Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hq1585-il-100000-n5 Airfoil,hq1585-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,48.3666 Max Cl/Cd alpha,4 Url,http://airfoiltools.com/polar/csv?polar=xf-hq1585-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.250,-0.5363,0.08787,0.08299,-0.0206,1.0000,0.0260 -9.000,-0.5468,0.07808,0.07333,-0.0286,1.0000,0.0243 -8.500,-0.5620,0.06643,0.06162,-0.0380,1.0000,0.0237 -8.250,-0.5692,0.06148,0.05658,-0.0406,1.0000,0.0235 -8.000,-0.5738,0.05656,0.05148,-0.0425,1.0000,0.0234 -7.750,-0.5749,0.05168,0.04633,-0.0436,1.0000,0.0234 -7.500,-0.5717,0.04713,0.04143,-0.0442,1.0000,0.0235 -7.250,-0.5646,0.04292,0.03679,-0.0441,1.0000,0.0237 -7.000,-0.5549,0.03889,0.03226,-0.0437,1.0000,0.0240 -6.750,-0.5439,0.03519,0.02827,-0.0432,1.0000,0.0253 -6.500,-0.5276,0.03356,0.02651,-0.0426,1.0000,0.0276 -6.250,-0.5108,0.03140,0.02403,-0.0416,1.0000,0.0296 -6.000,-0.4932,0.02883,0.02102,-0.0404,1.0000,0.0308 -5.750,-0.4744,0.02662,0.01840,-0.0390,1.0000,0.0321 -5.500,-0.4548,0.02516,0.01656,-0.0376,1.0000,0.0345 -5.250,-0.4364,0.02336,0.01458,-0.0364,1.0000,0.0374 -5.000,-0.4174,0.02197,0.01309,-0.0350,1.0000,0.0392 -4.750,-0.3982,0.02082,0.01183,-0.0336,1.0000,0.0411 -4.500,-0.3790,0.01982,0.01067,-0.0322,1.0000,0.0435 -4.250,-0.3483,0.01893,0.00961,-0.0330,0.9955,0.0479 -4.000,-0.3159,0.01790,0.00858,-0.0345,0.9896,0.0543 -3.750,-0.2821,0.01710,0.00763,-0.0360,0.9838,0.0609 -3.500,-0.2490,0.01627,0.00676,-0.0374,0.9778,0.0729 -3.250,-0.2167,0.01532,0.00606,-0.0389,0.9720,0.1167 -3.000,-0.1861,0.01403,0.00564,-0.0406,0.9663,0.3006 -2.750,-0.1576,0.01308,0.00558,-0.0412,0.9606,0.5029 -2.500,-0.1290,0.01282,0.00572,-0.0409,0.9543,0.6303 -2.250,-0.0999,0.01282,0.00583,-0.0404,0.9485,0.7111 -2.000,-0.0714,0.01283,0.00580,-0.0401,0.9413,0.7530 -1.750,-0.0381,0.01279,0.00568,-0.0409,0.9363,0.7771 -1.500,-0.0102,0.01276,0.00558,-0.0407,0.9285,0.7987 -1.250,0.0221,0.01270,0.00545,-0.0412,0.9233,0.8219 -1.000,0.0488,0.01264,0.00540,-0.0406,0.9153,0.8449 -0.750,0.0811,0.01258,0.00531,-0.0410,0.9098,0.8684 -0.250,0.1504,0.01244,0.00515,-0.0429,0.8957,0.9213 0.000,0.1906,0.01237,0.00506,-0.0453,0.8866,0.9439 0.500,0.2735,0.01219,0.00482,-0.0507,0.8683,0.9872 0.750,0.3039,0.01215,0.00473,-0.0512,0.8549,1.0000 1.000,0.3285,0.01215,0.00469,-0.0505,0.8409,1.0000 1.250,0.3537,0.01216,0.00465,-0.0497,0.8265,1.0000 1.500,0.3791,0.01218,0.00463,-0.0490,0.8119,1.0000 1.750,0.4046,0.01222,0.00467,-0.0483,0.7973,1.0000 2.000,0.4302,0.01229,0.00474,-0.0477,0.7833,1.0000 2.250,0.4559,0.01237,0.00482,-0.0470,0.7688,1.0000 2.500,0.4813,0.01246,0.00495,-0.0464,0.7528,1.0000 2.750,0.5067,0.01254,0.00510,-0.0458,0.7346,1.0000 3.000,0.5323,0.01260,0.00521,-0.0450,0.7152,1.0000 3.250,0.5576,0.01267,0.00532,-0.0442,0.6915,1.0000 3.500,0.5826,0.01272,0.00537,-0.0432,0.6608,1.0000 3.750,0.6071,0.01283,0.00546,-0.0421,0.6211,1.0000 4.000,0.6307,0.01304,0.00551,-0.0408,0.5658,1.0000 4.250,0.6520,0.01350,0.00560,-0.0392,0.4832,1.0000 4.500,0.6716,0.01428,0.00587,-0.0376,0.3943,1.0000 4.750,0.6922,0.01509,0.00631,-0.0366,0.3226,1.0000 5.000,0.7143,0.01581,0.00680,-0.0359,0.2698,1.0000 5.250,0.7372,0.01647,0.00739,-0.0352,0.2277,1.0000 5.500,0.7599,0.01719,0.00799,-0.0346,0.1832,1.0000 5.750,0.7814,0.01811,0.00868,-0.0339,0.1292,1.0000 6.000,0.8019,0.01924,0.00959,-0.0330,0.0950,1.0000 6.250,0.8235,0.02024,0.01057,-0.0322,0.0786,1.0000 6.500,0.8448,0.02123,0.01156,-0.0313,0.0692,1.0000 6.750,0.8662,0.02220,0.01272,-0.0304,0.0638,1.0000 7.000,0.8860,0.02342,0.01399,-0.0294,0.0597,1.0000 7.250,0.9072,0.02440,0.01511,-0.0286,0.0516,1.0000 7.500,0.9276,0.02546,0.01629,-0.0279,0.0421,1.0000 7.750,0.9451,0.02706,0.01794,-0.0268,0.0354,1.0000 8.000,0.9643,0.02878,0.01993,-0.0256,0.0302,1.0000 8.250,0.9818,0.03071,0.02195,-0.0244,0.0266,1.0000 8.500,0.9986,0.03321,0.02465,-0.0233,0.0236,1.0000 8.750,1.0169,0.03492,0.02670,-0.0221,0.0206,1.0000 9.000,1.0327,0.03708,0.02919,-0.0210,0.0190,1.0000 9.250,1.0462,0.03933,0.03167,-0.0197,0.0180,1.0000 9.500,1.0568,0.04188,0.03443,-0.0185,0.0173,1.0000 9.750,1.0625,0.04527,0.03810,-0.0169,0.0168,1.0000 10.000,1.0635,0.04874,0.04203,-0.0149,0.0165,1.0000 10.250,1.0584,0.05233,0.04602,-0.0128,0.0163,1.0000 10.500,1.0470,0.05574,0.04974,-0.0104,0.0162,1.0000 10.750,1.0321,0.05950,0.05379,-0.0090,0.0162,1.0000 11.000,1.0163,0.06362,0.05815,-0.0088,0.0162,1.0000 11.250,0.9980,0.06850,0.06325,-0.0100,0.0162,1.0000 11.500,0.9787,0.07419,0.06914,-0.0126,0.0163,1.0000 11.750,0.9595,0.08078,0.07589,-0.0167,0.0164,1.0000 12.000,0.9413,0.08825,0.08349,-0.0219,0.0165,1.0000 12.250,0.9228,0.09705,0.09238,-0.0282,0.0167,1.0000 12.500,0.9062,0.10634,0.10172,-0.0344,0.0169,1.0000