Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-m3-il-200000 Airfoil,m3-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,45.8039 Max Cl/Cd alpha,4.25 Url,http://www.airfoiltools.com/polar/csv?polar=xf-m3-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -12.500,-0.6450,0.09044,0.08670,-0.0275,1.0000,0.0592 -12.250,-0.9128,0.06896,0.06448,-0.0375,1.0000,0.0504 -12.000,-0.9334,0.06401,0.05939,-0.0377,1.0000,0.0500 -11.750,-0.9548,0.05973,0.05493,-0.0365,1.0000,0.0497 -11.500,-0.9752,0.05600,0.05099,-0.0337,1.0000,0.0493 -11.250,-0.9915,0.05233,0.04706,-0.0305,1.0000,0.0490 -11.000,-1.0018,0.04859,0.04300,-0.0276,1.0000,0.0488 -10.750,-1.0065,0.04513,0.03919,-0.0248,1.0000,0.0489 -10.500,-1.0058,0.04220,0.03589,-0.0221,1.0000,0.0494 -10.250,-1.0005,0.03971,0.03301,-0.0196,1.0000,0.0500 -10.000,-0.9918,0.03758,0.03051,-0.0173,1.0000,0.0506 -9.750,-0.9801,0.03576,0.02834,-0.0151,1.0000,0.0510 -9.500,-0.9652,0.03246,0.02480,-0.0139,1.0000,0.0517 -9.250,-0.9459,0.03049,0.02278,-0.0130,1.0000,0.0530 -9.000,-0.9266,0.02922,0.02142,-0.0119,1.0000,0.0543 -8.750,-0.9067,0.02796,0.02004,-0.0108,1.0000,0.0556 -8.500,-0.8863,0.02663,0.01857,-0.0096,1.0000,0.0567 -8.250,-0.8656,0.02541,0.01720,-0.0084,1.0000,0.0579 -8.000,-0.8450,0.02445,0.01608,-0.0071,1.0000,0.0593 -7.750,-0.8243,0.02337,0.01488,-0.0058,1.0000,0.0606 -7.500,-0.8036,0.02196,0.01351,-0.0048,1.0000,0.0624 -7.250,-0.7836,0.02106,0.01264,-0.0034,1.0000,0.0641 -7.000,-0.7640,0.02028,0.01183,-0.0020,1.0000,0.0661 -6.750,-0.7446,0.01958,0.01109,-0.0004,1.0000,0.0685 -6.500,-0.7255,0.01895,0.01040,0.0012,1.0000,0.0710 -6.250,-0.7094,0.01799,0.00953,0.0032,1.0000,0.0745 -6.000,-0.6915,0.01737,0.00891,0.0050,1.0000,0.0786 -5.750,-0.6741,0.01671,0.00824,0.0069,1.0000,0.0838 -5.500,-0.6572,0.01603,0.00762,0.0087,1.0000,0.0930 -5.250,-0.6411,0.01518,0.00696,0.0107,1.0000,0.1142 -5.000,-0.6254,0.01422,0.00636,0.0126,1.0000,0.1688 -4.750,-0.6082,0.01346,0.00597,0.0141,1.0000,0.2341 -4.500,-0.5896,0.01291,0.00571,0.0154,1.0000,0.2953 -4.250,-0.5700,0.01244,0.00551,0.0166,1.0000,0.3544 -4.000,-0.5498,0.01203,0.00536,0.0178,1.0000,0.4138 -3.750,-0.5290,0.01171,0.00528,0.0188,1.0000,0.4705 -3.500,-0.5079,0.01143,0.00524,0.0199,1.0000,0.5257 -3.250,-0.4866,0.01122,0.00526,0.0210,1.0000,0.5821 -3.000,-0.4652,0.01108,0.00536,0.0222,1.0000,0.6354 -2.750,-0.4437,0.01102,0.00548,0.0234,1.0000,0.6820 -2.500,-0.4075,0.01101,0.00561,0.0218,0.9959,0.7253 -2.250,-0.3683,0.01104,0.00573,0.0196,0.9903,0.7621 -2.000,-0.3289,0.01112,0.00590,0.0175,0.9844,0.7960 -1.750,-0.2918,0.01119,0.00603,0.0160,0.9775,0.8239 -1.500,-0.2516,0.01129,0.00616,0.0139,0.9714,0.8466 -1.250,-0.2154,0.01139,0.00628,0.0127,0.9637,0.8670 -1.000,-0.1737,0.01150,0.00639,0.0104,0.9578,0.8848 -0.750,-0.1329,0.01160,0.00649,0.0083,0.9510,0.8994 -0.500,-0.0891,0.01166,0.00654,0.0056,0.9444,0.9117 -0.250,-0.0411,0.01167,0.00654,0.0021,0.9398,0.9217 0.000,0.0000,0.01172,0.00659,0.0000,0.9298,0.9298 0.250,0.0411,0.01167,0.00654,-0.0021,0.9217,0.9398 0.500,0.0891,0.01166,0.00654,-0.0056,0.9117,0.9444 0.750,0.1329,0.01160,0.00649,-0.0083,0.8994,0.9510 1.000,0.1737,0.01150,0.00639,-0.0104,0.8848,0.9578 1.250,0.2154,0.01139,0.00628,-0.0127,0.8670,0.9637 1.500,0.2516,0.01129,0.00616,-0.0139,0.8466,0.9715 1.750,0.2919,0.01119,0.00603,-0.0160,0.8240,0.9775 2.000,0.3289,0.01111,0.00590,-0.0175,0.7960,0.9845 2.250,0.3683,0.01104,0.00573,-0.0196,0.7621,0.9903 2.500,0.4075,0.01101,0.00560,-0.0218,0.7252,0.9959 2.750,0.4435,0.01102,0.00548,-0.0234,0.6820,1.0000 3.000,0.4651,0.01107,0.00535,-0.0222,0.6354,1.0000 3.250,0.4865,0.01122,0.00526,-0.0210,0.5821,1.0000 3.500,0.5078,0.01143,0.00524,-0.0199,0.5259,1.0000 3.750,0.5288,0.01171,0.00527,-0.0188,0.4706,1.0000 4.000,0.5497,0.01203,0.00536,-0.0177,0.4137,1.0000 4.250,0.5698,0.01244,0.00550,-0.0166,0.3546,1.0000 4.500,0.5895,0.01290,0.00570,-0.0154,0.2954,1.0000 4.750,0.6081,0.01346,0.00597,-0.0141,0.2343,1.0000 5.000,0.6253,0.01421,0.00635,-0.0125,0.1690,1.0000 5.250,0.6410,0.01517,0.00695,-0.0107,0.1143,1.0000 5.500,0.6571,0.01602,0.00762,-0.0087,0.0931,1.0000 5.750,0.6740,0.01671,0.00824,-0.0069,0.0839,1.0000 6.000,0.6914,0.01737,0.00891,-0.0049,0.0786,1.0000 6.250,0.7093,0.01798,0.00952,-0.0032,0.0745,1.0000 6.500,0.7254,0.01895,0.01040,-0.0012,0.0710,1.0000 6.750,0.7446,0.01958,0.01109,0.0004,0.0685,1.0000 7.000,0.7639,0.02027,0.01183,0.0020,0.0661,1.0000 7.250,0.7836,0.02106,0.01263,0.0034,0.0641,1.0000 7.500,0.8035,0.02195,0.01351,0.0048,0.0624,1.0000 7.750,0.8242,0.02336,0.01487,0.0058,0.0606,1.0000 8.000,0.8450,0.02444,0.01607,0.0071,0.0593,1.0000 8.250,0.8656,0.02541,0.01720,0.0084,0.0579,1.0000 8.500,0.8863,0.02663,0.01857,0.0096,0.0567,1.0000 8.750,0.9067,0.02795,0.02004,0.0108,0.0556,1.0000 9.000,0.9267,0.02923,0.02143,0.0119,0.0543,1.0000 9.250,0.9460,0.03049,0.02278,0.0130,0.0529,1.0000 9.500,0.9653,0.03247,0.02481,0.0138,0.0517,1.0000 9.750,0.9802,0.03577,0.02834,0.0151,0.0510,1.0000 10.000,0.9920,0.03759,0.03051,0.0172,0.0506,1.0000 10.250,1.0007,0.03970,0.03301,0.0196,0.0500,1.0000 10.500,1.0059,0.04220,0.03589,0.0221,0.0493,1.0000 10.750,1.0067,0.04514,0.03920,0.0248,0.0488,1.0000 11.000,1.0020,0.04861,0.04302,0.0276,0.0488,1.0000 11.250,0.9918,0.05235,0.04709,0.0305,0.0490,1.0000 11.500,0.9755,0.05603,0.05103,0.0336,0.0493,1.0000 11.750,0.9550,0.05978,0.05498,0.0364,0.0497,1.0000 12.000,0.9337,0.06407,0.05945,0.0376,0.0500,1.0000 12.250,0.9131,0.06903,0.06456,0.0373,0.0504,1.0000