Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-vr8-il-1000000 Airfoil,vr8-il Reynolds number,1000000 Ncrit,9 Mach,0 Max Cl/Cd,123.19 Max Cl/Cd alpha,7.25 Url,http://www.airfoiltools.com/polar/csv?polar=xf-vr8-il-1000000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.750,-0.4682,0.11061,0.10907,0.0031,1.0000,0.0084 -10.500,-0.4673,0.10606,0.10453,0.0013,1.0000,0.0089 -6.250,-0.5444,0.02960,0.02659,-0.0230,1.0000,0.0093 -6.000,-0.5333,0.02554,0.02217,-0.0205,1.0000,0.0093 -5.750,-0.5214,0.02166,0.01790,-0.0180,1.0000,0.0089 -5.500,-0.4999,0.01766,0.01336,-0.0167,0.9988,0.0092 -5.250,-0.4517,0.01507,0.01029,-0.0213,0.9890,0.0104 -5.000,-0.4122,0.01422,0.00946,-0.0243,0.9742,0.0111 -4.750,-0.3753,0.01330,0.00842,-0.0263,0.9471,0.0119 -4.500,-0.3469,0.01261,0.00746,-0.0261,0.8934,0.0129 -4.250,-0.3234,0.01320,0.00770,-0.0248,0.8226,0.0141 -4.000,-0.3021,0.01157,0.00590,-0.0239,0.7754,0.0167 -3.750,-0.2769,0.01164,0.00573,-0.0234,0.7308,0.0207 -3.500,-0.2525,0.01075,0.00464,-0.0226,0.6946,0.0207 -3.250,-0.2286,0.00992,0.00363,-0.0218,0.6582,0.0214 -3.000,-0.2043,0.00956,0.00302,-0.0212,0.6027,0.0228 -2.750,-0.1805,0.00963,0.00260,-0.0205,0.4782,0.0234 -2.500,-0.1600,0.01072,0.00245,-0.0198,0.0459,0.0231 -2.250,-0.1330,0.01050,0.00214,-0.0196,0.0396,0.0233 -2.000,-0.1058,0.01033,0.00190,-0.0194,0.0362,0.0229 -1.750,-0.0784,0.01019,0.00169,-0.0193,0.0359,0.0225 -1.500,-0.0510,0.01007,0.00151,-0.0192,0.0355,0.0223 -1.250,-0.0234,0.00998,0.00136,-0.0192,0.0352,0.0225 -1.000,0.0042,0.00992,0.00123,-0.0191,0.0351,0.0233 -0.750,0.0318,0.00988,0.00115,-0.0190,0.0350,0.0242 -0.500,0.0593,0.00983,0.00109,-0.0190,0.0350,0.0265 -0.250,0.0870,0.00981,0.00107,-0.0190,0.0339,0.0269 0.000,0.1146,0.00980,0.00104,-0.0190,0.0325,0.0341 0.250,0.1422,0.00981,0.00098,-0.0189,0.0284,0.0366 0.500,0.1693,0.00996,0.00096,-0.0188,0.0276,0.0409 0.750,0.1973,0.00988,0.00102,-0.0189,0.0251,0.0406 1.000,0.2249,0.00990,0.00105,-0.0189,0.0245,0.0416 1.250,0.2525,0.00993,0.00110,-0.0189,0.0243,0.0449 1.500,0.2772,0.00868,0.00110,-0.0192,0.0241,0.5062 1.750,0.3036,0.00832,0.00120,-0.0192,0.0238,0.6484 2.000,0.3267,0.00777,0.00133,-0.0182,0.0234,0.8439 2.250,0.3377,0.00768,0.00153,-0.0138,0.0233,0.9407 2.500,0.3581,0.00785,0.00172,-0.0119,0.0230,0.9783 2.750,0.3969,0.00796,0.00185,-0.0143,0.0229,0.9890 3.000,0.4724,0.00809,0.00197,-0.0249,0.0232,0.9994 3.250,0.5000,0.00825,0.00214,-0.0249,0.0233,1.0000 3.500,0.5239,0.00843,0.00237,-0.0241,0.0237,1.0000 3.750,0.5479,0.00864,0.00260,-0.0234,0.0241,1.0000 4.000,0.5719,0.00885,0.00286,-0.0226,0.0245,1.0000 4.250,0.5957,0.00910,0.00315,-0.0218,0.0251,1.0000 4.500,0.6192,0.00938,0.00349,-0.0209,0.0256,1.0000 4.750,0.6424,0.00971,0.00387,-0.0200,0.0256,1.0000 5.000,0.6651,0.01010,0.00431,-0.0190,0.0252,1.0000 5.250,0.6876,0.01052,0.00478,-0.0180,0.0255,1.0000 5.500,0.7096,0.01101,0.00532,-0.0169,0.0255,1.0000 5.750,0.7308,0.01159,0.00597,-0.0157,0.0251,1.0000 6.000,0.7476,0.01282,0.00728,-0.0138,0.0236,1.0000 6.250,0.7687,0.01354,0.00806,-0.0126,0.0213,1.0000 6.500,0.7828,0.01734,0.01176,-0.0108,0.0183,1.0000 6.750,0.8081,0.01596,0.01042,-0.0105,0.0153,1.0000 7.000,0.8061,0.00693,0.00158,-0.0081,0.0131,1.0000 7.250,0.8303,0.00674,0.00158,-0.0076,0.0118,1.0000 7.500,0.8530,0.00706,0.00196,-0.0072,0.0107,1.0000 7.750,0.8757,0.00748,0.00235,-0.0069,0.0101,1.0000 8.000,0.8975,0.00901,0.00380,-0.0066,0.0096,1.0000 8.250,0.9182,0.00911,0.00433,-0.0054,0.0083,1.0000 8.500,0.9397,0.00985,0.00523,-0.0048,0.0076,1.0000 8.750,0.9606,0.01047,0.00595,-0.0042,0.0072,1.0000 9.000,0.9827,0.01075,0.00628,-0.0039,0.0069,1.0000 9.250,0.9986,0.01229,0.00802,-0.0029,0.0065,1.0000 9.500,1.0141,0.01406,0.01001,-0.0017,0.0062,1.0000 9.750,1.0258,0.01656,0.01281,-0.0002,0.0056,1.0000 10.000,1.0371,0.01865,0.01512,0.0010,0.0052,1.0000 10.250,1.0441,0.02081,0.01750,0.0027,0.0050,1.0000 10.500,1.0502,0.02283,0.01970,0.0042,0.0048,1.0000 10.750,1.0410,0.02589,0.02301,0.0072,0.0047,1.0000 11.000,1.0098,0.03017,0.02760,0.0108,0.0048,1.0000 11.250,0.9875,0.03402,0.03165,0.0116,0.0047,1.0000 11.500,0.9443,0.04164,0.03955,0.0102,0.0048,1.0000 11.750,0.9066,0.05035,0.04847,0.0068,0.0049,1.0000 12.000,0.8762,0.05962,0.05790,0.0021,0.0050,1.0000 12.250,0.8367,0.07163,0.07005,-0.0041,0.0052,1.0000