Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-p51htip-il-200000 Airfoil,p51htip-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,52.5457 Max Cl/Cd alpha,4.25 Url,http://airfoiltools.com/polar/csv?polar=xf-p51htip-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.4689,0.09313,0.08972,-0.0499,1.0000,0.0522 -10.250,-0.4747,0.08826,0.08490,-0.0533,1.0000,0.0534 -10.000,-0.4919,0.08353,0.08026,-0.0561,1.0000,0.0542 -9.750,-0.5232,0.08143,0.07824,-0.0536,0.9991,0.0534 -9.500,-0.5306,0.07416,0.07086,-0.0625,0.9919,0.0540 -9.250,-0.5465,0.06836,0.06478,-0.0691,0.9830,0.0559 -9.000,-0.4645,0.04832,0.04482,-0.0792,0.9731,0.0610 -8.750,-0.4665,0.04503,0.04145,-0.0788,0.9660,0.0625 -8.500,-0.4657,0.04125,0.03749,-0.0791,0.9610,0.0651 -8.250,-0.4858,0.04073,0.03637,-0.0747,0.9502,0.0704 -8.000,-0.4856,0.03401,0.02954,-0.0746,0.9469,0.0724 -7.750,-0.4717,0.03103,0.02662,-0.0742,0.9431,0.0745 -7.500,-0.4634,0.02883,0.02431,-0.0726,0.9376,0.0782 -7.250,-0.4640,0.02593,0.02097,-0.0698,0.9327,0.0868 -7.000,-0.4496,0.02372,0.01880,-0.0690,0.9293,0.0903 -6.750,-0.4490,0.02212,0.01685,-0.0656,0.9234,0.1009 -6.500,-0.4303,0.02023,0.01501,-0.0652,0.9209,0.1082 -6.250,-0.4335,0.02823,0.02072,-0.0594,0.9226,0.0465 -6.000,-0.4076,0.02733,0.01957,-0.0588,0.9202,0.0456 -5.750,-0.3801,0.02569,0.01771,-0.0587,0.9184,0.0454 -5.500,-0.3497,0.02282,0.01473,-0.0596,0.9173,0.0481 -5.250,-0.3323,0.02202,0.01388,-0.0580,0.9130,0.0495 -5.000,-0.3084,0.02113,0.01292,-0.0574,0.9100,0.0508 -4.750,-0.2834,0.02033,0.01208,-0.0569,0.9078,0.0530 -4.500,-0.2583,0.01984,0.01152,-0.0566,0.9058,0.0565 -4.250,-0.2359,0.01895,0.01064,-0.0558,0.9040,0.0596 -4.000,-0.2203,0.01852,0.01024,-0.0539,0.9013,0.0630 -3.750,-0.2122,0.01845,0.01015,-0.0506,0.8965,0.0670 -3.500,-0.1966,0.01815,0.00983,-0.0486,0.8936,0.0738 -3.250,-0.1772,0.01783,0.00950,-0.0473,0.8914,0.0862 -3.000,-0.1709,0.01625,0.00901,-0.0442,0.8891,0.3072 -2.750,-0.1949,0.01525,0.00941,-0.0350,0.8833,0.6008 -2.500,-0.1905,0.01566,0.01033,-0.0292,0.8798,0.7698 -2.250,-0.1720,0.01618,0.01083,-0.0264,0.8774,0.8111 -2.000,-0.1516,0.01683,0.01147,-0.0236,0.8757,0.8407 -1.750,-0.1287,0.01785,0.01252,-0.0201,0.8744,0.8724 -1.500,-0.0777,0.01918,0.01381,-0.0216,0.8745,0.8978 -1.250,-0.0062,0.01980,0.01431,-0.0293,0.8752,0.9069 -1.000,-0.0060,0.01999,0.01447,-0.0245,0.8712,0.9167 -0.750,0.0302,0.02024,0.01467,-0.0268,0.8686,0.9197 -0.500,0.0633,0.02040,0.01478,-0.0285,0.8661,0.9234 -0.250,0.0708,0.02043,0.01478,-0.0249,0.8623,0.9312 0.000,0.1173,0.02045,0.01477,-0.0291,0.8612,0.9323 0.250,0.1619,0.02044,0.01473,-0.0329,0.8602,0.9335 0.500,0.2050,0.02040,0.01468,-0.0362,0.8591,0.9349 0.750,0.1805,0.02092,0.01522,-0.0273,0.8495,0.9457 1.000,0.2226,0.02089,0.01520,-0.0306,0.8476,0.9467 1.250,0.2653,0.02082,0.01515,-0.0338,0.8459,0.9476 1.500,0.3086,0.02071,0.01506,-0.0370,0.8445,0.9486 1.750,0.3107,0.02117,0.01556,-0.0333,0.8358,0.9553 2.000,0.3380,0.02105,0.01549,-0.0333,0.8322,0.9589 2.250,0.3837,0.02079,0.01528,-0.0367,0.8303,0.9594 2.500,0.4121,0.02097,0.01554,-0.0377,0.8235,0.9621 2.750,0.4503,0.02071,0.01538,-0.0397,0.8187,0.9635 3.000,0.5121,0.01886,0.01359,-0.0434,0.8141,0.9612 3.250,0.5522,0.01692,0.01171,-0.0431,0.7950,0.9618 3.500,0.5936,0.01451,0.00923,-0.0422,0.7707,0.9624 3.750,0.6234,0.01353,0.00831,-0.0414,0.7458,0.9655 4.000,0.6485,0.01280,0.00762,-0.0400,0.7139,0.9696 4.250,0.6605,0.01257,0.00650,-0.0356,0.5047,0.9742 4.500,0.6427,0.01570,0.00766,-0.0293,0.1507,0.9829 4.750,0.6595,0.01723,0.00865,-0.0285,0.0723,0.9876 5.000,0.6845,0.01807,0.00948,-0.0289,0.0612,0.9921 5.250,0.7110,0.01881,0.01030,-0.0295,0.0557,0.9960 5.500,0.7379,0.01971,0.01120,-0.0302,0.0517,0.9997 5.750,0.7422,0.02047,0.01195,-0.0264,0.0499,1.0000 6.000,0.7483,0.02149,0.01296,-0.0229,0.0480,1.0000 6.250,0.7547,0.02188,0.01341,-0.0193,0.0464,1.0000 6.500,0.7640,0.02248,0.01406,-0.0161,0.0447,1.0000 6.750,0.7805,0.02337,0.01502,-0.0142,0.0435,1.0000 7.000,0.8036,0.02455,0.01627,-0.0133,0.0425,1.0000 7.250,0.8292,0.02600,0.01781,-0.0129,0.0417,1.0000 7.500,0.8497,0.02737,0.01929,-0.0116,0.0408,1.0000 7.750,0.8684,0.02892,0.02088,-0.0104,0.0392,1.0000 8.000,0.8899,0.03107,0.02323,-0.0094,0.0389,1.0000 8.250,0.9074,0.03306,0.02554,-0.0072,0.0398,1.0000 8.500,0.9205,0.03807,0.03128,-0.0040,0.0457,1.0000 13.500,0.5963,0.12709,0.12384,0.0079,0.0603,1.0000 13.750,0.5776,0.13218,0.12892,0.0033,0.0600,1.0000 14.000,0.5527,0.13736,0.13407,-0.0030,0.0587,1.0000