Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-naca001264-il-100000-n5 Airfoil,naca001264-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,32.2036 Max Cl/Cd alpha,3.5 Url,http://airfoiltools.com/polar/csv?polar=xf-naca001264-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.750,-0.7594,0.08725,0.08155,-0.0367,1.0000,0.0445 -12.500,-0.8158,0.07417,0.06826,-0.0454,1.0000,0.0436 -12.250,-0.8538,0.06691,0.06076,-0.0479,1.0000,0.0433 -12.000,-0.8824,0.06190,0.05553,-0.0476,1.0000,0.0433 -11.750,-0.9053,0.05803,0.05140,-0.0456,1.0000,0.0435 -11.500,-0.9245,0.05480,0.04793,-0.0425,1.0000,0.0439 -11.250,-0.9408,0.05201,0.04487,-0.0384,1.0000,0.0443 -11.000,-0.9520,0.04924,0.04179,-0.0345,1.0000,0.0448 -10.750,-0.9583,0.04654,0.03873,-0.0309,1.0000,0.0455 -10.500,-0.9616,0.04409,0.03587,-0.0272,1.0000,0.0465 -10.250,-0.9618,0.04190,0.03326,-0.0236,1.0000,0.0475 -10.000,-0.9504,0.04017,0.03149,-0.0218,1.0000,0.0485 -9.750,-0.9395,0.03872,0.02993,-0.0197,1.0000,0.0495 -9.500,-0.9281,0.03720,0.02823,-0.0175,1.0000,0.0505 -9.250,-0.9156,0.03569,0.02653,-0.0153,1.0000,0.0515 -9.000,-0.9024,0.03434,0.02497,-0.0131,1.0000,0.0531 -8.750,-0.8881,0.03303,0.02342,-0.0111,1.0000,0.0548 -8.500,-0.8723,0.03174,0.02186,-0.0091,1.0000,0.0562 -8.250,-0.8545,0.03037,0.02037,-0.0076,1.0000,0.0574 -8.000,-0.8370,0.02919,0.01918,-0.0061,1.0000,0.0587 -7.750,-0.8198,0.02821,0.01814,-0.0044,1.0000,0.0601 -7.500,-0.8029,0.02734,0.01722,-0.0026,1.0000,0.0621 -7.250,-0.7859,0.02653,0.01631,-0.0008,1.0000,0.0646 -7.000,-0.7685,0.02574,0.01539,0.0010,1.0000,0.0670 -6.750,-0.7522,0.02483,0.01446,0.0029,1.0000,0.0691 -6.500,-0.7368,0.02405,0.01370,0.0049,1.0000,0.0715 -6.250,-0.7212,0.02336,0.01299,0.0070,1.0000,0.0745 -6.000,-0.7054,0.02272,0.01228,0.0091,1.0000,0.0781 -5.750,-0.6906,0.02204,0.01161,0.0113,1.0000,0.0826 -5.500,-0.6751,0.02146,0.01103,0.0133,1.0000,0.0890 -5.250,-0.6594,0.02087,0.01046,0.0153,1.0000,0.0966 -5.000,-0.6430,0.02035,0.00993,0.0172,1.0000,0.1067 -4.750,-0.6265,0.01980,0.00946,0.0191,1.0000,0.1195 -4.500,-0.6094,0.01930,0.00904,0.0208,1.0000,0.1381 -4.250,-0.5921,0.01879,0.00868,0.0224,1.0000,0.1659 -4.000,-0.5694,0.01818,0.00832,0.0227,0.9983,0.2109 -3.750,-0.5415,0.01729,0.00794,0.0218,0.9946,0.2987 -3.500,-0.5188,0.01612,0.00769,0.0221,0.9904,0.4614 -3.250,-0.4930,0.01553,0.00784,0.0228,0.9866,0.6114 -3.000,-0.4604,0.01552,0.00808,0.0224,0.9833,0.6925 -2.750,-0.4296,0.01562,0.00826,0.0223,0.9786,0.7419 -2.500,-0.3952,0.01583,0.00849,0.0215,0.9746,0.7803 -2.250,-0.3603,0.01614,0.00879,0.0207,0.9710,0.8151 -2.000,-0.3272,0.01647,0.00910,0.0203,0.9661,0.8422 -1.750,-0.2910,0.01679,0.00935,0.0191,0.9621,0.8641 -1.500,-0.2484,0.01729,0.00982,0.0169,0.9598,0.8850 -1.250,-0.2077,0.01770,0.01017,0.0148,0.9562,0.9009 -1.000,-0.1691,0.01786,0.01027,0.0126,0.9512,0.9107 -0.750,-0.1256,0.01795,0.01031,0.0093,0.9476,0.9166 -0.500,-0.0789,0.01803,0.01035,0.0052,0.9448,0.9216 -0.250,-0.0476,0.01805,0.01035,0.0043,0.9372,0.9300 0.000,0.0000,0.01807,0.01037,0.0000,0.9333,0.9333 0.250,0.0475,0.01805,0.01035,-0.0043,0.9300,0.9372 0.500,0.0789,0.01803,0.01035,-0.0052,0.9216,0.9448 0.750,0.1256,0.01795,0.01031,-0.0093,0.9166,0.9476 1.000,0.1691,0.01786,0.01027,-0.0127,0.9107,0.9512 1.250,0.2076,0.01770,0.01016,-0.0148,0.9009,0.9562 1.500,0.2483,0.01729,0.00982,-0.0169,0.8850,0.9598 1.750,0.2910,0.01679,0.00935,-0.0191,0.8642,0.9621 2.000,0.3272,0.01647,0.00909,-0.0203,0.8422,0.9661 2.250,0.3603,0.01614,0.00878,-0.0207,0.8152,0.9711 2.500,0.3952,0.01583,0.00849,-0.0215,0.7804,0.9746 2.750,0.4296,0.01562,0.00826,-0.0223,0.7421,0.9786 3.000,0.4603,0.01552,0.00807,-0.0224,0.6925,0.9833 3.250,0.4930,0.01553,0.00784,-0.0228,0.6115,0.9866 3.500,0.5188,0.01611,0.00769,-0.0221,0.4615,0.9905 3.750,0.5415,0.01729,0.00794,-0.0219,0.2985,0.9946 4.000,0.5694,0.01817,0.00832,-0.0228,0.2109,0.9984 4.250,0.5920,0.01878,0.00868,-0.0223,0.1660,1.0000 4.500,0.6093,0.01929,0.00904,-0.0207,0.1381,1.0000 4.750,0.6264,0.01979,0.00946,-0.0190,0.1195,1.0000 5.000,0.6429,0.02034,0.00992,-0.0172,0.1068,1.0000 5.250,0.6593,0.02087,0.01045,-0.0153,0.0967,1.0000 5.500,0.6750,0.02146,0.01103,-0.0133,0.0890,1.0000 5.750,0.6905,0.02203,0.01161,-0.0112,0.0826,1.0000 6.000,0.7053,0.02271,0.01228,-0.0091,0.0781,1.0000 6.250,0.7211,0.02336,0.01299,-0.0070,0.0745,1.0000 6.500,0.7367,0.02405,0.01370,-0.0049,0.0715,1.0000 6.750,0.7521,0.02483,0.01446,-0.0029,0.0691,1.0000 7.000,0.7684,0.02574,0.01539,-0.0010,0.0670,1.0000 7.250,0.7858,0.02652,0.01631,0.0009,0.0646,1.0000 7.500,0.8029,0.02733,0.01721,0.0027,0.0621,1.0000 7.750,0.8197,0.02820,0.01814,0.0044,0.0601,1.0000 8.000,0.8369,0.02919,0.01918,0.0061,0.0587,1.0000 8.250,0.8545,0.03036,0.02036,0.0076,0.0574,1.0000 8.500,0.8723,0.03173,0.02186,0.0091,0.0562,1.0000 8.750,0.8880,0.03302,0.02342,0.0111,0.0548,1.0000 9.000,0.9023,0.03434,0.02496,0.0132,0.0531,1.0000 9.250,0.9156,0.03568,0.02653,0.0153,0.0515,1.0000 9.500,0.9281,0.03719,0.02823,0.0175,0.0505,1.0000 9.750,0.9395,0.03872,0.02993,0.0197,0.0495,1.0000 10.000,0.9505,0.04016,0.03148,0.0218,0.0485,1.0000 10.250,0.9619,0.04190,0.03326,0.0236,0.0475,1.0000 10.500,0.9618,0.04409,0.03587,0.0272,0.0465,1.0000 10.750,0.9584,0.04655,0.03874,0.0309,0.0455,1.0000 11.000,0.9522,0.04925,0.04180,0.0345,0.0448,1.0000 11.250,0.9412,0.05202,0.04489,0.0383,0.0443,1.0000 11.500,0.9249,0.05483,0.04796,0.0424,0.0439,1.0000 11.750,0.9058,0.05805,0.05143,0.0455,0.0435,1.0000 12.000,0.8829,0.06194,0.05557,0.0474,0.0433,1.0000 12.250,0.8543,0.06698,0.06083,0.0477,0.0433,1.0000 12.500,0.8162,0.07428,0.06837,0.0451,0.0436,1.0000 12.750,0.7593,0.08756,0.08187,0.0363,0.0446,1.0000