Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-vr1-il-50000-n5 Airfoil,vr1-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,30.0188 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-vr1-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.250,-0.5356,0.08837,0.08047,-0.0460,1.0000,0.0579 -10.000,-0.5393,0.08383,0.07597,-0.0480,1.0000,0.0574 -9.750,-0.5504,0.07886,0.07104,-0.0505,1.0000,0.0568 -9.500,-0.5658,0.07441,0.06659,-0.0519,1.0000,0.0563 -9.250,-0.5845,0.07067,0.06285,-0.0514,1.0000,0.0558 -9.000,-0.6014,0.06702,0.05913,-0.0502,1.0000,0.0554 -8.750,-0.6153,0.06347,0.05546,-0.0486,1.0000,0.0550 -8.500,-0.6261,0.06011,0.05195,-0.0465,1.0000,0.0546 -8.250,-0.6341,0.05687,0.04850,-0.0441,1.0000,0.0543 -8.000,-0.6392,0.05376,0.04515,-0.0416,1.0000,0.0541 -7.750,-0.6407,0.05090,0.04201,-0.0389,1.0000,0.0539 -7.500,-0.6399,0.04821,0.03903,-0.0362,1.0000,0.0538 -7.250,-0.6366,0.04575,0.03626,-0.0334,1.0000,0.0541 -7.000,-0.6309,0.04348,0.03368,-0.0308,1.0000,0.0547 -6.750,-0.6232,0.04135,0.03121,-0.0283,1.0000,0.0556 -6.500,-0.6132,0.03934,0.02884,-0.0258,1.0000,0.0564 -6.250,-0.6010,0.03749,0.02664,-0.0236,1.0000,0.0571 -6.000,-0.5866,0.03576,0.02457,-0.0216,1.0000,0.0577 -5.750,-0.5706,0.03420,0.02275,-0.0197,1.0000,0.0581 -5.500,-0.5537,0.03269,0.02115,-0.0181,1.0000,0.0590 -5.250,-0.5364,0.03143,0.01981,-0.0165,1.0000,0.0600 -5.000,-0.5187,0.03035,0.01863,-0.0149,1.0000,0.0613 -4.750,-0.5011,0.02940,0.01760,-0.0132,1.0000,0.0637 -4.500,-0.4831,0.02857,0.01663,-0.0116,1.0000,0.0664 -4.250,-0.4651,0.02780,0.01574,-0.0099,1.0000,0.0691 -4.000,-0.4452,0.02699,0.01492,-0.0089,0.9989,0.0722 -3.750,-0.4129,0.02623,0.01406,-0.0101,0.9932,0.0769 -3.500,-0.3814,0.02547,0.01325,-0.0113,0.9872,0.0845 -3.250,-0.3492,0.02471,0.01252,-0.0127,0.9816,0.1015 -3.000,-0.3205,0.02344,0.01172,-0.0137,0.9754,0.1687 -2.750,-0.2967,0.02181,0.01142,-0.0141,0.9702,0.4023 -2.500,-0.2829,0.02093,0.01210,-0.0096,0.9638,0.6949 -2.250,-0.2389,0.02158,0.01311,-0.0087,0.9618,0.8704 -2.000,-0.1684,0.02223,0.01344,-0.0154,0.9620,0.9325 -1.750,-0.1014,0.02248,0.01334,-0.0230,0.9608,0.9609 -1.500,-0.0420,0.02254,0.01312,-0.0299,0.9580,0.9804 -1.250,0.0195,0.02256,0.01291,-0.0374,0.9561,1.0000 -1.000,0.0428,0.02254,0.01276,-0.0379,0.9462,1.0000 -0.750,0.0743,0.02260,0.01268,-0.0397,0.9387,1.0000 -0.500,0.0968,0.02267,0.01265,-0.0397,0.9290,1.0000 -0.250,0.1255,0.02279,0.01267,-0.0407,0.9212,1.0000 0.000,0.1497,0.02293,0.01273,-0.0409,0.9122,1.0000 0.250,0.1780,0.02310,0.01283,-0.0416,0.9045,1.0000 0.500,0.2018,0.02329,0.01298,-0.0415,0.8956,1.0000 0.750,0.2323,0.02349,0.01314,-0.0425,0.8884,1.0000 1.000,0.2539,0.02373,0.01337,-0.0419,0.8790,1.0000 1.250,0.2849,0.02394,0.01358,-0.0429,0.8720,1.0000 1.500,0.3052,0.02422,0.01386,-0.0419,0.8621,1.0000 1.750,0.3335,0.02446,0.01413,-0.0423,0.8543,1.0000 2.000,0.3561,0.02474,0.01445,-0.0416,0.8446,1.0000 2.250,0.3802,0.02502,0.01478,-0.0412,0.8354,1.0000 2.500,0.4084,0.02523,0.01507,-0.0413,0.8265,1.0000 2.750,0.4281,0.02555,0.01548,-0.0400,0.8155,1.0000 3.000,0.4659,0.02556,0.01563,-0.0413,0.8075,1.0000 3.250,0.4950,0.02540,0.01559,-0.0407,0.7917,1.0000 3.500,0.5278,0.02449,0.01480,-0.0391,0.7635,1.0000 3.750,0.5687,0.02275,0.01313,-0.0374,0.7234,1.0000 4.000,0.5879,0.02217,0.01261,-0.0340,0.6876,1.0000 4.250,0.6058,0.02185,0.01237,-0.0308,0.6507,1.0000 4.500,0.6227,0.02156,0.01209,-0.0273,0.5994,1.0000 4.750,0.6403,0.02133,0.01155,-0.0236,0.4906,1.0000 5.000,0.6437,0.02259,0.01143,-0.0184,0.2948,1.0000 5.500,0.6512,0.02580,0.01350,-0.0116,0.1740,1.0000 5.750,0.6623,0.02703,0.01454,-0.0092,0.1524,1.0000 6.000,0.6757,0.02819,0.01559,-0.0072,0.1371,1.0000 6.250,0.6918,0.02932,0.01668,-0.0054,0.1250,1.0000 6.500,0.7111,0.03049,0.01778,-0.0042,0.1155,1.0000 6.750,0.7348,0.03161,0.01893,-0.0035,0.1064,1.0000 7.000,0.7649,0.03290,0.02026,-0.0036,0.0993,1.0000 7.250,0.7939,0.03419,0.02163,-0.0036,0.0930,1.0000 7.500,0.8236,0.03575,0.02317,-0.0039,0.0878,1.0000 7.750,0.8525,0.03746,0.02515,-0.0039,0.0839,1.0000 8.000,0.8776,0.03921,0.02706,-0.0036,0.0805,1.0000 8.250,0.9005,0.04098,0.02886,-0.0032,0.0775,1.0000 8.500,0.9198,0.04307,0.03120,-0.0023,0.0750,1.0000 8.750,0.9359,0.04535,0.03390,-0.0009,0.0730,1.0000 9.000,0.9497,0.04787,0.03678,0.0007,0.0716,1.0000 9.250,0.9603,0.05047,0.03972,0.0024,0.0705,1.0000 9.500,0.9680,0.05306,0.04261,0.0043,0.0693,1.0000 9.750,0.9742,0.05555,0.04534,0.0061,0.0680,1.0000 10.000,0.9812,0.05796,0.04791,0.0077,0.0667,1.0000 10.250,0.9875,0.06051,0.05057,0.0092,0.0654,1.0000 10.500,0.9846,0.06359,0.05385,0.0113,0.0648,1.0000 10.750,0.9712,0.06675,0.05733,0.0143,0.0645,1.0000 11.000,0.9542,0.07003,0.06085,0.0171,0.0644,1.0000 11.250,0.9363,0.07363,0.06465,0.0189,0.0644,1.0000 11.500,0.9158,0.07772,0.06894,0.0198,0.0645,1.0000 11.750,0.8943,0.08237,0.07375,0.0195,0.0646,1.0000 12.000,0.8717,0.08772,0.07924,0.0181,0.0648,1.0000