Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-goe804-il-50000-n5 Airfoil,goe804-il Reynolds number,50000 Ncrit,5 Mach,0 Max Cl/Cd,41.1062 Max Cl/Cd alpha,7 Url,http://airfoiltools.com/polar/csv?polar=xf-goe804-il-50000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.3846,0.12844,0.12214,-0.0225,1.0000,0.0614 -7.500,-0.3931,0.12763,0.12141,-0.0214,1.0000,0.0615 -7.250,-0.4016,0.12674,0.12060,-0.0203,1.0000,0.0617 -7.000,-0.4070,0.12547,0.11942,-0.0206,1.0000,0.0618 -6.750,-0.3982,0.11944,0.11340,-0.0178,1.0000,0.0627 -6.500,-0.3939,0.11558,0.10957,-0.0161,1.0000,0.0639 -6.250,-0.3937,0.11291,0.10694,-0.0150,1.0000,0.0651 -6.000,-0.3940,0.11052,0.10460,-0.0144,1.0000,0.0663 -5.750,-0.3938,0.10816,0.10229,-0.0142,1.0000,0.0680 -5.500,-0.3926,0.10578,0.09997,-0.0147,1.0000,0.0696 -5.250,-0.3891,0.10360,0.09783,-0.0171,1.0000,0.0722 -5.000,-0.3659,0.10144,0.09566,-0.0285,0.9975,0.0742 -4.750,-0.3481,0.09656,0.09080,-0.0316,0.9939,0.0755 -4.500,-0.3388,0.09245,0.08667,-0.0294,0.9908,0.0788 -4.250,-0.3147,0.08867,0.08285,-0.0345,0.9867,0.0828 -4.000,-0.2591,0.08469,0.07867,-0.0530,0.9811,0.0888 -3.750,-0.2298,0.07983,0.07377,-0.0587,0.9779,0.0899 -3.500,-0.2158,0.07593,0.06988,-0.0583,0.9739,0.0920 -3.250,-0.1844,0.07214,0.06598,-0.0635,0.9703,0.0979 -3.000,-0.0950,0.06372,0.05700,-0.0852,0.9689,0.0613 -2.750,-0.0645,0.05972,0.05293,-0.0889,0.9661,0.0570 -2.500,-0.0010,0.05418,0.04702,-0.1010,0.9645,0.0538 -2.250,0.0614,0.04965,0.04203,-0.1118,0.9630,0.0565 -2.000,0.1311,0.04493,0.03661,-0.1232,0.9626,0.0584 -1.750,0.1944,0.04125,0.03216,-0.1323,0.9620,0.0642 -1.500,0.2487,0.03889,0.02894,-0.1385,0.9607,0.0743 -1.250,0.2914,0.03749,0.02712,-0.1424,0.9586,0.0870 -1.000,0.3348,0.03641,0.02546,-0.1459,0.9566,0.1031 -0.750,0.3709,0.03555,0.02430,-0.1481,0.9536,0.1146 -0.500,0.4015,0.03518,0.02364,-0.1490,0.9492,0.1305 -0.250,0.4335,0.03483,0.02308,-0.1500,0.9456,0.1393 0.000,0.4681,0.03474,0.02281,-0.1516,0.9425,0.1549 0.250,0.4957,0.03473,0.02271,-0.1521,0.9373,0.1711 0.500,0.5276,0.03474,0.02264,-0.1533,0.9326,0.1909 0.750,0.5655,0.03466,0.02270,-0.1560,0.9293,0.2394 1.000,0.5847,0.03313,0.02295,-0.1546,0.9240,1.0000 1.250,0.6130,0.03368,0.02315,-0.1550,0.9177,1.0000 1.500,0.6478,0.03425,0.02345,-0.1568,0.9134,1.0000 1.750,0.6715,0.03479,0.02386,-0.1566,0.9052,1.0000 2.250,0.7358,0.03554,0.02442,-0.1588,0.8883,1.0000 2.500,0.7691,0.03583,0.02465,-0.1599,0.8797,1.0000 2.750,0.8011,0.03613,0.02496,-0.1609,0.8712,1.0000 3.000,0.8261,0.03662,0.02549,-0.1608,0.8622,1.0000 3.250,0.8598,0.03695,0.02588,-0.1621,0.8558,1.0000 3.500,0.8823,0.03749,0.02653,-0.1616,0.8457,1.0000 3.750,0.9174,0.03771,0.02686,-0.1630,0.8394,1.0000 4.000,0.9419,0.03807,0.02740,-0.1626,0.8281,1.0000 4.250,0.9675,0.03833,0.02782,-0.1623,0.8161,1.0000 4.500,0.9958,0.03839,0.02807,-0.1622,0.8038,1.0000 4.750,1.0259,0.03825,0.02818,-0.1621,0.7908,1.0000 5.000,1.0563,0.03798,0.02817,-0.1619,0.7768,1.0000 5.250,1.0859,0.03766,0.02812,-0.1615,0.7620,1.0000 5.500,1.1149,0.03734,0.02815,-0.1609,0.7471,1.0000 5.750,1.1440,0.03704,0.02821,-0.1603,0.7329,1.0000 6.000,1.1708,0.03662,0.02816,-0.1590,0.7149,1.0000 6.250,1.2022,0.03561,0.02760,-0.1578,0.6943,1.0000 6.500,1.2348,0.03403,0.02642,-0.1558,0.6612,1.0000 6.750,1.2644,0.03263,0.02527,-0.1530,0.6022,1.0000 7.000,1.2969,0.03155,0.02324,-0.1493,0.4225,1.0000 7.250,1.2876,0.03456,0.02499,-0.1438,0.2643,1.0000 7.500,1.2830,0.03789,0.02745,-0.1399,0.1426,1.0000 7.750,1.2834,0.04144,0.03031,-0.1367,0.0809,1.0000 8.000,1.2900,0.04437,0.03301,-0.1342,0.0607,1.0000 8.250,1.3006,0.04686,0.03567,-0.1319,0.0503,1.0000 8.500,1.3159,0.04920,0.03833,-0.1299,0.0438,1.0000 8.750,1.3336,0.05159,0.04081,-0.1283,0.0385,1.0000 9.000,1.3665,0.05393,0.04352,-0.1278,0.0343,1.0000 9.250,1.3968,0.05688,0.04658,-0.1279,0.0309,1.0000 9.500,1.4351,0.06090,0.05125,-0.1284,0.0287,1.0000 9.750,1.4579,0.06540,0.05637,-0.1274,0.0279,1.0000 10.000,1.4643,0.06966,0.06118,-0.1248,0.0272,1.0000 10.250,1.4624,0.07381,0.06581,-0.1217,0.0268,1.0000 10.500,1.4549,0.07801,0.07045,-0.1184,0.0263,1.0000 10.750,1.4435,0.08233,0.07519,-0.1153,0.0260,1.0000 11.000,1.4292,0.08686,0.08009,-0.1127,0.0258,1.0000 11.250,1.4125,0.09170,0.08528,-0.1106,0.0257,1.0000 11.500,1.3944,0.09686,0.09076,-0.1093,0.0258,1.0000 11.750,1.3750,0.10242,0.09662,-0.1089,0.0259,1.0000 12.000,1.3546,0.10847,0.10294,-0.1096,0.0260,1.0000 12.250,1.3344,0.11493,0.10963,-0.1114,0.0263,1.0000