Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hq308-il-100000-n5 Airfoil,hq308-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,60.9304 Max Cl/Cd alpha,4.75 Url,http://airfoiltools.com/polar/csv?polar=xf-hq308-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.2895,0.10007,0.09542,-0.0321,1.0000,0.0380 -9.250,-0.2887,0.09686,0.09224,-0.0327,1.0000,0.0392 -8.750,-0.3731,0.10125,0.09633,-0.0311,1.0000,0.0339 -8.500,-0.3692,0.09845,0.09357,-0.0312,1.0000,0.0365 -8.250,-0.3683,0.09563,0.09082,-0.0320,1.0000,0.0391 -8.000,-0.3680,0.09280,0.08805,-0.0324,1.0000,0.0391 -7.750,-0.3692,0.09008,0.08536,-0.0326,1.0000,0.0388 -7.250,-0.3864,0.08578,0.08135,-0.0333,1.0000,0.0421 -7.000,-0.3893,0.08298,0.07856,-0.0331,1.0000,0.0417 -6.750,-0.3954,0.07999,0.07570,-0.0390,1.0000,0.0430 -6.500,-0.3966,0.07692,0.07261,-0.0412,1.0000,0.0432 -6.250,-0.3961,0.07398,0.06956,-0.0437,1.0000,0.0436 -6.000,-0.3923,0.07082,0.06631,-0.0445,1.0000,0.0436 -5.750,-0.3757,0.06409,0.05957,-0.0478,0.9961,0.0446 -5.500,-0.3499,0.05887,0.05421,-0.0526,0.9910,0.0450 -5.250,-0.3237,0.05297,0.04821,-0.0551,0.9869,0.0268 -5.000,-0.2922,0.04709,0.04202,-0.0607,0.9815,0.0236 -4.750,-0.2513,0.04003,0.03426,-0.0662,0.9767,0.0201 -4.250,-0.1845,0.03313,0.02643,-0.0711,0.9676,0.0189 -4.000,-0.1498,0.02956,0.02233,-0.0735,0.9637,0.0188 -3.750,-0.1131,0.02660,0.01881,-0.0756,0.9609,0.0189 -3.500,-0.0829,0.02398,0.01574,-0.0763,0.9557,0.0197 -3.250,-0.0502,0.02248,0.01405,-0.0779,0.9514,0.0240 -3.000,-0.0142,0.02079,0.01200,-0.0792,0.9484,0.0260 -2.750,0.0164,0.01935,0.01036,-0.0794,0.9435,0.0280 -2.500,0.0484,0.01826,0.00911,-0.0800,0.9387,0.0305 -2.250,0.0839,0.01721,0.00797,-0.0816,0.9352,0.0382 -2.000,0.1142,0.01646,0.00730,-0.0823,0.9294,0.0759 -1.750,0.1438,0.01441,0.00692,-0.0839,0.9250,0.4865 -1.500,0.1717,0.01397,0.00694,-0.0829,0.9210,0.7042 -1.250,0.1907,0.01377,0.00690,-0.0802,0.9130,0.7982 -1.000,0.2198,0.01330,0.00661,-0.0789,0.9088,0.9132 -0.750,0.2617,0.01320,0.00631,-0.0820,0.9031,1.0000 -0.500,0.2956,0.01322,0.00609,-0.0834,0.8966,1.0000 -0.250,0.3280,0.01325,0.00594,-0.0845,0.8895,1.0000 0.000,0.3611,0.01325,0.00580,-0.0855,0.8822,1.0000 0.250,0.3912,0.01328,0.00572,-0.0860,0.8733,1.0000 0.500,0.4256,0.01323,0.00556,-0.0871,0.8667,1.0000 0.750,0.4532,0.01329,0.00555,-0.0871,0.8566,1.0000 1.000,0.4827,0.01332,0.00552,-0.0873,0.8474,1.0000 1.250,0.5139,0.01327,0.00542,-0.0876,0.8380,1.0000 1.500,0.5431,0.01323,0.00535,-0.0876,0.8263,1.0000 1.750,0.5709,0.01323,0.00532,-0.0872,0.8135,1.0000 2.000,0.5984,0.01325,0.00534,-0.0869,0.8008,1.0000 2.250,0.6259,0.01327,0.00536,-0.0866,0.7876,1.0000 2.500,0.6536,0.01328,0.00537,-0.0862,0.7733,1.0000 2.750,0.6805,0.01328,0.00544,-0.0857,0.7559,1.0000 3.000,0.7069,0.01331,0.00548,-0.0850,0.7359,1.0000 3.250,0.7338,0.01334,0.00552,-0.0844,0.7157,1.0000 3.500,0.7599,0.01343,0.00563,-0.0838,0.6938,1.0000 3.750,0.7859,0.01354,0.00582,-0.0831,0.6694,1.0000 4.000,0.8116,0.01368,0.00597,-0.0823,0.6413,1.0000 4.250,0.8367,0.01387,0.00614,-0.0814,0.6077,1.0000 4.500,0.8609,0.01414,0.00635,-0.0804,0.5675,1.0000 4.750,0.8841,0.01451,0.00661,-0.0793,0.5208,1.0000 5.000,0.9061,0.01501,0.00695,-0.0781,0.4703,1.0000 5.250,0.9271,0.01564,0.00749,-0.0768,0.4204,1.0000 5.500,0.9478,0.01634,0.00804,-0.0756,0.3733,1.0000 5.750,0.9678,0.01711,0.00866,-0.0743,0.3265,1.0000 6.000,0.9871,0.01795,0.00934,-0.0731,0.2810,1.0000 6.250,1.0067,0.01880,0.01006,-0.0720,0.2388,1.0000 6.500,1.0256,0.01973,0.01082,-0.0708,0.1923,1.0000 6.750,1.0438,0.02078,0.01163,-0.0697,0.1453,1.0000 7.000,1.0623,0.02187,0.01254,-0.0686,0.1007,1.0000 7.250,1.0784,0.02331,0.01374,-0.0673,0.0569,1.0000 7.750,1.1087,0.02664,0.01708,-0.0638,0.0213,1.0000 8.000,1.1232,0.02829,0.01895,-0.0619,0.0168,1.0000 8.250,1.1343,0.03026,0.02105,-0.0598,0.0136,1.0000 8.500,1.1486,0.03175,0.02281,-0.0580,0.0115,1.0000 8.750,1.1604,0.03354,0.02483,-0.0560,0.0103,1.0000 9.000,1.1707,0.03556,0.02709,-0.0538,0.0097,1.0000 9.250,1.1804,0.03773,0.02950,-0.0517,0.0094,1.0000 9.500,1.1883,0.04001,0.03203,-0.0494,0.0090,1.0000 9.750,1.1947,0.04253,0.03481,-0.0472,0.0088,1.0000 10.000,1.1986,0.04525,0.03782,-0.0449,0.0086,1.0000 10.250,1.1997,0.04817,0.04103,-0.0425,0.0085,1.0000 10.500,1.1974,0.05134,0.04451,-0.0403,0.0084,1.0000 10.750,1.1919,0.05472,0.04819,-0.0384,0.0083,1.0000 11.000,1.1833,0.05842,0.05219,-0.0369,0.0083,1.0000 11.250,1.1723,0.06249,0.05656,-0.0360,0.0083,1.0000 11.500,1.1589,0.06704,0.06139,-0.0359,0.0083,1.0000 11.750,1.1436,0.07216,0.06678,-0.0368,0.0083,1.0000 12.000,1.1271,0.07790,0.07278,-0.0387,0.0084,1.0000 12.250,1.1089,0.08456,0.07968,-0.0419,0.0084,1.0000 12.500,1.0894,0.09231,0.08765,-0.0465,0.0085,1.0000 12.750,1.0685,0.10145,0.09699,-0.0525,0.0087,1.0000 13.000,1.0464,0.11235,0.10805,-0.0598,0.0089,1.0000