Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-hq158-il-200000-n5 Airfoil,hq158-il Reynolds number,200000 Ncrit,5 Mach,0 Max Cl/Cd,60.7391 Max Cl/Cd alpha,3.25 Url,http://airfoiltools.com/polar/csv?polar=xf-hq158-il-200000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -10.000,-0.4194,0.09821,0.09486,-0.0136,1.0000,0.0101 -9.750,-0.5087,0.10323,0.09962,-0.0109,1.0000,0.0104 -9.500,-0.5086,0.09881,0.09524,-0.0126,1.0000,0.0100 -9.250,-0.5078,0.09470,0.09117,-0.0144,1.0000,0.0098 -9.000,-0.5075,0.09050,0.08700,-0.0164,1.0000,0.0096 -8.750,-0.5084,0.08604,0.08258,-0.0186,1.0000,0.0094 -8.500,-0.5089,0.08189,0.07848,-0.0209,1.0000,0.0092 -8.250,-0.5120,0.07731,0.07395,-0.0237,1.0000,0.0090 -8.000,-0.5180,0.07241,0.06912,-0.0273,1.0000,0.0089 -7.750,-0.5226,0.06656,0.06328,-0.0333,1.0000,0.0087 -7.500,-0.5234,0.06104,0.05769,-0.0372,1.0000,0.0085 -7.250,-0.5225,0.05555,0.05208,-0.0398,1.0000,0.0083 -7.000,-0.5190,0.05026,0.04661,-0.0413,1.0000,0.0081 -6.750,-0.5137,0.04495,0.04106,-0.0418,1.0000,0.0080 -6.500,-0.5060,0.04000,0.03581,-0.0414,1.0000,0.0078 -6.250,-0.4965,0.03517,0.03060,-0.0403,1.0000,0.0077 -6.000,-0.4850,0.03079,0.02577,-0.0388,1.0000,0.0077 -5.750,-0.4713,0.02717,0.02169,-0.0371,1.0000,0.0080 -5.500,-0.4486,0.02401,0.01802,-0.0367,0.9978,0.0086 -5.250,-0.4156,0.02216,0.01575,-0.0381,0.9928,0.0103 -5.000,-0.3838,0.01969,0.01276,-0.0391,0.9878,0.0114 -4.750,-0.3524,0.01729,0.01003,-0.0400,0.9834,0.0122 -4.500,-0.3213,0.01585,0.00844,-0.0408,0.9779,0.0134 -4.250,-0.2880,0.01475,0.00721,-0.0420,0.9736,0.0154 -4.000,-0.2566,0.01413,0.00648,-0.0429,0.9670,0.0192 -3.750,-0.2246,0.01305,0.00530,-0.0439,0.9611,0.0242 -3.500,-0.1934,0.01238,0.00455,-0.0446,0.9540,0.0354 -3.250,-0.1613,0.01184,0.00404,-0.0457,0.9475,0.0638 -3.000,-0.1317,0.01122,0.00365,-0.0465,0.9395,0.1209 -2.750,-0.1017,0.01039,0.00327,-0.0475,0.9326,0.2449 -2.500,-0.0757,0.00956,0.00303,-0.0476,0.9236,0.4119 -2.250,-0.0488,0.00905,0.00296,-0.0474,0.9160,0.5507 -2.000,-0.0217,0.00884,0.00290,-0.0470,0.9077,0.6297 -1.750,0.0052,0.00871,0.00286,-0.0465,0.8992,0.6789 -1.500,0.0322,0.00861,0.00282,-0.0459,0.8914,0.7251 -1.250,0.0574,0.00854,0.00280,-0.0449,0.8814,0.7599 -1.000,0.0833,0.00847,0.00273,-0.0441,0.8706,0.7855 -0.750,0.1091,0.00841,0.00263,-0.0433,0.8593,0.8081 -0.500,0.1354,0.00835,0.00254,-0.0426,0.8480,0.8246 -0.250,0.1619,0.00830,0.00245,-0.0421,0.8364,0.8392 0.000,0.1884,0.00824,0.00238,-0.0415,0.8238,0.8550 0.250,0.2158,0.00819,0.00232,-0.0411,0.8116,0.8727 0.500,0.2450,0.00814,0.00228,-0.0412,0.7996,0.8933 1.000,0.3166,0.00808,0.00222,-0.0442,0.7739,0.9508 1.250,0.3549,0.00808,0.00221,-0.0465,0.7599,0.9992 1.500,0.3808,0.00816,0.00222,-0.0461,0.7446,1.0000 1.750,0.4066,0.00824,0.00224,-0.0456,0.7276,1.0000 2.000,0.4325,0.00834,0.00230,-0.0452,0.7097,1.0000 2.250,0.4584,0.00844,0.00240,-0.0447,0.6899,1.0000 2.500,0.4842,0.00857,0.00248,-0.0442,0.6675,1.0000 2.750,0.5098,0.00872,0.00257,-0.0436,0.6407,1.0000 3.000,0.5348,0.00892,0.00267,-0.0429,0.6045,1.0000 3.250,0.5588,0.00920,0.00278,-0.0421,0.5529,1.0000 3.500,0.5812,0.00965,0.00297,-0.0410,0.4829,1.0000 3.750,0.6031,0.01023,0.00323,-0.0400,0.4104,1.0000 4.000,0.6257,0.01081,0.00354,-0.0393,0.3403,1.0000 4.250,0.6479,0.01147,0.00392,-0.0385,0.3011,1.0000 4.750,0.6966,0.01238,0.00466,-0.0376,0.2180,1.0000 5.000,0.7201,0.01296,0.00514,-0.0371,0.1715,1.0000 5.250,0.7425,0.01371,0.00564,-0.0365,0.1170,1.0000 5.500,0.7654,0.01444,0.00624,-0.0359,0.0833,1.0000 5.750,0.7881,0.01519,0.00688,-0.0353,0.0587,1.0000 6.000,0.8113,0.01586,0.00750,-0.0347,0.0406,1.0000 6.250,0.8343,0.01655,0.00818,-0.0342,0.0268,1.0000 6.500,0.8564,0.01747,0.00911,-0.0333,0.0157,1.0000 6.750,0.8778,0.01853,0.01033,-0.0322,0.0117,1.0000 7.000,0.8988,0.01961,0.01165,-0.0311,0.0098,1.0000 7.250,0.9183,0.02092,0.01308,-0.0300,0.0083,1.0000 7.500,0.9382,0.02214,0.01445,-0.0290,0.0068,1.0000 7.750,0.9579,0.02346,0.01595,-0.0278,0.0060,1.0000 8.000,0.9764,0.02506,0.01776,-0.0266,0.0056,1.0000 8.250,0.9941,0.02685,0.01978,-0.0253,0.0053,1.0000 8.500,1.0108,0.02884,0.02203,-0.0239,0.0050,1.0000 8.750,1.0257,0.03108,0.02458,-0.0224,0.0049,1.0000 9.000,1.0381,0.03363,0.02747,-0.0208,0.0048,1.0000 9.250,1.0471,0.03649,0.03071,-0.0189,0.0047,1.0000 9.500,1.0513,0.03968,0.03429,-0.0168,0.0046,1.0000 9.750,1.0500,0.04314,0.03814,-0.0144,0.0046,1.0000 10.000,1.0419,0.04658,0.04192,-0.0116,0.0046,1.0000 10.250,1.0270,0.05023,0.04589,-0.0088,0.0047,1.0000 10.500,1.0103,0.05407,0.04997,-0.0074,0.0047,1.0000 10.750,0.9912,0.05883,0.05498,-0.0077,0.0048,1.0000 11.000,0.9702,0.06470,0.06106,-0.0100,0.0048,1.0000 11.250,0.9492,0.07183,0.06838,-0.0145,0.0049,1.0000 11.500,0.9273,0.08128,0.07799,-0.0218,0.0049,1.0000