0.00607,-0.0384,0.0130,1.0000 5.750,0.7841,0.01226,0.00652,-0.0382,0.0119,1.0000 6.000,0.8065,0.01333,0.00767,-0.0373,0.0110,1.0000 6.250,0.8258,0.01551,0.01003,-0.0359,0.0102,1.0000 6.500,0.8516,0.01591,0.01049,-0.0356,0.0099,1.0000 6.750,0.8764,0.01667,0.01134,-0.0351,0.0094,1.0000 7.000,0.9010,0.01742,0.01218,-0.0347,0.0087,1.0000 7.250,0.9258,0.01790,0.01274,-0.0344,0.0080,1.0000 7.500,0.9500,0.01848,0.01338,-0.0341,0.0075,1.0000 7.750,0.9731,0.01936,0.01434,-0.0336,0.0072,1.0000 8.000,0.9919,0.02163,0.01684,-0.0324,0.0068,1.0000 8.250,0.9975,0.02775,0.02365,-0.0293,0.0064,1.0000 8.500,1.0187,0.02867,0.02475,-0.0286,0.0062,1.0000 8.750,1.0321,0.03162,0.02805,-0.0268,0.0060,1.0000 9.000,1.0187,0.04124,0.03841,-0.0219,0.0057,1.0000 9.250,0.9959,0.05099,0.04868,-0.0177,0.0058,1.0000 9.500,0.9760,0.05764,0.05561,-0.0152,0.0061,1.0000