Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh44-il-200000 Airfoil,mh44-il Reynolds number,200000 Ncrit,9 Mach,0 Max Cl/Cd,60.5929 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-mh44-il-200000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -11.250,-0.5459,0.12849,0.12496,0.0106,1.0000,0.0365 -11.000,-0.5483,0.12406,0.12058,0.0061,1.0000,0.0377 -5.750,-0.5319,0.02901,0.02277,-0.0178,1.0000,0.0283 -5.500,-0.5235,0.02566,0.01926,-0.0149,1.0000,0.0263 -5.250,-0.5123,0.02340,0.01670,-0.0120,1.0000,0.0251 -5.000,-0.4877,0.02115,0.01409,-0.0113,0.9978,0.0240 -4.750,-0.4498,0.01910,0.01177,-0.0129,0.9929,0.0235 -4.500,-0.4126,0.01748,0.01002,-0.0146,0.9872,0.0241 -4.250,-0.3730,0.01613,0.00859,-0.0168,0.9825,0.0260 -4.000,-0.3389,0.01479,0.00716,-0.0180,0.9751,0.0304 -3.750,-0.3006,0.01311,0.00567,-0.0201,0.9701,0.0771 -3.500,-0.2716,0.01164,0.00528,-0.0212,0.9618,0.2967 -3.250,-0.2330,0.01114,0.00506,-0.0236,0.9562,0.3825 -3.000,-0.2038,0.01072,0.00489,-0.0238,0.9463,0.4582 -2.750,-0.1761,0.01029,0.00477,-0.0235,0.9369,0.5444 -2.500,-0.1488,0.00990,0.00465,-0.0229,0.9282,0.6247 -2.250,-0.1268,0.00955,0.00458,-0.0210,0.9167,0.7041 -2.000,-0.1001,0.00924,0.00452,-0.0198,0.9064,0.7934 -1.750,-0.0486,0.00907,0.00445,-0.0234,0.9006,0.8820 -1.500,0.0063,0.00910,0.00441,-0.0282,0.8919,0.9295 -1.250,0.0525,0.00919,0.00437,-0.0312,0.8824,0.9575 -1.000,0.0999,0.00926,0.00429,-0.0346,0.8723,0.9782 -0.750,0.1501,0.00923,0.00415,-0.0390,0.8603,0.9959 -0.500,0.1785,0.00916,0.00395,-0.0392,0.8460,1.0000 -0.250,0.1978,0.00911,0.00379,-0.0373,0.8310,1.0000 0.000,0.2183,0.00908,0.00366,-0.0357,0.8160,1.0000 0.250,0.2399,0.00905,0.00353,-0.0342,0.8005,1.0000 0.500,0.2621,0.00903,0.00343,-0.0329,0.7840,1.0000 0.750,0.2848,0.00902,0.00334,-0.0317,0.7670,1.0000 1.000,0.3078,0.00901,0.00325,-0.0304,0.7497,1.0000 1.250,0.3310,0.00902,0.00317,-0.0292,0.7321,1.0000 1.500,0.3548,0.00905,0.00312,-0.0282,0.7130,1.0000 1.750,0.3787,0.00911,0.00308,-0.0272,0.6931,1.0000 2.000,0.4027,0.00919,0.00305,-0.0262,0.6739,1.0000 2.250,0.4271,0.00929,0.00310,-0.0253,0.6524,1.0000 2.500,0.4514,0.00943,0.00313,-0.0244,0.6323,1.0000 2.750,0.4761,0.00957,0.00320,-0.0237,0.6103,1.0000 3.000,0.5005,0.00974,0.00327,-0.0229,0.5896,1.0000 3.250,0.5253,0.00990,0.00341,-0.0222,0.5671,1.0000 3.500,0.5497,0.01011,0.00352,-0.0214,0.5457,1.0000 3.750,0.5744,0.01031,0.00367,-0.0207,0.5228,1.0000 4.000,0.5989,0.01053,0.00383,-0.0200,0.5004,1.0000 4.250,0.6233,0.01078,0.00403,-0.0193,0.4774,1.0000 4.500,0.6477,0.01103,0.00424,-0.0186,0.4536,1.0000 4.750,0.6718,0.01131,0.00446,-0.0179,0.4298,1.0000 5.000,0.6957,0.01162,0.00471,-0.0172,0.4054,1.0000 5.250,0.7196,0.01193,0.00500,-0.0165,0.3793,1.0000 5.500,0.7432,0.01227,0.00530,-0.0158,0.3529,1.0000 5.750,0.7665,0.01265,0.00563,-0.0150,0.3263,1.0000 6.000,0.7895,0.01308,0.00600,-0.0143,0.2993,1.0000 6.250,0.8121,0.01354,0.00642,-0.0135,0.2723,1.0000 6.500,0.8343,0.01405,0.00687,-0.0127,0.2460,1.0000 6.750,0.8560,0.01463,0.00736,-0.0118,0.2210,1.0000 7.000,0.8775,0.01522,0.00790,-0.0109,0.1967,1.0000 7.250,0.8987,0.01584,0.00849,-0.0100,0.1732,1.0000 7.500,0.9188,0.01658,0.00914,-0.0090,0.1521,1.0000 7.750,0.9392,0.01728,0.00987,-0.0080,0.1316,1.0000 8.000,0.9577,0.01817,0.01067,-0.0069,0.1141,1.0000 8.250,0.9767,0.01901,0.01152,-0.0057,0.0974,1.0000 8.500,0.9946,0.01994,0.01246,-0.0044,0.0832,1.0000 8.750,1.0112,0.02099,0.01352,-0.0030,0.0713,1.0000 9.000,1.0253,0.02232,0.01481,-0.0013,0.0618,1.0000 9.250,1.0421,0.02329,0.01591,0.0002,0.0540,1.0000 9.500,1.0550,0.02481,0.01748,0.0020,0.0480,1.0000 9.750,1.0697,0.02592,0.01871,0.0036,0.0429,1.0000 10.000,1.0803,0.02820,0.02101,0.0055,0.0393,1.0000 10.250,1.0946,0.02949,0.02251,0.0072,0.0364,1.0000 10.500,1.1064,0.03070,0.02384,0.0089,0.0333,1.0000 10.750,1.1154,0.03286,0.02603,0.0106,0.0307,1.0000 11.000,1.1221,0.03539,0.02883,0.0127,0.0289,1.0000 11.250,1.1251,0.03679,0.03046,0.0153,0.0271,1.0000 11.500,1.1264,0.03827,0.03210,0.0175,0.0251,1.0000 11.750,1.1274,0.04021,0.03415,0.0192,0.0237,1.0000 12.000,1.1251,0.04309,0.03709,0.0206,0.0220,1.0000 12.250,1.1132,0.04669,0.04099,0.0218,0.0209,1.0000 12.500,1.1068,0.04955,0.04411,0.0223,0.0203,1.0000 12.750,1.0984,0.05279,0.04759,0.0222,0.0193,1.0000 13.000,1.0890,0.05657,0.05158,0.0214,0.0187,1.0000 13.250,1.0765,0.06110,0.05631,0.0199,0.0180,1.0000 13.500,1.0613,0.06645,0.06189,0.0176,0.0181,1.0000 13.750,1.0450,0.07229,0.06792,0.0146,0.0178,1.0000 14.000,1.0258,0.07903,0.07487,0.0107,0.0180,1.0000 14.250,1.0008,0.08745,0.08350,0.0057,0.0188,1.0000 14.500,0.9768,0.09631,0.09253,0.0001,0.0191,1.0000 14.750,0.9495,0.10664,0.10301,-0.0065,0.0197,1.0000 15.000,0.9174,0.11826,0.11469,-0.0126,0.0213,1.0000