Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-ag46c03-il-200000 Airfoil,ag46c03-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,58.0678 Max Cl/Cd alpha,5.25 Url,http://airfoiltools.com/polar/csv?polar=xf-ag46c03-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.000,-0.4770,0.08412,0.08101,0.0108,1.0000,0.0355 -6.750,-0.4755,0.08025,0.07716,0.0098,1.0000,0.0363 -6.500,-0.4750,0.07626,0.07320,0.0084,1.0000,0.0372 -6.250,-0.4755,0.07216,0.06914,0.0066,1.0000,0.0381 -6.000,-0.4760,0.06781,0.06482,0.0037,1.0000,0.0390 -5.750,-0.4723,0.06267,0.05968,-0.0011,1.0000,0.0401 -5.500,-0.4650,0.05690,0.05388,-0.0074,1.0000,0.0418 -5.250,-0.4476,0.05014,0.04684,-0.0185,1.0000,0.0441 -5.000,-0.4322,0.04508,0.04148,-0.0220,1.0000,0.0445 -4.750,-0.4280,0.03785,0.03442,-0.0223,1.0000,0.0463 -4.500,-0.4130,0.03450,0.03108,-0.0224,1.0000,0.0483 -4.250,-0.3944,0.03059,0.02703,-0.0240,1.0000,0.0516 -4.000,-0.3705,0.02489,0.02071,-0.0275,1.0000,0.0585 -3.750,-0.3527,0.02191,0.01781,-0.0274,1.0000,0.0612 -3.500,-0.3293,0.01871,0.01420,-0.0285,1.0000,0.0725 -3.250,-0.3065,0.01649,0.01174,-0.0288,1.0000,0.0856 -3.000,-0.2850,0.02384,0.01777,-0.0285,1.0000,0.0421 -2.750,-0.2542,0.02030,0.01345,-0.0275,1.0000,0.0329 -2.500,-0.2266,0.01792,0.01078,-0.0271,1.0000,0.0318 -2.250,-0.1988,0.01606,0.00865,-0.0266,1.0000,0.0320 -2.000,-0.1716,0.01405,0.00649,-0.0261,1.0000,0.0336 -1.750,-0.1449,0.01302,0.00548,-0.0258,1.0000,0.0408 -1.500,-0.1180,0.01182,0.00428,-0.0253,1.0000,0.0490 -1.250,-0.0907,0.01091,0.00347,-0.0251,1.0000,0.0748 -1.000,-0.0642,0.00956,0.00287,-0.0252,1.0000,0.2261 -0.750,-0.0425,0.00787,0.00273,-0.0247,1.0000,0.6053 -0.500,-0.0127,0.00687,0.00261,-0.0234,1.0000,1.0000 -0.250,0.0137,0.00688,0.00247,-0.0232,1.0000,1.0000 0.000,0.0397,0.00691,0.00240,-0.0231,1.0000,1.0000 0.250,0.0867,0.00696,0.00230,-0.0273,0.9685,1.0000 0.500,0.1304,0.00701,0.00218,-0.0304,0.9229,1.0000 0.750,0.1628,0.00710,0.00207,-0.0308,0.8756,1.0000 1.000,0.1883,0.00725,0.00201,-0.0297,0.8374,1.0000 1.250,0.2132,0.00744,0.00199,-0.0287,0.8071,1.0000 1.500,0.2386,0.00764,0.00201,-0.0278,0.7816,1.0000 1.750,0.2641,0.00787,0.00205,-0.0270,0.7592,1.0000 2.000,0.2903,0.00809,0.00213,-0.0264,0.7374,1.0000 2.250,0.3162,0.00835,0.00224,-0.0257,0.7178,1.0000 2.500,0.3427,0.00857,0.00237,-0.0252,0.6972,1.0000 2.750,0.3695,0.00871,0.00246,-0.0248,0.6753,1.0000 3.000,0.3962,0.00880,0.00250,-0.0243,0.6532,1.0000 3.250,0.4230,0.00887,0.00253,-0.0239,0.6281,1.0000 3.500,0.4497,0.00897,0.00258,-0.0234,0.6008,1.0000 3.750,0.4762,0.00911,0.00262,-0.0230,0.5709,1.0000 4.000,0.5028,0.00929,0.00270,-0.0225,0.5377,1.0000 4.250,0.5292,0.00952,0.00282,-0.0221,0.5020,1.0000 4.500,0.5556,0.00980,0.00300,-0.0217,0.4633,1.0000 4.750,0.5818,0.01012,0.00319,-0.0214,0.4226,1.0000 5.000,0.6080,0.01049,0.00342,-0.0211,0.3799,1.0000 5.250,0.6341,0.01092,0.00370,-0.0209,0.3362,1.0000 5.500,0.6600,0.01142,0.00405,-0.0207,0.2924,1.0000 5.750,0.6858,0.01197,0.00444,-0.0205,0.2510,1.0000 6.000,0.7117,0.01255,0.00490,-0.0203,0.2148,1.0000 6.250,0.7373,0.01318,0.00541,-0.0201,0.1844,1.0000 6.500,0.7630,0.01383,0.00600,-0.0199,0.1597,1.0000 6.750,0.7882,0.01455,0.00666,-0.0197,0.1383,1.0000 7.000,0.8137,0.01523,0.00736,-0.0195,0.1196,1.0000 7.250,0.8388,0.01599,0.00810,-0.0192,0.1030,1.0000 7.500,0.8632,0.01692,0.00900,-0.0189,0.0881,1.0000 7.750,0.8875,0.01790,0.01000,-0.0185,0.0751,1.0000 8.000,0.9122,0.01874,0.01096,-0.0182,0.0638,1.0000 8.250,0.9362,0.01988,0.01222,-0.0177,0.0547,1.0000 8.500,0.9590,0.02132,0.01375,-0.0171,0.0471,1.0000 8.750,0.9823,0.02260,0.01513,-0.0166,0.0413,1.0000 9.000,1.0036,0.02473,0.01747,-0.0159,0.0366,1.0000 9.250,1.0262,0.02619,0.01915,-0.0153,0.0326,1.0000 9.500,1.0465,0.02834,0.02148,-0.0147,0.0299,1.0000 9.750,1.0602,0.03313,0.02676,-0.0137,0.0282,1.0000 10.000,1.0789,0.03498,0.02906,-0.0129,0.0263,1.0000 10.250,1.0929,0.03800,0.03252,-0.0122,0.0245,1.0000 10.500,1.1005,0.04223,0.03725,-0.0115,0.0238,1.0000 10.750,1.1005,0.04724,0.04277,-0.0110,0.0235,1.0000 11.000,1.0909,0.05299,0.04900,-0.0112,0.0237,1.0000 11.250,1.0723,0.05877,0.05513,-0.0122,0.0240,1.0000 11.500,1.0493,0.06503,0.06163,-0.0164,0.0243,1.0000 11.750,1.0250,0.07359,0.07038,-0.0244,0.0249,1.0000 12.000,0.9979,0.08505,0.08196,-0.0346,0.0257,1.0000 12.250,0.9683,0.09837,0.09527,-0.0440,0.0269,1.0000 12.500,0.9354,0.11465,0.11150,-0.0520,0.0304,1.0000 12.750,0.9322,0.11940,0.11624,-0.0540,0.0296,1.0000