Xfoil polar. Reynolds number fixed. Mach number fixed Polar key,xf-fx77w343-il-500000 Airfoil,fx77w343-il Reynolds number,500000 Ncrit,9 Mach,0 Max Cl/Cd,45.1724 Max Cl/Cd alpha,7.25 Url,http://airfoiltools.com/polar/csv?polar=xf-fx77w343-il-500000 Alpha,Cl,Cd,Cdp,Cm,Top_Xtr,Bot_Xtr -19.250,-0.9600,0.10342,0.09602,-0.0149,0.4982,0.0364 -19.000,-0.9546,0.10070,0.09325,-0.0158,0.4953,0.0368 -18.750,-0.9496,0.09791,0.09040,-0.0167,0.4925,0.0372 -18.500,-0.9422,0.09544,0.08786,-0.0175,0.4897,0.0377 -18.250,-0.9348,0.09298,0.08532,-0.0183,0.4867,0.0382 -18.000,-0.9279,0.09046,0.08274,-0.0190,0.4849,0.0387 -17.750,-0.9188,0.08823,0.08045,-0.0196,0.4833,0.0392 -17.500,-0.9094,0.08603,0.07818,-0.0201,0.4816,0.0396 -17.250,-0.9030,0.08353,0.07564,-0.0206,0.4799,0.0400 -17.000,-0.8986,0.08088,0.07297,-0.0211,0.4782,0.0405 -16.750,-0.8936,0.07828,0.07034,-0.0215,0.4765,0.0410 -16.500,-0.8862,0.07599,0.06799,-0.0219,0.4747,0.0415 -16.250,-0.8774,0.07386,0.06581,-0.0222,0.4729,0.0420 -16.000,-0.8687,0.07172,0.06361,-0.0226,0.4711,0.0426 -15.750,-0.8583,0.06976,0.06158,-0.0229,0.4692,0.0431 -15.500,-0.8466,0.06796,0.05970,-0.0232,0.4669,0.0436 -15.250,-0.8372,0.06595,0.05765,-0.0234,0.4657,0.0440 -15.000,-0.8283,0.06393,0.05562,-0.0235,0.4647,0.0447 -14.750,-0.8183,0.06205,0.05372,-0.0236,0.4637,0.0453 -14.500,-0.8076,0.06023,0.05188,-0.0237,0.4625,0.0459 -14.250,-0.7951,0.05863,0.05025,-0.0238,0.4613,0.0465 -14.000,-0.7819,0.05711,0.04872,-0.0239,0.4601,0.0473 -13.750,-0.7685,0.05562,0.04720,-0.0239,0.4589,0.0480 -13.500,-0.7554,0.05411,0.04568,-0.0240,0.4577,0.0489 -13.250,-0.7408,0.05278,0.04435,-0.0240,0.4565,0.0500 -13.000,-0.7252,0.05155,0.04310,-0.0241,0.4553,0.0512 -12.750,-0.7092,0.05034,0.04189,-0.0242,0.4541,0.0526 -12.500,-0.6928,0.04917,0.04071,-0.0243,0.4529,0.0543 -12.250,-0.6762,0.04805,0.03954,-0.0244,0.4517,0.0562 -12.000,-0.6590,0.04701,0.03847,-0.0244,0.4503,0.0578 -11.750,-0.6412,0.04605,0.03747,-0.0245,0.4486,0.0598 -11.500,-0.6216,0.04526,0.03662,-0.0248,0.4466,0.0616 -11.250,-0.6075,0.04400,0.03536,-0.0246,0.4461,0.0630 -11.000,-0.5912,0.04292,0.03426,-0.0245,0.4455,0.0646 -10.750,-0.5730,0.04199,0.03332,-0.0245,0.4449,0.0662 -10.500,-0.5584,0.04085,0.03217,-0.0243,0.4442,0.0678 -10.250,-0.5448,0.03966,0.03098,-0.0240,0.4436,0.0696 -10.000,-0.5299,0.03858,0.02989,-0.0237,0.4430,0.0714 -9.750,-0.5158,0.03749,0.02881,-0.0233,0.4423,0.0733 -9.500,-0.5019,0.03644,0.02777,-0.0229,0.4417,0.0755 -9.250,-0.4884,0.03541,0.02677,-0.0224,0.4410,0.0785 -9.000,-0.4763,0.03433,0.02574,-0.0217,0.4403,0.0825 -8.750,-0.4645,0.03324,0.02471,-0.0210,0.4397,0.0928 -8.500,-0.4488,0.03240,0.02387,-0.0205,0.4390,0.0993 -8.250,-0.4337,0.03154,0.02300,-0.0200,0.4383,0.1038 -8.000,-0.4214,0.03053,0.02200,-0.0192,0.4377,0.1084 -7.750,-0.4120,0.02939,0.02090,-0.0181,0.4371,0.1143 -7.500,-0.4090,0.02801,0.01963,-0.0162,0.4365,0.1274 -7.250,-0.4095,0.02697,0.01859,-0.0134,0.4360,0.1410 -7.000,-0.4070,0.02596,0.01758,-0.0111,0.4354,0.1482 -6.750,-0.3938,0.02481,0.01649,-0.0111,0.4346,0.1598 -6.500,-0.3749,0.02340,0.01522,-0.0127,0.4337,0.1922 -6.250,-0.3467,0.02241,0.01430,-0.0153,0.4329,0.2105 -6.000,-0.3140,0.02111,0.01317,-0.0194,0.4322,0.2531 -5.750,-0.2794,0.02000,0.01228,-0.0234,0.4313,0.3057 -5.500,-0.2422,0.01900,0.01154,-0.0277,0.4304,0.3642 -5.250,-0.2042,0.01835,0.01117,-0.0315,0.4291,0.4259 -5.000,-0.1691,0.01846,0.01140,-0.0339,0.4277,0.4544 -4.750,-0.1336,0.01840,0.01148,-0.0362,0.4271,0.4870 -4.500,-0.0987,0.01834,0.01147,-0.0380,0.4267,0.5039 -4.000,-0.0299,0.01844,0.01174,-0.0413,0.4258,0.5342 -3.750,0.0043,0.01856,0.01189,-0.0428,0.4253,0.5481 -3.500,0.0387,0.01866,0.01194,-0.0444,0.4247,0.5567 -3.250,0.0722,0.01883,0.01215,-0.0457,0.4241,0.5633 -3.000,0.1062,0.01897,0.01229,-0.0472,0.4233,0.5709 -2.750,0.1399,0.01913,0.01244,-0.0487,0.4225,0.5770 -2.500,0.1727,0.01942,0.01277,-0.0498,0.4216,0.5822 -2.250,0.2059,0.01968,0.01304,-0.0510,0.4208,0.5877 -2.000,0.2399,0.01987,0.01318,-0.0526,0.4200,0.5934 -1.750,0.2723,0.02020,0.01354,-0.0537,0.4192,0.5966 -1.500,0.3050,0.02050,0.01384,-0.0548,0.4184,0.5998 -1.250,0.3380,0.02077,0.01409,-0.0561,0.4176,0.6036 -1.000,0.3717,0.02098,0.01425,-0.0577,0.4167,0.6078 -0.750,0.4057,0.02114,0.01435,-0.0593,0.4159,0.6113 -0.500,0.4376,0.02138,0.01460,-0.0602,0.4150,0.6133 -0.250,0.4694,0.02166,0.01488,-0.0612,0.4141,0.6156 0.000,0.5014,0.02195,0.01516,-0.0621,0.4133,0.6184 0.250,0.5338,0.02224,0.01542,-0.0633,0.4124,0.6214 0.500,0.5665,0.02257,0.01570,-0.0646,0.4114,0.6247 0.750,0.5991,0.02309,0.01616,-0.0662,0.4102,0.6278 1.000,0.6295,0.02384,0.01692,-0.0675,0.4089,0.6300 1.250,0.6606,0.02394,0.01707,-0.0684,0.4084,0.6317 1.500,0.6913,0.02414,0.01732,-0.0693,0.4078,0.6333 1.750,0.7217,0.02442,0.01765,-0.0701,0.4072,0.6352 2.000,0.7517,0.02475,0.01802,-0.0709,0.4064,0.6374 2.250,0.7818,0.02508,0.01839,-0.0717,0.4055,0.6401 2.500,0.8122,0.02538,0.01872,-0.0726,0.4046,0.6429 2.750,0.8433,0.02563,0.01897,-0.0739,0.4036,0.6455 3.000,0.8749,0.02589,0.01923,-0.0753,0.4026,0.6479 3.250,0.9058,0.02601,0.01936,-0.0766,0.4015,0.6501 3.500,0.9347,0.02618,0.01958,-0.0773,0.4006,0.6520 3.750,0.9635,0.02642,0.01985,-0.0779,0.3996,0.6536 4.000,0.9929,0.02662,0.02007,-0.0787,0.3987,0.6551 4.250,1.0230,0.02676,0.02021,-0.0797,0.3978,0.6565 4.500,1.0537,0.02686,0.02030,-0.0809,0.3970,0.6577 4.750,1.0846,0.02695,0.02038,-0.0821,0.3962,0.6589 5.000,1.1157,0.02703,0.02043,-0.0834,0.3954,0.6602 5.250,1.1470,0.02714,0.02050,-0.0848,0.3945,0.6615 5.500,1.1775,0.02738,0.02071,-0.0861,0.3934,0.6631 5.750,1.2022,0.02841,0.02177,-0.0869,0.3913,0.6647 6.000,1.2301,0.02855,0.02193,-0.0879,0.3907,0.6662 6.250,1.2569,0.02876,0.02218,-0.0888,0.3900,0.6674 6.500,1.2826,0.02903,0.02249,-0.0895,0.3890,0.6684 6.750,1.3063,0.02938,0.02287,-0.0899,0.3879,0.6692 7.000,1.3287,0.02957,0.02312,-0.0902,0.3866,0.6705 7.250,1.3493,0.02987,0.02347,-0.0901,0.3854,0.6716 7.500,1.3677,0.03031,0.02397,-0.0897,0.3843,0.6727 7.750,1.3849,0.03076,0.02447,-0.0891,0.3833,0.6737 8.000,1.4012,0.03120,0.02494,-0.0884,0.3822,0.6747 8.250,1.4053,0.03181,0.02559,-0.0857,0.3811,0.6756 8.500,1.4166,0.03244,0.02625,-0.0845,0.3801,0.6767 8.750,1.4345,0.03299,0.02681,-0.0843,0.3791,0.6781 9.000,1.4566,0.03337,0.02719,-0.0846,0.3781,0.6795 9.250,1.4803,0.03370,0.02749,-0.0852,0.3771,0.6808 9.500,1.5036,0.03414,0.02791,-0.0857,0.3756,0.6822 9.750,1.4964,0.03664,0.03050,-0.0839,0.3736,0.6834 10.000,0.7309,0.12178,0.11693,-0.0652,0.3141,0.6775