Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-mh25-il-50000 Airfoil,mh25-il Reynolds number,50000 Ncrit,9 Mach,0 Max Cl/Cd,34.434 Max Cl/Cd alpha,5.75 Url,http://airfoiltools.com/polar/csv?polar=xf-mh25-il-50000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.4666,0.11289,0.10613,-0.0232,1.0000,0.2334 -9.250,-0.4768,0.11105,0.10437,-0.0227,1.0000,0.2438 -9.000,-0.4672,0.10716,0.10052,-0.0210,1.0000,0.2554 -8.750,-0.4649,0.10394,0.09735,-0.0196,1.0000,0.2658 -8.500,-0.4678,0.10101,0.09450,-0.0181,1.0000,0.2787 -8.250,-0.4716,0.09834,0.09192,-0.0165,1.0000,0.2911 -8.000,-0.4738,0.09556,0.08921,-0.0144,1.0000,0.3063 -7.750,-0.4779,0.09297,0.08669,-0.0122,1.0000,0.3216 -7.500,-0.5002,0.09144,0.08530,-0.0092,1.0000,0.3398 -5.500,-0.6012,0.05637,0.04931,-0.0121,1.0000,0.1437 -5.250,-0.5937,0.05147,0.04320,-0.0095,1.0000,0.1082 -5.000,-0.5787,0.04717,0.03889,-0.0078,1.0000,0.1008 -4.750,-0.5643,0.04366,0.03470,-0.0051,1.0000,0.0919 -4.500,-0.5481,0.04036,0.03096,-0.0029,1.0000,0.0875 -4.250,-0.5288,0.03742,0.02726,-0.0003,1.0000,0.0832 -4.000,-0.5080,0.03491,0.02444,0.0014,1.0000,0.0848 -3.750,-0.4862,0.03292,0.02201,0.0030,1.0000,0.0914 -3.500,-0.1782,0.02388,0.01565,-0.0353,1.0000,1.0000 -3.250,-0.1710,0.02349,0.01490,-0.0326,1.0000,1.0000 -3.000,-0.1626,0.02320,0.01428,-0.0300,1.0000,1.0000 -2.750,-0.1532,0.02296,0.01367,-0.0274,1.0000,1.0000 -2.500,-0.1432,0.02278,0.01322,-0.0249,1.0000,1.0000 -2.250,-0.1325,0.02264,0.01282,-0.0223,1.0000,1.0000 -2.000,-0.1216,0.02254,0.01249,-0.0199,1.0000,1.0000 -1.750,-0.1103,0.02247,0.01221,-0.0174,1.0000,1.0000 -1.500,-0.0988,0.02244,0.01199,-0.0150,1.0000,1.0000 -1.250,-0.0871,0.02243,0.01180,-0.0126,1.0000,1.0000 -1.000,-0.0753,0.02245,0.01166,-0.0102,1.0000,1.0000 -0.750,-0.0634,0.02250,0.01153,-0.0079,1.0000,1.0000 -0.500,-0.0515,0.02258,0.01148,-0.0056,1.0000,1.0000 -0.250,-0.0394,0.02269,0.01147,-0.0033,1.0000,1.0000 0.000,-0.0274,0.02283,0.01151,-0.0011,1.0000,1.0000 0.250,-0.0154,0.02300,0.01158,0.0010,1.0000,1.0000 0.500,-0.0033,0.02320,0.01168,0.0032,1.0000,1.0000 0.750,0.0088,0.02344,0.01185,0.0052,1.0000,1.0000 1.000,0.0208,0.02371,0.01207,0.0072,1.0000,1.0000 1.250,0.0328,0.02402,0.01234,0.0091,1.0000,1.0000 1.500,0.0448,0.02438,0.01267,0.0109,1.0000,1.0000 1.750,0.0567,0.02478,0.01305,0.0127,1.0000,1.0000 2.000,0.0684,0.02523,0.01349,0.0143,1.0000,1.0000 2.250,0.0799,0.02574,0.01400,0.0159,1.0000,1.0000 2.500,0.0913,0.02631,0.01457,0.0174,1.0000,1.0000 2.750,0.1025,0.02694,0.01522,0.0187,1.0000,1.0000 3.000,0.1136,0.02764,0.01595,0.0199,1.0000,1.0000 3.250,0.1244,0.02841,0.01677,0.0210,1.0000,1.0000 3.500,0.1919,0.03051,0.01908,0.0109,0.9752,1.0000 3.750,0.2564,0.03217,0.02095,0.0021,0.9468,1.0000 4.000,0.3164,0.03334,0.02236,-0.0052,0.9185,1.0000 4.250,0.3772,0.03405,0.02343,-0.0118,0.8899,1.0000 4.500,0.4266,0.03420,0.02387,-0.0158,0.8591,1.0000 4.750,0.4855,0.03382,0.02387,-0.0205,0.8275,1.0000 5.000,0.5555,0.03255,0.02316,-0.0257,0.7942,1.0000 5.250,0.6550,0.02915,0.02052,-0.0329,0.7554,1.0000 5.500,0.7578,0.02465,0.01682,-0.0384,0.6873,1.0000 5.750,0.8061,0.02341,0.01544,-0.0373,0.5848,1.0000 6.000,0.8233,0.02406,0.01558,-0.0331,0.4888,1.0000 6.250,0.8328,0.02531,0.01627,-0.0285,0.4035,1.0000 6.500,0.8406,0.02687,0.01732,-0.0243,0.3282,1.0000 6.750,0.8516,0.02871,0.01864,-0.0208,0.2636,1.0000 7.000,0.8630,0.03057,0.02021,-0.0176,0.2125,1.0000 7.250,0.8852,0.03311,0.02260,-0.0161,0.1736,1.0000 7.500,0.8999,0.03513,0.02470,-0.0137,0.1467,1.0000 7.750,0.9275,0.03845,0.02803,-0.0132,0.1299,1.0000 8.000,0.9416,0.04120,0.03129,-0.0102,0.1203,1.0000 8.250,0.9491,0.04380,0.03424,-0.0068,0.1106,1.0000 8.500,0.9637,0.04718,0.03768,-0.0048,0.1032,1.0000 8.750,0.9638,0.05052,0.04161,-0.0004,0.1017,1.0000 9.000,0.9606,0.05415,0.04574,0.0041,0.1009,1.0000 9.250,0.9543,0.05778,0.04977,0.0085,0.1008,1.0000 9.500,0.9452,0.06152,0.05385,0.0127,0.1013,1.0000 9.750,0.9336,0.06532,0.05793,0.0167,0.1019,1.0000 10.000,0.9184,0.06902,0.06185,0.0205,0.1022,1.0000 10.250,0.9016,0.07274,0.06574,0.0240,0.1026,1.0000 10.500,0.8867,0.07651,0.06961,0.0270,0.1032,1.0000 10.750,0.8706,0.08055,0.07373,0.0294,0.1036,1.0000 11.000,0.7116,0.07872,0.07243,0.0330,0.1146,1.0000 11.250,0.6355,0.09473,0.08825,0.0221,0.1406,1.0000