Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-n63012a-il-100000 Airfoil,n63012a-il Reynolds number,100000 Ncrit,9 Mach,0 Max Cl/Cd,41.25 Max Cl/Cd alpha,5 Url,http://airfoiltools.com/polar/csv?polar=xf-n63012a-il-100000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.6451,0.10393,0.09898,0.0008,1.0000,0.1695 -10.000,-0.7116,0.06091,0.05593,-0.0347,1.0000,0.0882 -9.750,-0.7390,0.05556,0.05044,-0.0336,1.0000,0.0844 -9.500,-0.7820,0.04933,0.04370,-0.0300,1.0000,0.0758 -9.250,-0.8475,0.05545,0.04925,-0.0237,1.0000,0.0739 -9.000,-0.8659,0.05060,0.04324,-0.0191,1.0000,0.0659 -8.750,-0.8555,0.04768,0.03993,-0.0173,1.0000,0.0656 -8.500,-0.8453,0.04389,0.03581,-0.0156,1.0000,0.0658 -8.250,-0.8314,0.04062,0.03218,-0.0140,1.0000,0.0659 -8.000,-0.8145,0.03794,0.02913,-0.0124,1.0000,0.0656 -7.750,-0.7959,0.03474,0.02560,-0.0112,1.0000,0.0659 -7.500,-0.7740,0.03158,0.02225,-0.0104,1.0000,0.0670 -7.250,-0.7514,0.02947,0.02008,-0.0097,1.0000,0.0698 -7.000,-0.7290,0.02793,0.01843,-0.0087,1.0000,0.0740 -6.750,-0.7053,0.02642,0.01669,-0.0076,1.0000,0.0775 -6.500,-0.6811,0.02436,0.01475,-0.0069,1.0000,0.0822 -6.250,-0.6602,0.02319,0.01353,-0.0056,1.0000,0.0900 -6.000,-0.6425,0.02176,0.01228,-0.0039,1.0000,0.1002 -5.750,-0.6277,0.02048,0.01113,-0.0017,1.0000,0.1139 -5.500,-0.6162,0.01916,0.01003,0.0010,1.0000,0.1381 -5.250,-0.6115,0.01722,0.00876,0.0045,1.0000,0.2086 -5.000,-0.6175,0.01497,0.00823,0.0099,1.0000,0.4738 -4.750,-0.6054,0.01487,0.00841,0.0135,1.0000,0.5696 -4.500,-0.5896,0.01502,0.00858,0.0163,1.0000,0.6188 -4.250,-0.5728,0.01525,0.00882,0.0191,1.0000,0.6545 -4.000,-0.5558,0.01551,0.00907,0.0217,1.0000,0.6846 -3.750,-0.5391,0.01574,0.00925,0.0243,1.0000,0.7119 -3.500,-0.5221,0.01607,0.00960,0.0272,1.0000,0.7353 -3.250,-0.5062,0.01632,0.00983,0.0300,1.0000,0.7594 -3.000,-0.4900,0.01662,0.01013,0.0330,1.0000,0.7808 -2.750,-0.4743,0.01676,0.01022,0.0355,1.0000,0.8022 -2.500,-0.4580,0.01691,0.01033,0.0379,1.0000,0.8201 -2.250,-0.4413,0.01701,0.01040,0.0400,1.0000,0.8368 -2.000,-0.4049,0.01724,0.01054,0.0382,0.9942,0.8522 -1.750,-0.3622,0.01744,0.01062,0.0350,0.9854,0.8660 -1.500,-0.3200,0.01761,0.01071,0.0318,0.9764,0.8791 -1.250,-0.2686,0.01791,0.01091,0.0271,0.9700,0.8891 -1.000,-0.2248,0.01805,0.01099,0.0237,0.9607,0.9001 -0.750,-0.1739,0.01821,0.01108,0.0187,0.9538,0.9110 -0.500,-0.1188,0.01839,0.01121,0.0132,0.9462,0.9188 -0.250,-0.0581,0.01847,0.01126,0.0063,0.9411,0.9269 0.000,0.0000,0.01853,0.01132,0.0000,0.9333,0.9333 0.250,0.0580,0.01847,0.01126,-0.0063,0.9269,0.9411 0.500,0.1188,0.01838,0.01121,-0.0132,0.9188,0.9462 0.750,0.1738,0.01821,0.01107,-0.0187,0.9110,0.9538 1.000,0.2248,0.01805,0.01099,-0.0237,0.9001,0.9607 1.250,0.2686,0.01790,0.01091,-0.0271,0.8891,0.9700 1.500,0.3200,0.01761,0.01070,-0.0318,0.8791,0.9765 1.750,0.3621,0.01743,0.01062,-0.0350,0.8660,0.9855 2.000,0.4048,0.01724,0.01054,-0.0382,0.8522,0.9942 2.250,0.4409,0.01701,0.01039,-0.0400,0.8368,1.0000 2.500,0.4576,0.01691,0.01033,-0.0379,0.8201,1.0000 2.750,0.4739,0.01676,0.01021,-0.0354,0.8023,1.0000 3.000,0.4896,0.01661,0.01013,-0.0329,0.7809,1.0000 3.250,0.5058,0.01632,0.00983,-0.0300,0.7595,1.0000 3.500,0.5217,0.01607,0.00960,-0.0272,0.7355,1.0000 3.750,0.5386,0.01574,0.00925,-0.0243,0.7120,1.0000 4.000,0.5553,0.01551,0.00907,-0.0217,0.6848,1.0000 4.250,0.5723,0.01525,0.00882,-0.0190,0.6548,1.0000 4.500,0.5891,0.01502,0.00857,-0.0162,0.6192,1.0000 4.750,0.6049,0.01487,0.00841,-0.0134,0.5702,1.0000 5.000,0.6171,0.01496,0.00823,-0.0098,0.4753,1.0000 5.250,0.6113,0.01719,0.00875,-0.0044,0.2099,1.0000 5.500,0.6160,0.01915,0.01002,-0.0009,0.1383,1.0000 5.750,0.6275,0.02047,0.01112,0.0017,0.1140,1.0000 6.000,0.6423,0.02175,0.01227,0.0040,0.1002,1.0000 6.250,0.6600,0.02318,0.01352,0.0056,0.0901,1.0000 6.500,0.6809,0.02436,0.01475,0.0070,0.0822,1.0000 6.750,0.7052,0.02641,0.01668,0.0077,0.0776,1.0000 7.000,0.7289,0.02793,0.01843,0.0088,0.0740,1.0000 7.250,0.7514,0.02946,0.02008,0.0097,0.0698,1.0000 7.500,0.7740,0.03158,0.02225,0.0104,0.0670,1.0000 7.750,0.7959,0.03474,0.02561,0.0112,0.0659,1.0000 8.000,0.8146,0.03795,0.02912,0.0124,0.0656,1.0000 8.250,0.8316,0.04063,0.03219,0.0140,0.0659,1.0000 8.500,0.8455,0.04389,0.03581,0.0156,0.0658,1.0000 8.750,0.8558,0.04771,0.03997,0.0172,0.0656,1.0000 9.000,0.8663,0.05061,0.04326,0.0190,0.0659,1.0000 9.250,0.8480,0.05552,0.04932,0.0236,0.0739,1.0000 9.500,0.8552,0.06512,0.05914,0.0239,0.0912,1.0000 9.750,0.7387,0.05553,0.05042,0.0335,0.0845,1.0000 10.000,0.7115,0.06090,0.05592,0.0346,0.0882,1.0000