Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-eh2070-il-100000-n5 Airfoil,eh2070-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,45.8423 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-eh2070-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -7.750,-0.5322,0.09104,0.08655,0.0072,1.0000,0.0372 -7.500,-0.5327,0.08731,0.08288,0.0046,1.0000,0.0376 -7.250,-0.5313,0.08339,0.07899,0.0015,1.0000,0.0381 -7.000,-0.5267,0.07929,0.07489,-0.0015,1.0000,0.0385 -6.750,-0.5203,0.07508,0.07066,-0.0042,1.0000,0.0387 -6.500,-0.5074,0.07169,0.06697,-0.0107,1.0000,0.0427 -6.250,-0.4600,0.05450,0.05028,-0.0096,1.0000,0.0264 -6.000,-0.4529,0.04939,0.04507,-0.0111,1.0000,0.0246 -5.750,-0.4438,0.04400,0.03954,-0.0125,1.0000,0.0228 -5.500,-0.4316,0.03807,0.03333,-0.0136,1.0000,0.0209 -5.250,-0.4158,0.03266,0.02757,-0.0140,1.0000,0.0198 -5.000,-0.4202,0.04140,0.03558,-0.0130,1.0000,0.0199 -4.750,-0.4031,0.03985,0.03399,-0.0130,1.0000,0.0237 -4.500,-0.3820,0.03643,0.03023,-0.0125,1.0000,0.0252 -4.250,-0.3603,0.03274,0.02614,-0.0116,1.0000,0.0244 -4.000,-0.3375,0.02934,0.02227,-0.0105,1.0000,0.0238 -3.750,-0.3137,0.02634,0.01879,-0.0094,1.0000,0.0234 -3.500,-0.2891,0.02378,0.01577,-0.0083,1.0000,0.0233 -3.250,-0.2640,0.02161,0.01322,-0.0072,1.0000,0.0234 -3.000,-0.2390,0.01982,0.01107,-0.0062,1.0000,0.0239 -2.750,-0.2147,0.01832,0.00939,-0.0052,1.0000,0.0249 -2.500,-0.1842,0.01693,0.00785,-0.0056,0.9855,0.0270 -2.250,-0.1463,0.01574,0.00656,-0.0076,0.9513,0.0334 -2.000,-0.1093,0.01480,0.00556,-0.0093,0.9159,0.0497 -1.750,-0.0769,0.01388,0.00481,-0.0099,0.8804,0.1065 -1.500,-0.0519,0.01246,0.00428,-0.0097,0.8471,0.3390 -1.250,0.0277,0.01110,0.00435,-0.0165,0.8247,0.9777 -1.000,0.0814,0.01108,0.00389,-0.0216,0.7921,1.0000 -0.750,0.1036,0.01114,0.00367,-0.0203,0.7627,1.0000 -0.500,0.1260,0.01121,0.00348,-0.0192,0.7375,1.0000 -0.250,0.1486,0.01129,0.00331,-0.0180,0.7149,1.0000 0.000,0.1717,0.01138,0.00320,-0.0171,0.6939,1.0000 0.250,0.1948,0.01147,0.00311,-0.0161,0.6749,1.0000 0.500,0.2181,0.01158,0.00306,-0.0152,0.6570,1.0000 0.750,0.2414,0.01169,0.00303,-0.0143,0.6399,1.0000 1.000,0.2653,0.01182,0.00304,-0.0135,0.6238,1.0000 1.250,0.2892,0.01195,0.00305,-0.0127,0.6086,1.0000 1.500,0.3131,0.01209,0.00310,-0.0119,0.5939,1.0000 1.750,0.3371,0.01225,0.00316,-0.0112,0.5798,1.0000 2.000,0.3611,0.01241,0.00325,-0.0105,0.5658,1.0000 2.250,0.3854,0.01258,0.00342,-0.0098,0.5522,1.0000 2.500,0.4096,0.01275,0.00355,-0.0091,0.5388,1.0000 2.750,0.4340,0.01294,0.00372,-0.0084,0.5258,1.0000 3.000,0.4584,0.01314,0.00391,-0.0077,0.5128,1.0000 3.250,0.4829,0.01334,0.00413,-0.0071,0.4998,1.0000 3.500,0.5074,0.01355,0.00437,-0.0065,0.4868,1.0000 3.750,0.5321,0.01378,0.00472,-0.0059,0.4738,1.0000 4.000,0.5568,0.01401,0.00502,-0.0053,0.4608,1.0000 4.250,0.5815,0.01426,0.00534,-0.0047,0.4479,1.0000 4.500,0.6064,0.01453,0.00571,-0.0042,0.4353,1.0000 4.750,0.6313,0.01481,0.00611,-0.0036,0.4226,1.0000 5.000,0.6561,0.01510,0.00653,-0.0030,0.4092,1.0000 5.250,0.6809,0.01539,0.00698,-0.0024,0.3946,1.0000 5.500,0.7054,0.01568,0.00755,-0.0018,0.3774,1.0000 5.750,0.7266,0.01585,0.00756,-0.0007,0.3021,1.0000 6.000,0.7406,0.01779,0.00832,0.0002,0.1026,1.0000 6.250,0.7557,0.02022,0.01022,0.0013,0.0302,1.0000 6.500,0.7757,0.02165,0.01190,0.0024,0.0246,1.0000 6.750,0.7948,0.02307,0.01360,0.0035,0.0218,1.0000 7.000,0.8103,0.02487,0.01556,0.0047,0.0182,1.0000 7.250,0.8275,0.02641,0.01727,0.0059,0.0158,1.0000 7.500,0.8445,0.02816,0.01918,0.0073,0.0150,1.0000 7.750,0.8625,0.03013,0.02142,0.0087,0.0144,1.0000 8.000,0.8810,0.03238,0.02388,0.0099,0.0140,1.0000 8.250,0.8992,0.03492,0.02668,0.0111,0.0137,1.0000 8.500,0.9155,0.03772,0.02983,0.0123,0.0135,1.0000 8.750,0.9287,0.04078,0.03327,0.0134,0.0134,1.0000 9.000,0.9376,0.04414,0.03705,0.0146,0.0133,1.0000 9.250,0.9420,0.04762,0.04093,0.0158,0.0134,1.0000 9.500,0.9413,0.05125,0.04493,0.0168,0.0134,1.0000 9.750,0.9356,0.05484,0.04884,0.0176,0.0135,1.0000 10.000,0.9231,0.05828,0.05251,0.0184,0.0135,1.0000 10.250,0.9089,0.06215,0.05658,0.0176,0.0136,1.0000 10.500,0.8941,0.06678,0.06139,0.0150,0.0137,1.0000 10.750,0.8793,0.07212,0.06688,0.0114,0.0138,1.0000 11.000,0.8627,0.07853,0.07344,0.0066,0.0139,1.0000 11.250,0.8483,0.08520,0.08020,0.0016,0.0140,1.0000