Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fx77w153-il-100000-n5 Airfoil,fx77w153-il Reynolds number,100000 Ncrit,5 Mach,0 Max Cl/Cd,33.8307 Max Cl/Cd alpha,8.25 Url,http://airfoiltools.com/polar/csv?polar=xf-fx77w153-il-100000-n5 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -9.500,-0.2452,0.10582,0.10005,-0.0122,0.5333,0.0623 -9.250,-0.2623,0.09685,0.09106,-0.0170,0.5338,0.0423 -8.750,-0.3632,0.09022,0.08429,-0.0177,0.5419,0.0368 -8.500,-0.3557,0.08750,0.08155,-0.0182,0.5358,0.0364 -8.250,-0.3521,0.08378,0.07782,-0.0204,0.5311,0.0358 -8.000,-0.3528,0.07893,0.07295,-0.0246,0.5276,0.0351 -7.750,-0.3589,0.07376,0.06771,-0.0284,0.5251,0.0343 -7.500,-0.3892,0.06020,0.05371,-0.0360,0.5265,0.0314 -7.250,-0.3840,0.05659,0.04990,-0.0363,0.5225,0.0312 -7.000,-0.3777,0.05277,0.04583,-0.0363,0.5184,0.0311 -6.750,-0.3700,0.04892,0.04165,-0.0360,0.5146,0.0309 -6.500,-0.3604,0.04517,0.03749,-0.0353,0.5112,0.0308 -6.000,-0.3338,0.03849,0.02983,-0.0332,0.5045,0.0310 -5.750,-0.3170,0.03558,0.02634,-0.0319,0.5010,0.0316 -5.500,-0.2949,0.03447,0.02515,-0.0315,0.4972,0.0325 -5.250,-0.2728,0.03319,0.02361,-0.0309,0.4939,0.0338 -5.000,-0.2504,0.03150,0.02150,-0.0300,0.4911,0.0351 -4.750,-0.2265,0.02967,0.01922,-0.0291,0.4875,0.0362 -4.500,-0.2014,0.02817,0.01744,-0.0285,0.4841,0.0372 -4.250,-0.1759,0.02718,0.01632,-0.0281,0.4810,0.0384 -4.000,-0.1497,0.02619,0.01514,-0.0276,0.4784,0.0402 -3.750,-0.1229,0.02519,0.01383,-0.0270,0.4762,0.0427 -3.500,-0.0970,0.02457,0.01321,-0.0267,0.4740,0.0458 -3.250,-0.0704,0.02401,0.01255,-0.0264,0.4715,0.0507 -3.000,-0.0439,0.02366,0.01215,-0.0261,0.4691,0.0572 -2.750,-0.0182,0.02313,0.01169,-0.0258,0.4669,0.0621 -2.500,0.0079,0.02266,0.01113,-0.0253,0.4649,0.0656 -2.250,0.0335,0.02228,0.01075,-0.0249,0.4630,0.0702 -2.000,0.0594,0.02198,0.01035,-0.0243,0.4613,0.0750 -1.750,0.0851,0.02168,0.00998,-0.0238,0.4597,0.0803 -1.500,0.1112,0.02144,0.00967,-0.0233,0.4578,0.0895 -1.250,0.1370,0.02112,0.00951,-0.0230,0.4550,0.1089 -1.000,0.1624,0.02063,0.00939,-0.0227,0.4524,0.1852 -0.750,0.1868,0.01972,0.00935,-0.0225,0.4500,0.4081 -0.500,0.2767,0.01863,0.00979,-0.0330,0.4465,0.9162 -0.250,0.3635,0.01903,0.00985,-0.0440,0.4436,0.9996 0.000,0.3890,0.01921,0.00981,-0.0437,0.4421,1.0000 0.250,0.4136,0.01945,0.00999,-0.0434,0.4401,1.0000 0.500,0.4382,0.01973,0.01020,-0.0431,0.4382,1.0000 0.750,0.4627,0.02001,0.01041,-0.0427,0.4363,1.0000 1.000,0.4871,0.02030,0.01063,-0.0423,0.4344,1.0000 1.250,0.5115,0.02060,0.01084,-0.0419,0.4326,1.0000 1.500,0.5359,0.02090,0.01106,-0.0414,0.4309,1.0000 1.750,0.5604,0.02119,0.01126,-0.0410,0.4293,1.0000 2.000,0.5848,0.02149,0.01146,-0.0405,0.4278,1.0000 2.250,0.6095,0.02177,0.01162,-0.0400,0.4263,1.0000 2.500,0.6328,0.02221,0.01208,-0.0395,0.4237,1.0000 2.750,0.6557,0.02266,0.01257,-0.0390,0.4205,1.0000 3.000,0.6790,0.02306,0.01296,-0.0384,0.4176,1.0000 3.250,0.7026,0.02340,0.01327,-0.0379,0.4152,1.0000 3.500,0.7267,0.02370,0.01351,-0.0373,0.4131,1.0000 3.750,0.7510,0.02398,0.01372,-0.0368,0.4112,1.0000 4.000,0.7758,0.02426,0.01390,-0.0362,0.4095,1.0000 4.250,0.7957,0.02500,0.01480,-0.0355,0.4061,1.0000 4.500,0.8164,0.02564,0.01552,-0.0348,0.4028,1.0000 4.750,0.8383,0.02613,0.01605,-0.0341,0.4000,1.0000 5.000,0.8613,0.02652,0.01642,-0.0335,0.3977,1.0000 5.250,0.8849,0.02687,0.01674,-0.0329,0.3958,1.0000 5.500,0.9091,0.02719,0.01702,-0.0324,0.3941,1.0000 5.750,0.9289,0.02792,0.01784,-0.0316,0.3916,1.0000 6.000,0.9434,0.02907,0.01919,-0.0304,0.3877,1.0000 6.250,0.9614,0.02987,0.02008,-0.0295,0.3846,1.0000 6.500,0.9821,0.03040,0.02063,-0.0287,0.3821,1.0000 6.750,1.0058,0.03064,0.02088,-0.0281,0.3799,1.0000 7.000,1.0319,0.03067,0.02084,-0.0276,0.3780,1.0000 7.250,1.0381,0.03221,0.02263,-0.0258,0.3726,1.0000 7.500,1.0529,0.03301,0.02352,-0.0245,0.3683,1.0000 7.750,1.0750,0.03324,0.02378,-0.0238,0.3656,1.0000 8.000,1.1003,0.03328,0.02381,-0.0232,0.3636,1.0000 8.250,1.1269,0.03331,0.02381,-0.0229,0.3621,1.0000 8.500,1.1071,0.03673,0.02760,-0.0195,0.3550,1.0000 8.750,1.1169,0.03788,0.02885,-0.0181,0.3516,1.0000 9.000,1.1370,0.03826,0.02928,-0.0173,0.3493,1.0000 9.250,1.1625,0.03829,0.02931,-0.0168,0.3477,1.0000 9.500,1.1912,0.03814,0.02916,-0.0166,0.3463,1.0000 10.000,1.0923,0.04958,0.04098,-0.0113,0.3309,1.0000 11.500,0.9175,0.09081,0.08253,-0.0209,0.2761,1.0000