Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-p51htip-il-500000 Airfoil,p51htip-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,72.9262 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-p51htip-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.4820,0.08633,0.08415,-0.0541,0.9777,0.0226 -10.500,-0.4817,0.07801,0.07582,-0.0632,0.9643,0.0229 -10.250,-0.5021,0.06870,0.06638,-0.0720,0.9440,0.0226 -10.000,-0.5248,0.06409,0.06164,-0.0729,0.9281,0.0227 -9.750,-0.5488,0.06028,0.05768,-0.0716,0.9153,0.0227 -9.500,-0.5676,0.05740,0.05466,-0.0688,0.9047,0.0227 -9.250,-0.5811,0.05479,0.05190,-0.0658,0.8964,0.0231 -9.000,-0.5894,0.05163,0.04855,-0.0633,0.8900,0.0234 -8.750,-0.5918,0.04846,0.04514,-0.0609,0.8844,0.0249 -8.500,-0.5878,0.04750,0.04372,-0.0574,0.8787,0.0265 -8.250,-0.5861,0.04498,0.04088,-0.0547,0.8744,0.0266 -8.000,-0.5797,0.04222,0.03785,-0.0527,0.8704,0.0266 -7.000,-0.5445,0.02219,0.01609,-0.0437,0.8569,0.0214 -6.750,-0.5209,0.02069,0.01443,-0.0432,0.8539,0.0218 -6.500,-0.4962,0.01953,0.01316,-0.0429,0.8512,0.0224 -6.250,-0.4713,0.01868,0.01221,-0.0427,0.8488,0.0234 -6.000,-0.4459,0.01788,0.01129,-0.0424,0.8466,0.0246 -5.750,-0.4202,0.01706,0.01035,-0.0420,0.8446,0.0255 -5.500,-0.3941,0.01646,0.00965,-0.0418,0.8426,0.0263 -5.250,-0.3691,0.01508,0.00820,-0.0415,0.8404,0.0274 -5.000,-0.3460,0.01413,0.00724,-0.0410,0.8381,0.0287 -4.750,-0.3214,0.01371,0.00683,-0.0407,0.8359,0.0308 -4.500,-0.2968,0.01330,0.00638,-0.0403,0.8339,0.0327 -4.250,-0.2724,0.01290,0.00593,-0.0398,0.8319,0.0342 -4.000,-0.2492,0.01240,0.00536,-0.0391,0.8300,0.0357 -3.750,-0.2266,0.01187,0.00481,-0.0383,0.8283,0.0391 -3.500,-0.2011,0.01159,0.00453,-0.0382,0.8264,0.0425 -3.250,-0.1752,0.01137,0.00428,-0.0380,0.8245,0.0452 -3.000,-0.1504,0.01102,0.00394,-0.0376,0.8226,0.0537 -2.750,-0.1291,0.01032,0.00363,-0.0368,0.8207,0.1436 -2.500,-0.1231,0.00836,0.00314,-0.0339,0.8184,0.5201 -2.250,-0.1065,0.00774,0.00321,-0.0317,0.8166,0.7140 -2.000,-0.0803,0.00778,0.00328,-0.0313,0.8152,0.7493 -1.750,-0.0540,0.00790,0.00343,-0.0308,0.8139,0.7754 -1.500,-0.0282,0.00808,0.00367,-0.0302,0.8124,0.7997 -1.250,-0.0019,0.00825,0.00387,-0.0297,0.8106,0.8151 -1.000,0.0240,0.00843,0.00409,-0.0291,0.8087,0.8292 -0.750,0.0503,0.00861,0.00427,-0.0286,0.8070,0.8406 -0.500,0.0774,0.00870,0.00438,-0.0284,0.8054,0.8462 -0.250,0.1050,0.00875,0.00442,-0.0284,0.8037,0.8509 0.000,0.1330,0.00878,0.00441,-0.0286,0.8021,0.8554 0.250,0.1613,0.00877,0.00440,-0.0288,0.8005,0.8579 0.500,0.1895,0.00882,0.00444,-0.0290,0.7989,0.8602 0.750,0.2171,0.00885,0.00450,-0.0292,0.7963,0.8627 1.000,0.2450,0.00886,0.00454,-0.0295,0.7935,0.8654 1.250,0.2731,0.00885,0.00453,-0.0297,0.7907,0.8685 1.500,0.3016,0.00882,0.00449,-0.0300,0.7881,0.8714 1.750,0.3301,0.00876,0.00445,-0.0302,0.7855,0.8735 2.000,0.3575,0.00875,0.00448,-0.0302,0.7817,0.8759 2.250,0.3849,0.00858,0.00433,-0.0300,0.7747,0.8786 2.500,0.4126,0.00833,0.00407,-0.0297,0.7654,0.8817 2.750,0.4409,0.00809,0.00379,-0.0295,0.7558,0.8851 3.000,0.4673,0.00781,0.00350,-0.0289,0.7405,0.8879 3.250,0.4923,0.00760,0.00332,-0.0281,0.7209,0.8907 3.500,0.5182,0.00751,0.00327,-0.0277,0.7032,0.8940 3.750,0.5433,0.00745,0.00320,-0.0271,0.6742,0.8979 4.000,0.5576,0.00784,0.00311,-0.0244,0.5518,0.9026 4.250,0.5549,0.00930,0.00373,-0.0191,0.3678,0.9092 4.500,0.5515,0.01086,0.00438,-0.0141,0.1735,0.9174 4.750,0.5544,0.01202,0.00498,-0.0099,0.0551,0.9249 5.000,0.5724,0.01241,0.00535,-0.0083,0.0441,0.9314 5.250,0.5874,0.01284,0.00581,-0.0059,0.0386,0.9383 5.500,0.6042,0.01318,0.00621,-0.0040,0.0362,0.9462 5.750,0.6197,0.01350,0.00659,-0.0018,0.0339,0.9552 6.000,0.6390,0.01392,0.00705,-0.0006,0.0317,0.9640 6.250,0.6578,0.01487,0.00804,0.0004,0.0292,0.9742 6.500,0.6864,0.01566,0.00890,-0.0006,0.0279,0.9806 6.750,0.7169,0.01641,0.00970,-0.0020,0.0268,0.9862 7.000,0.7486,0.01720,0.01054,-0.0035,0.0254,0.9908 7.250,0.7802,0.01794,0.01128,-0.0052,0.0238,0.9963 7.500,0.8003,0.01879,0.01213,-0.0045,0.0229,1.0000 8.000,0.8697,0.02230,0.01581,-0.0079,0.0214,1.0000 8.250,0.8858,0.02308,0.01668,-0.0061,0.0210,1.0000 8.500,0.9105,0.02446,0.01821,-0.0058,0.0206,1.0000 8.750,0.9325,0.02571,0.01961,-0.0052,0.0199,1.0000 9.000,0.9536,0.02714,0.02122,-0.0045,0.0192,1.0000 9.250,0.9742,0.02928,0.02358,-0.0037,0.0190,1.0000 9.500,0.9906,0.03205,0.02665,-0.0023,0.0190,1.0000 9.750,0.9984,0.03617,0.03120,0.0003,0.0197,1.0000 10.000,0.9978,0.04080,0.03620,0.0034,0.0207,1.0000 13.500,0.7323,0.12068,0.11840,0.0015,0.0233,1.0000 13.750,0.7273,0.12725,0.12495,-0.0019,0.0232,1.0000 14.000,0.7310,0.13048,0.12819,-0.0034,0.0227,1.0000 14.250,0.7331,0.13422,0.13193,-0.0049,0.0224,1.0000 15.000,0.5769,0.14458,0.14256,-0.0134,0.0228,1.0000 15.250,0.5815,0.14699,0.14497,-0.0146,0.0224,1.0000