Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hq2195-il-50000 Airfoil,hq2195-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,37.2685 Max Cl/Cd alpha,6 Url,http://airfoiltools.com/polar/csv?polar=xf-hq2195-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -8.500,-0.4187,0.09996,0.09292,-0.0123,1.0000,0.3133 -8.250,-0.4201,0.09764,0.09068,-0.0117,1.0000,0.3302 -8.000,-0.4270,0.09587,0.08901,-0.0110,1.0000,0.3466 -7.750,-0.4019,0.09119,0.08429,-0.0095,1.0000,0.3656 -7.500,-0.4015,0.08924,0.08242,-0.0078,1.0000,0.3898 -7.250,-0.3832,0.08569,0.07888,-0.0060,1.0000,0.4162 -7.000,-0.3750,0.08291,0.07615,-0.0042,1.0000,0.4405 -6.750,-0.3876,0.08216,0.07554,-0.0012,1.0000,0.4654 -6.500,-0.3638,0.07775,0.07112,-0.0006,1.0000,0.4838 -5.750,-0.4898,0.05953,0.05324,-0.0295,1.0000,0.2564 -5.500,-0.4699,0.04714,0.03934,-0.0425,1.0000,0.1547 -5.250,-0.4531,0.04374,0.03570,-0.0421,1.0000,0.1494 -5.000,-0.4344,0.04020,0.03168,-0.0421,1.0000,0.1439 -4.750,-0.4113,0.03726,0.02792,-0.0422,1.0000,0.1374 -4.500,-0.3895,0.03454,0.02484,-0.0416,1.0000,0.1354 -4.250,-0.3663,0.03223,0.02213,-0.0410,1.0000,0.1347 -4.000,-0.3422,0.03047,0.01985,-0.0403,1.0000,0.1379 -3.750,-0.3195,0.02855,0.01787,-0.0395,1.0000,0.1437 -3.500,-0.2955,0.02706,0.01616,-0.0385,1.0000,0.1489 -3.250,-0.2719,0.02564,0.01461,-0.0373,1.0000,0.1575 -3.000,-0.2491,0.02443,0.01343,-0.0361,1.0000,0.1732 -2.750,-0.2265,0.02324,0.01228,-0.0347,1.0000,0.1950 -2.500,-0.2023,0.02162,0.01108,-0.0342,1.0000,0.2496 -2.250,-0.2047,0.01926,0.01153,-0.0253,1.0000,0.7353 -2.000,-0.2167,0.01923,0.01172,-0.0136,1.0000,0.8584 -1.750,-0.1379,0.01929,0.01121,-0.0197,1.0000,1.0000 -1.500,-0.1348,0.01894,0.01066,-0.0177,1.0000,1.0000 -1.250,-0.1188,0.01883,0.01026,-0.0175,1.0000,1.0000 -1.000,-0.0974,0.01887,0.01000,-0.0181,1.0000,1.0000 -0.750,-0.0742,0.01901,0.00986,-0.0187,1.0000,1.0000 -0.500,-0.0504,0.01922,0.00983,-0.0193,1.0000,1.0000 -0.250,-0.0267,0.01948,0.00987,-0.0199,1.0000,1.0000 0.000,-0.0033,0.01979,0.00997,-0.0203,1.0000,1.0000 0.250,0.0197,0.02014,0.01016,-0.0206,1.0000,1.0000 0.500,0.0423,0.02053,0.01041,-0.0209,1.0000,1.0000 0.750,0.0645,0.02097,0.01072,-0.0211,1.0000,1.0000 1.000,0.0863,0.02145,0.01110,-0.0213,1.0000,1.0000 1.250,0.1075,0.02198,0.01156,-0.0215,1.0000,1.0000 1.500,0.1282,0.02258,0.01209,-0.0217,1.0000,1.0000 1.750,0.1482,0.02323,0.01271,-0.0219,1.0000,1.0000 2.000,0.1675,0.02397,0.01342,-0.0221,1.0000,1.0000 2.250,0.2067,0.02520,0.01468,-0.0263,0.9893,1.0000 2.500,0.2678,0.02678,0.01631,-0.0341,0.9659,1.0000 2.750,0.3288,0.02812,0.01775,-0.0413,0.9416,1.0000 3.000,0.3807,0.02908,0.01885,-0.0466,0.9149,1.0000 3.250,0.4322,0.02987,0.01979,-0.0513,0.8876,1.0000 3.500,0.4845,0.03042,0.02054,-0.0555,0.8597,1.0000 3.750,0.5383,0.03067,0.02103,-0.0593,0.8320,1.0000 4.000,0.5999,0.03038,0.02103,-0.0635,0.8055,1.0000 4.250,0.6513,0.02984,0.02078,-0.0653,0.7777,1.0000 4.500,0.6965,0.02907,0.02026,-0.0656,0.7488,1.0000 4.750,0.7412,0.02783,0.01926,-0.0649,0.7186,1.0000 5.000,0.7773,0.02663,0.01826,-0.0628,0.6837,1.0000 5.250,0.8130,0.02515,0.01689,-0.0601,0.6451,1.0000 5.500,0.8424,0.02407,0.01582,-0.0571,0.6007,1.0000 5.750,0.8670,0.02361,0.01528,-0.0540,0.5487,1.0000 6.000,0.8896,0.02387,0.01523,-0.0510,0.4884,1.0000 6.250,0.9073,0.02496,0.01588,-0.0480,0.4174,1.0000 6.500,0.9218,0.02662,0.01705,-0.0450,0.3410,1.0000 6.750,0.9370,0.02836,0.01839,-0.0424,0.2792,1.0000 7.000,0.9551,0.03006,0.01981,-0.0406,0.2348,1.0000 7.250,0.9759,0.03192,0.02137,-0.0393,0.2013,1.0000 7.500,0.9980,0.03402,0.02338,-0.0382,0.1755,1.0000 7.750,1.0211,0.03656,0.02601,-0.0373,0.1571,1.0000 8.000,1.0449,0.03941,0.02899,-0.0366,0.1445,1.0000 8.250,1.0654,0.04208,0.03188,-0.0356,0.1339,1.0000 8.500,1.0815,0.04573,0.03604,-0.0341,0.1290,1.0000 8.750,1.0929,0.04952,0.04040,-0.0323,0.1257,1.0000 9.000,1.1068,0.05293,0.04405,-0.0311,0.1211,1.0000 9.250,1.1174,0.05705,0.04839,-0.0299,0.1175,1.0000 9.500,1.1154,0.06146,0.05334,-0.0278,0.1169,1.0000 9.750,1.1114,0.06628,0.05859,-0.0260,0.1172,1.0000 10.000,1.1059,0.07134,0.06396,-0.0246,0.1178,1.0000 10.250,1.0720,0.07628,0.06937,-0.0224,0.1204,1.0000 10.500,1.0094,0.08279,0.07615,-0.0218,0.1250,1.0000 10.750,0.9758,0.09022,0.08364,-0.0246,0.1286,1.0000 11.000,0.9592,0.09734,0.09078,-0.0275,0.1308,1.0000