Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-p51htip-il-200000-n5 Airfoil,p51htip-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,47.9875 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-p51htip-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.500,-0.5289,0.06967,0.06610,-0.0680,0.9694,0.0181 -10.250,-0.5448,0.06289,0.05914,-0.0733,0.9529,0.0179 -10.000,-0.5625,0.05803,0.05408,-0.0744,0.9376,0.0178 -9.750,-0.5795,0.05445,0.05029,-0.0726,0.9246,0.0177 -9.500,-0.5953,0.05127,0.04689,-0.0693,0.9144,0.0175 -9.250,-0.6061,0.04761,0.04294,-0.0664,0.9060,0.0175 -9.000,-0.6117,0.04404,0.03903,-0.0636,0.8993,0.0177 -8.750,-0.6126,0.04063,0.03525,-0.0608,0.8931,0.0178 -8.500,-0.6098,0.03742,0.03164,-0.0580,0.8884,0.0180 -8.250,-0.6022,0.03435,0.02813,-0.0558,0.8830,0.0184 -8.000,-0.5908,0.03177,0.02504,-0.0536,0.8783,0.0193 -7.750,-0.5764,0.02973,0.02255,-0.0517,0.8748,0.0199 -7.500,-0.5582,0.02773,0.02033,-0.0509,0.8716,0.0204 -7.250,-0.5374,0.02623,0.01864,-0.0502,0.8680,0.0209 -7.000,-0.5154,0.02490,0.01711,-0.0496,0.8649,0.0215 -6.750,-0.4924,0.02367,0.01568,-0.0490,0.8622,0.0222 -6.500,-0.4685,0.02251,0.01434,-0.0485,0.8599,0.0232 -6.250,-0.4437,0.02149,0.01315,-0.0481,0.8576,0.0243 -6.000,-0.4186,0.02083,0.01233,-0.0478,0.8546,0.0258 -5.750,-0.3941,0.01961,0.01105,-0.0476,0.8519,0.0274 -5.500,-0.3706,0.01876,0.01018,-0.0471,0.8492,0.0287 -5.250,-0.3473,0.01810,0.00946,-0.0465,0.8468,0.0302 -5.000,-0.3239,0.01759,0.00889,-0.0459,0.8447,0.0326 -4.750,-0.3006,0.01705,0.00829,-0.0453,0.8425,0.0342 -4.500,-0.2775,0.01658,0.00776,-0.0447,0.8398,0.0355 -4.250,-0.2571,0.01589,0.00705,-0.0437,0.8371,0.0378 -4.000,-0.2343,0.01549,0.00663,-0.0431,0.8348,0.0414 -3.750,-0.2106,0.01517,0.00624,-0.0426,0.8328,0.0452 -3.500,-0.1870,0.01483,0.00584,-0.0419,0.8310,0.0495 -3.250,-0.1633,0.01450,0.00548,-0.0413,0.8293,0.0586 -3.000,-0.1424,0.01397,0.00522,-0.0405,0.8265,0.1082 -2.750,-0.1303,0.01276,0.00490,-0.0386,0.8236,0.3183 -2.500,-0.1244,0.01143,0.00477,-0.0349,0.8208,0.5820 -2.250,-0.1059,0.01142,0.00526,-0.0322,0.8189,0.7393 -2.000,-0.0832,0.01173,0.00566,-0.0304,0.8172,0.7873 -1.750,-0.0595,0.01202,0.00594,-0.0288,0.8157,0.8133 -1.500,-0.0344,0.01232,0.00621,-0.0275,0.8143,0.8307 -1.250,-0.0106,0.01248,0.00633,-0.0268,0.8119,0.8410 -1.000,0.0160,0.01260,0.00642,-0.0266,0.8097,0.8450 -0.750,0.0423,0.01267,0.00647,-0.0265,0.8075,0.8492 -0.500,0.0681,0.01269,0.00644,-0.0263,0.8054,0.8537 -0.250,0.0945,0.01269,0.00640,-0.0263,0.8035,0.8573 0.000,0.1223,0.01272,0.00640,-0.0265,0.8020,0.8596 0.250,0.1501,0.01272,0.00639,-0.0266,0.8005,0.8622 0.500,0.1770,0.01275,0.00641,-0.0266,0.7987,0.8653 0.750,0.2005,0.01287,0.00655,-0.0263,0.7950,0.8694 1.000,0.2260,0.01293,0.00663,-0.0261,0.7921,0.8725 1.250,0.2532,0.01296,0.00669,-0.0261,0.7896,0.8748 1.500,0.2809,0.01296,0.00671,-0.0262,0.7875,0.8775 1.750,0.3091,0.01294,0.00671,-0.0263,0.7855,0.8808 2.000,0.3326,0.01303,0.00687,-0.0259,0.7814,0.8851 2.250,0.3576,0.01310,0.00700,-0.0255,0.7771,0.8881 2.500,0.3855,0.01306,0.00702,-0.0255,0.7737,0.8907 2.750,0.4151,0.01293,0.00695,-0.0258,0.7708,0.8934 3.000,0.4376,0.01297,0.00708,-0.0249,0.7636,0.8978 3.250,0.4660,0.01248,0.00661,-0.0244,0.7520,0.9016 3.500,0.4921,0.01195,0.00613,-0.0232,0.7316,0.9045 3.750,0.5164,0.01150,0.00568,-0.0218,0.7017,0.9082 4.000,0.5365,0.01118,0.00526,-0.0197,0.6328,0.9133 4.250,0.5405,0.01187,0.00491,-0.0147,0.4460,0.9194 4.500,0.5399,0.01305,0.00543,-0.0100,0.3101,0.9281 4.750,0.5434,0.01427,0.00603,-0.0064,0.1795,0.9363 5.000,0.5507,0.01540,0.00665,-0.0035,0.0777,0.9459 5.500,0.5931,0.01661,0.00775,-0.0023,0.0435,0.9598 5.750,0.6176,0.01731,0.00847,-0.0024,0.0387,0.9660 6.000,0.6429,0.01784,0.00910,-0.0027,0.0352,0.9733 6.250,0.6700,0.01852,0.00984,-0.0035,0.0323,0.9797 6.500,0.6950,0.01937,0.01073,-0.0040,0.0303,0.9876 6.750,0.7181,0.02057,0.01197,-0.0043,0.0286,0.9982 7.000,0.7289,0.02107,0.01252,-0.0018,0.0277,1.0000 7.250,0.7427,0.02163,0.01313,0.0002,0.0263,1.0000 7.500,0.7593,0.02234,0.01388,0.0016,0.0250,1.0000 7.750,0.7780,0.02319,0.01477,0.0027,0.0239,1.0000 8.000,0.7984,0.02411,0.01574,0.0034,0.0231,1.0000 8.250,0.8209,0.02519,0.01684,0.0039,0.0224,1.0000 8.500,0.8499,0.02680,0.01850,0.0032,0.0216,1.0000 8.750,0.8797,0.02852,0.02038,0.0024,0.0209,1.0000 9.000,0.9012,0.02969,0.02177,0.0031,0.0202,1.0000 9.250,0.9220,0.03109,0.02340,0.0037,0.0193,1.0000 9.500,0.9419,0.03279,0.02533,0.0044,0.0186,1.0000 9.750,0.9588,0.03466,0.02745,0.0055,0.0181,1.0000 10.000,0.9718,0.03658,0.02962,0.0071,0.0177,1.0000 10.250,0.9816,0.03850,0.03177,0.0090,0.0174,1.0000 10.500,0.9882,0.04057,0.03406,0.0111,0.0172,1.0000 10.750,0.9908,0.04290,0.03667,0.0136,0.0170,1.0000 11.000,0.9907,0.04516,0.03916,0.0162,0.0168,1.0000 11.250,0.9894,0.04725,0.04142,0.0185,0.0166,1.0000 11.500,0.9860,0.04953,0.04388,0.0208,0.0164,1.0000 11.750,0.9804,0.05204,0.04654,0.0227,0.0161,1.0000 12.000,0.9694,0.05531,0.05000,0.0247,0.0159,1.0000 12.250,0.9549,0.05877,0.05368,0.0264,0.0159,1.0000 12.500,0.9352,0.06277,0.05795,0.0277,0.0158,1.0000 12.750,0.9153,0.06722,0.06265,0.0281,0.0157,1.0000 13.000,0.8930,0.07237,0.06802,0.0276,0.0157,1.0000 13.250,0.8703,0.07818,0.07401,0.0258,0.0157,1.0000 13.500,0.8521,0.08406,0.08001,0.0233,0.0158,1.0000 13.750,0.8280,0.09191,0.08802,0.0188,0.0158,1.0000