Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hq1010-il-500000 Airfoil,hq1010-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,79.1372 Max Cl/Cd alpha,3.75 Url,http://airfoiltools.com/polar/csv?polar=xf-hq1010-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.7559,0.03821,0.03489,-0.0406,1.0000,0.0102 -9.000,-0.7629,0.03346,0.02972,-0.0386,1.0000,0.0101 -8.750,-0.7609,0.02951,0.02535,-0.0366,1.0000,0.0101 -8.500,-0.7508,0.02674,0.02222,-0.0349,1.0000,0.0102 -8.250,-0.7359,0.02484,0.02003,-0.0333,1.0000,0.0104 -8.000,-0.7223,0.02245,0.01732,-0.0315,1.0000,0.0106 -7.750,-0.7107,0.01943,0.01396,-0.0294,1.0000,0.0111 -7.500,-0.6944,0.01789,0.01227,-0.0276,1.0000,0.0115 -7.250,-0.6766,0.01704,0.01136,-0.0261,1.0000,0.0122 -7.000,-0.6599,0.01632,0.01058,-0.0243,1.0000,0.0128 -6.750,-0.6430,0.01580,0.00998,-0.0225,0.9998,0.0139 -6.500,-0.6076,0.01482,0.00888,-0.0244,0.9962,0.0149 -6.250,-0.5747,0.01334,0.00725,-0.0260,0.9918,0.0168 -6.000,-0.5399,0.01261,0.00649,-0.0278,0.9871,0.0195 -5.750,-0.5035,0.01189,0.00570,-0.0298,0.9835,0.0238 -5.500,-0.4685,0.01141,0.00522,-0.0316,0.9787,0.0326 -5.250,-0.4334,0.01097,0.00478,-0.0333,0.9733,0.0426 -5.000,-0.3974,0.01049,0.00430,-0.0353,0.9689,0.0538 -4.750,-0.3667,0.01007,0.00391,-0.0360,0.9595,0.0649 -4.500,-0.3352,0.00969,0.00355,-0.0369,0.9511,0.0801 -4.250,-0.3066,0.00919,0.00318,-0.0372,0.9414,0.1134 -4.000,-0.2816,0.00860,0.00287,-0.0369,0.9297,0.1830 -3.750,-0.2567,0.00813,0.00262,-0.0365,0.9187,0.2520 -3.500,-0.2328,0.00756,0.00236,-0.0360,0.9083,0.3434 -3.250,-0.2094,0.00702,0.00217,-0.0353,0.8986,0.4547 -3.000,-0.1847,0.00674,0.00209,-0.0346,0.8881,0.5237 -2.750,-0.1588,0.00661,0.00203,-0.0341,0.8787,0.5683 -2.500,-0.1325,0.00655,0.00198,-0.0336,0.8699,0.6020 -2.250,-0.1062,0.00648,0.00195,-0.0331,0.8602,0.6321 -2.000,-0.0794,0.00646,0.00192,-0.0327,0.8513,0.6545 -1.750,-0.0524,0.00646,0.00189,-0.0324,0.8429,0.6730 -1.500,-0.0257,0.00643,0.00190,-0.0320,0.8340,0.6936 -1.250,0.0012,0.00644,0.00188,-0.0315,0.8253,0.7111 -1.000,0.0281,0.00644,0.00185,-0.0311,0.8150,0.7242 -0.750,0.0552,0.00642,0.00183,-0.0308,0.8042,0.7351 -0.500,0.0824,0.00642,0.00181,-0.0305,0.7943,0.7468 -0.250,0.1095,0.00643,0.00178,-0.0302,0.7848,0.7589 0.000,0.1366,0.00643,0.00178,-0.0299,0.7741,0.7705 0.250,0.1636,0.00641,0.00178,-0.0295,0.7632,0.7820 0.500,0.1905,0.00641,0.00179,-0.0291,0.7527,0.7935 0.750,0.2176,0.00642,0.00178,-0.0288,0.7433,0.8039 1.000,0.2450,0.00642,0.00179,-0.0287,0.7326,0.8140 1.250,0.2721,0.00641,0.00182,-0.0283,0.7220,0.8234 1.500,0.2991,0.00641,0.00183,-0.0280,0.7111,0.8334 1.750,0.3260,0.00642,0.00184,-0.0277,0.6991,0.8443 2.250,0.3788,0.00643,0.00190,-0.0268,0.6701,0.8684 2.500,0.4047,0.00643,0.00193,-0.0262,0.6527,0.8826 2.750,0.4302,0.00644,0.00197,-0.0256,0.6336,0.8993 3.000,0.4561,0.00647,0.00202,-0.0249,0.6106,0.9192 3.250,0.4855,0.00657,0.00209,-0.0251,0.5774,0.9442 3.500,0.5211,0.00677,0.00217,-0.0268,0.5337,0.9680 3.750,0.5595,0.00707,0.00230,-0.0293,0.4802,0.9875 4.000,0.5908,0.00754,0.00249,-0.0305,0.4127,1.0000 4.250,0.6121,0.00802,0.00271,-0.0295,0.3510,1.0000 4.500,0.6345,0.00851,0.00297,-0.0288,0.2997,1.0000 4.750,0.6583,0.00890,0.00322,-0.0282,0.2686,1.0000 5.000,0.6828,0.00925,0.00348,-0.0277,0.2432,1.0000 5.250,0.7070,0.00963,0.00376,-0.0272,0.2125,1.0000 5.500,0.7311,0.01005,0.00404,-0.0268,0.1800,1.0000 5.750,0.7549,0.01051,0.00436,-0.0262,0.1439,1.0000 6.000,0.7779,0.01107,0.00474,-0.0256,0.1117,1.0000 6.250,0.8012,0.01159,0.00516,-0.0250,0.0885,1.0000 6.500,0.8247,0.01209,0.00561,-0.0244,0.0705,1.0000 6.750,0.8483,0.01259,0.00604,-0.0239,0.0557,1.0000 7.000,0.8717,0.01309,0.00651,-0.0233,0.0443,1.0000 7.250,0.8948,0.01364,0.00704,-0.0226,0.0349,1.0000 7.500,0.9168,0.01433,0.00771,-0.0218,0.0264,1.0000 7.750,0.9370,0.01525,0.00864,-0.0207,0.0190,1.0000 8.000,0.9599,0.01579,0.00923,-0.0200,0.0153,1.0000 8.250,0.9779,0.01692,0.01044,-0.0186,0.0125,1.0000 8.500,0.9987,0.01767,0.01128,-0.0176,0.0113,1.0000 8.750,1.0186,0.01849,0.01218,-0.0165,0.0104,1.0000 9.000,1.0369,0.01947,0.01322,-0.0153,0.0097,1.0000 9.250,1.0504,0.02099,0.01486,-0.0134,0.0091,1.0000 9.500,1.0607,0.02305,0.01711,-0.0112,0.0086,1.0000 9.750,1.0776,0.02414,0.01835,-0.0098,0.0084,1.0000 10.000,1.0920,0.02555,0.01994,-0.0082,0.0081,1.0000 10.250,1.1045,0.02714,0.02171,-0.0064,0.0078,1.0000 10.500,1.1140,0.02903,0.02381,-0.0043,0.0076,1.0000 10.750,1.1193,0.03101,0.02600,-0.0018,0.0076,1.0000 11.000,1.1202,0.03312,0.02833,0.0012,0.0075,1.0000 11.250,1.1165,0.03560,0.03105,0.0042,0.0074,1.0000 11.500,1.1103,0.03828,0.03397,0.0067,0.0075,1.0000 11.750,1.1012,0.04129,0.03721,0.0087,0.0076,1.0000 12.000,1.0871,0.04499,0.04116,0.0101,0.0076,1.0000 12.250,1.0726,0.04898,0.04538,0.0105,0.0077,1.0000 12.500,1.0562,0.05355,0.05016,0.0098,0.0078,1.0000 12.750,1.0375,0.05892,0.05574,0.0080,0.0078,1.0000 13.000,1.0162,0.06537,0.06239,0.0049,0.0079,1.0000 13.250,0.9970,0.07229,0.06947,0.0006,0.0079,1.0000 13.500,0.9761,0.08048,0.07783,-0.0048,0.0080,1.0000 13.750,0.9549,0.08982,0.08731,-0.0113,0.0080,1.0000 14.000,0.9330,0.10024,0.09787,-0.0182,0.0081,1.0000 14.250,0.9042,0.11322,0.11096,-0.0262,0.0082,1.0000 14.500,0.8658,0.12941,0.12720,-0.0351,0.0085,1.0000