naca0005: AirfoilSeq = AirfoilSeq(
[
(1.000000, 0.002100),
(0.999748, 0.002159),
(0.998993, 0.002335),
(0.997736, 0.002629),
(0.995977, 0.003038),
(0.993719, 0.003563),
(0.990964, 0.004201),
(0.987715, 0.004951),
(0.983974, 0.005811),
(0.979746, 0.006778),
(0.975036, 0.007849),
(0.969846, 0.009023),
(0.964184, 0.010294),
(0.958054, 0.011661),
(0.951463, 0.013120),
(0.944418, 0.014667),
(0.936925, 0.016298),
(0.928992, 0.018009),
(0.920627, 0.019796),
(0.911838, 0.021655),
(0.902635, 0.023581),
(0.893027, 0.025570),
(0.883022, 0.027617),
(0.872632, 0.029719),
(0.861867, 0.031869),
(0.850737, 0.034065),
(0.839255, 0.036300),
(0.827430, 0.038571),
(0.815276, 0.040873),
(0.802805, 0.043200),
(0.790028, 0.045548),
(0.776960, 0.047913),
(0.763613, 0.050289),
(0.750000, 0.052672),
(0.736136, 0.055056),
(0.722033, 0.057436),
(0.707708, 0.059808),
(0.693173, 0.062167),
(0.678443, 0.064506),
(0.663534, 0.066821),
(0.648460, 0.069106),
(0.633237, 0.071355),
(0.617879, 0.073564),
(0.602403, 0.075726),
(0.586824, 0.077836),
(0.571157, 0.079887),
(0.555419, 0.081874),
(0.539625, 0.083790),
(0.523791, 0.085631),
(0.507933, 0.087388),
(0.492067, 0.089057),
(0.476209, 0.090630),
(0.460375, 0.092103),
(0.444581, 0.093469),
(0.428843, 0.094722),
(0.413176, 0.095855),
(0.397597, 0.096865),
(0.382121, 0.097744),
(0.366763, 0.098487),
(0.351540, 0.099090),
(0.336466, 0.099548),
(0.321557, 0.099856),
(0.306827, 0.100011),
(0.292292, 0.100007),
(0.277967, 0.099843),
(0.263864, 0.099515),
(0.250000, 0.099021),
(0.236387, 0.098358),
(0.223040, 0.097527),
(0.209972, 0.096524),
(0.197195, 0.095351),
(0.184724, 0.094007),
(0.172570, 0.092493),
(0.160745, 0.090810),
(0.149263, 0.088960),
(0.138133, 0.086945),
(0.127368, 0.084768),
(0.116978, 0.082431),
(0.106973, 0.079939),
(0.097365, 0.077295),
(0.088162, 0.074503),
(0.079373, 0.071568),
(0.071008, 0.068495),
(0.063075, 0.065289),
(0.055582, 0.061955),
(0.048537, 0.058498),
(0.041946, 0.054924),
(0.035816, 0.051238),
(0.030154, 0.047445),
(0.024964, 0.043550),
(0.020254, 0.039559),
(0.016026, 0.035477),
(0.012285, 0.031307),
(0.009036, 0.027055),
(0.006281, 0.022724),
(0.004023, 0.018318),
(0.002264, 0.013840),
(0.001007, 0.009293),
(0.000252, 0.004679),
(0.000000, 0.000000),
(0.000252, -0.004679),
(0.001007, -0.009293),
(0.002264, -0.013840),
(0.004023, -0.018318),
(0.006281, -0.022724),
(0.009036, -0.027055),
(0.012285, -0.031307),
(0.016026, -0.035477),
(0.020254, -0.039559),
(0.024964, -0.043550),
(0.030154, -0.047445),
(0.035816, -0.051238),
(0.041946, -0.054924),
(0.048537, -0.058498),
(0.055582, -0.061955),
(0.063075, -0.065289),
(0.071008, -0.068495),
(0.079373, -0.071568),
(0.088162, -0.074503),
(0.097365, -0.077295),
(0.106973, -0.079939),
(0.116978, -0.082431),
(0.127368, -0.084768),
(0.138133, -0.086945),
(0.149263, -0.088960),
(0.160745, -0.090810),
(0.172570, -0.092493),
(0.184724, -0.094007),
(0.197195, -0.095351),
(0.209972, -0.096524),
(0.223040, -0.097527),
(0.236387, -0.098358),
(0.250000, -0.099021),
(0.263864, -0.099515),
(0.277967, -0.099843),
(0.292292, -0.100007),
(0.306827, -0.100011),
(0.321557, -0.099856),
(0.336466, -0.099548),
(0.351540, -0.099090),
(0.366763, -0.098487),
(0.382121, -0.097744),
(0.397597, -0.096865),
(0.413176, -0.095855),
(0.428843, -0.094722),
(0.444581, -0.093469),
(0.460375, -0.092103),
(0.476209, -0.090630),
(0.492067, -0.089057),
(0.507933, -0.087388),
(0.523791, -0.085631),
(0.539625, -0.083790),
(0.555419, -0.081874),
(0.571157, -0.079887),
(0.586824, -0.077836),
(0.602403, -0.075726),
(0.617879, -0.073564),
(0.633237, -0.071355),
(0.648460, -0.069106),
(0.663534, -0.066821),
(0.678443, -0.064506),
(0.693173, -0.062167),
(0.707708, -0.059808),
(0.722033, -0.057436),
(0.736136, -0.055056),
(0.750000, -0.052672),
(0.763613, -0.050289),
(0.776960, -0.047913),
(0.790028, -0.045548),
(0.802805, -0.043200),
(0.815276, -0.040873),
(0.827430, -0.038571),
(0.839255, -0.036300),
(0.850737, -0.034065),
(0.861867, -0.031869),
(0.872632, -0.029719),
(0.883022, -0.027617),
(0.893027, -0.025570),
(0.902635, -0.023581),
(0.911838, -0.021655),
(0.920627, -0.019796),
(0.928992, -0.018009),
(0.936925, -0.016298),
(0.944418, -0.014667),
(0.951463, -0.013120),
(0.958054, -0.011661),
(0.964184, -0.010294),
(0.969846, -0.009023),
(0.975036, -0.007849),
(0.979746, -0.006778),
(0.983974, -0.005811),
(0.987715, -0.004951),
(0.990964, -0.004201),
(0.993719, -0.003563),
(0.995977, -0.003038),
(0.997736, -0.002629),
(0.998993, -0.002335),
(0.999748, -0.002159),
(1.000000, -0.002100),
]
)
naca5305: AirfoilSeq = AirfoilSeq([
(1.000074, 0.000520),
(0.998545, 0.000829),
(0.993968, 0.001750),
(0.986369, 0.003267),
(0.975792, 0.005351),
(0.962301, 0.007964),
(0.945974, 0.011059),
(0.926909, 0.014580),
(0.905218, 0.018465),
(0.881032, 0.022648),
(0.854494, 0.027058),
(0.825764, 0.031621),
(0.795017, 0.036263),
(0.762437, 0.040911),
(0.728224, 0.045493),
(0.692585, 0.049938),
(0.655739, 0.054180),
(0.617912, 0.058158),
(0.579336, 0.061813),
(0.540252, 0.065095),
(0.500900, 0.067958),
(0.461525, 0.070367),
(0.422374, 0.072291),
(0.383692, 0.073709),
(0.345722, 0.074611),
(0.308702, 0.074992),
(0.272257, 0.074521),
(0.237079, 0.072481),
(0.203612, 0.069020),
(0.172090, 0.064350),
(0.142727, 0.058704),
(0.115719, 0.052328),
(0.091240, 0.045475),
(0.069442, 0.038397),
(0.050454, 0.031335),
(0.034383, 0.024516),
(0.021313, 0.018141),
(0.011308, 0.012382),
(0.004410, 0.007379),
(0.000639, 0.003232),
(0.000000, 0.000000),
(0.002443, -0.002207),
(0.007902, -0.003318),
(0.016322, -0.003385),
(0.027630, -0.002492),
(0.041737, -0.000752),
(0.058539, 0.001696),
(0.077918, 0.004691),
(0.099743, 0.008055),
(0.123875, 0.011591),
(0.150167, 0.015098),
(0.178462, 0.018365),
(0.208603, 0.021185),
(0.240422, 0.023351),
(0.273752, 0.024670),
(0.308614, 0.024992),
(0.345261, 0.024967),
(0.382862, 0.024875),
(0.421191, 0.024682),
(0.460016, 0.024358),
(0.499100, 0.023878),
(0.538207, 0.023226),
(0.577098, 0.022390),
(0.615534, 0.021370),
(0.653278, 0.020171),
(0.690099, 0.018807),
(0.725767, 0.017298),
(0.760061, 0.015670),
(0.792768, 0.013955),
(0.823684, 0.012188),
(0.852613, 0.010407),
(0.879374, 0.008651),
(0.903799, 0.006957),
(0.925731, 0.005364),
(0.945032, 0.003906),
(0.961578, 0.002615),
(0.975264, 0.001519),
(0.986001, 0.000641),
(0.993720, 0.000001),
(0.998372, -0.000389),
(0.999926, -0.000520),
])
naca5305: AirfoilSeq = AirfoilSeq([
(1.000074, 0.000520),
(0.999825, 0.000570),
(0.999076, 0.000722),
(0.997829, 0.000974),
(0.996084, 0.001325),
(0.993844, 0.001775),
(0.991111, 0.002322),
(0.987887, 0.002965),
(0.984175, 0.003702),
(0.979979, 0.004530),
(0.975303, 0.005447),
(0.970152, 0.006450),
(0.964530, 0.007536),
(0.958442, 0.008702),
(0.951896, 0.009945),
(0.944896, 0.011261),
(0.937450, 0.012645),
(0.929565, 0.014095),
(0.921249, 0.015606),
(0.912509, 0.017173),
(0.903355, 0.018793),
(0.893795, 0.020460),
(0.883838, 0.022171),
(0.873495, 0.023920),
(0.862775, 0.025702),
(0.851689, 0.027513),
(0.840247, 0.029348),
(0.828462, 0.031201),
(0.816345, 0.033069),
(0.803907, 0.034946),
(0.791162, 0.036828),
(0.778120, 0.038709),
(0.764797, 0.040584),
(0.751204, 0.042449),
(0.737356, 0.044300),
(0.723265, 0.046131),
(0.708947, 0.047939),
(0.694416, 0.049718),
(0.679685, 0.051464),
(0.664770, 0.053174),
(0.649686, 0.054843),
(0.634447, 0.056466),
(0.619070, 0.058042),
(0.603569, 0.059564),
(0.587961, 0.061031),
(0.572261, 0.062439),
(0.556485, 0.063784),
(0.540648, 0.065063),
(0.524768, 0.066275),
(0.508859, 0.067415),
(0.492939, 0.068483),
(0.477023, 0.069475),
(0.461128, 0.070389),
(0.445270, 0.071224),
(0.429465, 0.071978),
(0.413729, 0.072650),
(0.398079, 0.073239),
(0.382530, 0.073744),
(0.367099, 0.074165),
(0.351800, 0.074500),
(0.336651, 0.074751),
(0.321667, 0.074916),
(0.306862, 0.074998),
(0.292078, 0.074968),
(0.277356, 0.074684),
(0.262866, 0.074133),
(0.248627, 0.073328),
(0.234654, 0.072280),
(0.220963, 0.071003),
(0.207570, 0.069508),
(0.194490, 0.067812),
(0.181738, 0.065929),
(0.169328, 0.063874),
(0.157274, 0.061662),
(0.145589, 0.059311),
(0.134285, 0.056837),
(0.123376, 0.054256),
(0.112871, 0.051585),
(0.102783, 0.048841),
(0.093120, 0.046040),
(0.083894, 0.043200),
(0.075113, 0.040335),
(0.066786, 0.037463),
(0.058920, 0.034599),
(0.051523, 0.031758),
(0.044601, 0.028955),
(0.038161, 0.026204),
(0.032208, 0.023517),
(0.026747, 0.020908),
(0.021783, 0.018387),
(0.017318, 0.015967),
(0.013357, 0.013657),
(0.009902, 0.011466),
(0.006955, 0.009402),
(0.004518, 0.007472),
(0.002592, 0.005682),
(0.001177, 0.004037),
(0.000274, 0.002540),
-(0.000118, 0.001194),
(0.000000, 0.000000),
(0.000621, -0.001026),
(0.001739, -0.001870),
(0.003351, -0.002533),
(0.005453, -0.003018),
(0.008043, -0.003329),
(0.011116, -0.003469),
(0.014668, -0.003444),
(0.018694, -0.003259),
(0.023189, -0.002921),
(0.028146, -0.002437),
(0.033560, -0.001815),
(0.039424, -0.001065),
(0.045730, -0.000195),
(0.052472, 0.000785),
(0.059642, 0.001864),
(0.067231, 0.003030),
(0.075231, 0.004273),
(0.083633, 0.005580),
(0.092429, 0.006939),
(0.101609, 0.008337),
(0.111164, 0.009760),
(0.121084, 0.011196),
(0.131360, 0.012631),
(0.141981, 0.014051),
(0.152936, 0.015442),
(0.164217, 0.016791),
(0.175811, 0.018084),
(0.187709, 0.019306),
(0.199900, 0.020445),
(0.212373, 0.021486),
(0.225117, 0.022417),
(0.238121, 0.023223),
(0.251373, 0.023894),
(0.264863, 0.024416),
(0.278578, 0.024777),
(0.292507, 0.024966),
(0.306793, 0.024993),
(0.321447, 0.024989),
(0.336281, 0.024978),
(0.351279, 0.024958),
(0.366428, 0.024926),
(0.381711, 0.024879),
(0.397114, 0.024817),
(0.412623, 0.024736),
(0.428220, 0.024634),
(0.443892, 0.024510),
(0.459622, 0.024362),
(0.475395, 0.024189),
(0.491195, 0.023989),
(0.507007, 0.023761),
(0.522814, 0.023504),
(0.538602, 0.023218),
(0.554354, 0.022902),
(0.570054, 0.022556),
(0.585687, 0.022180),
(0.601237, 0.021773),
(0.616689, 0.021337),
(0.632027, 0.020871),
(0.647235, 0.020377),
(0.662298, 0.019855),
(0.677201, 0.019307),
(0.691930, 0.018734),
(0.706468, 0.018138),
(0.720801, 0.017519),
(0.734915, 0.016881),
(0.748796, 0.016224),
(0.762428, 0.015551),
(0.775800, 0.014865),
(0.788895, 0.014167),
(0.801702, 0.013459),
(0.814208, 0.012745),
(0.826398, 0.012027),
(0.838262, 0.011306),
(0.849786, 0.010587),
(0.860959, 0.009871),
(0.871770, 0.009161),
(0.882206, 0.008459),
(0.892258, 0.007768),
(0.901916, 0.007091),
(0.911168, 0.006429),
(0.920005, 0.005786),
(0.928418, 0.005164),
(0.936399, 0.004564),
(0.943940, 0.003990),
(0.951031, 0.003442),
(0.957666, 0.002923),
(0.963838, 0.002435),
(0.969541, 0.001980),
(0.974768, 0.001559),
(0.979514, 0.001173),
(0.983774, 0.000824),
(0.987543, 0.000514),
(0.990818, 0.000242),
(0.993595, 0.000011),
(0.995871, -0.000179),
(0.997643, -0.000328),
(0.998911, -0.000434),
(0.999672, -0.000498),
(0.999926, -0.000520),
])
naca0005: AirfoilSeq = AirfoilSeq([
(1.000000, 0.000525),
(0.999748, 0.000540),
(0.998993, 0.000584),
(0.997736, 0.000657),
(0.995977, 0.000760),
(0.993719, 0.000891),
(0.990964, 0.001050),
(0.987715, 0.001238),
(0.983974, 0.001453),
(0.979746, 0.001694),
(0.975036, 0.001962),
(0.969846, 0.002256),
(0.964184, 0.002574),
(0.958054, 0.002915),
(0.951463, 0.003280),
(0.944418, 0.003667),
(0.936925, 0.004075),
(0.928992, 0.004502),
(0.920627, 0.004949),
(0.911838, 0.005414),
(0.902635, 0.005895),
(0.893027, 0.006392),
(0.883022, 0.006904),
(0.872632, 0.007430),
(0.861867, 0.007967),
(0.850737, 0.008516),
(0.839255, 0.009075),
(0.827430, 0.009643),
(0.815276, 0.010218),
(0.802805, 0.010800),
(0.790028, 0.011387),
(0.776960, 0.011978),
(0.763613, 0.012572),
(0.750000, 0.013168),
(0.736136, 0.013764),
(0.722033, 0.014359),
(0.707708, 0.014952),
(0.693173, 0.015542),
(0.678443, 0.016126),
(0.663534, 0.016705),
(0.648460, 0.017276),
(0.633237, 0.017839),
(0.617879, 0.018391),
(0.602403, 0.018932),
(0.586824, 0.019459),
(0.571157, 0.019972),
(0.555419, 0.020468),
(0.539625, 0.020948),
(0.523791, 0.021408),
(0.507933, 0.021847),
(0.492067, 0.022264),
(0.476209, 0.022658),
(0.460375, 0.023026),
(0.444581, 0.023367),
(0.428843, 0.023680),
(0.413176, 0.023964),
(0.397597, 0.024216),
(0.382121, 0.024436),
(0.366763, 0.024622),
(0.351540, 0.024773),
(0.336466, 0.024887),
(0.321557, 0.024964),
(0.306827, 0.025003),
(0.292292, 0.025002),
(0.277967, 0.024961),
(0.263864, 0.024879),
(0.250000, 0.024755),
(0.236387, 0.024590),
(0.223040, 0.024382),
(0.209972, 0.024131),
(0.197195, 0.023838),
(0.184724, 0.023502),
(0.172570, 0.023123),
(0.160745, 0.022703),
(0.149263, 0.022240),
(0.138133, 0.021736),
(0.127368, 0.021192),
(0.116978, 0.020608),
(0.106973, 0.019985),
(0.097365, 0.019324),
(0.088162, 0.018626),
(0.079373, 0.017892),
(0.071008, 0.017124),
(0.063075, 0.016322),
(0.055582, 0.015489),
(0.048537, 0.014625),
(0.041946, 0.013731),
(0.035816, 0.012809),
(0.030154, 0.011861),
(0.024964, 0.010888),
(0.020254, 0.009890),
(0.016026, 0.008869),
(0.012285, 0.007827),
(0.009036, 0.006764),
(0.006281, 0.005681),
(0.004023, 0.004580),
(0.002264, 0.003460),
(0.001007, 0.002323),
(0.000252, 0.001170),
(0.000000, 0.000000),
(0.000252, -0.001170),
(0.001007, -0.002323),
(0.002264, -0.003460),
(0.004023, -0.004580),
(0.006281, -0.005681),
(0.009036, -0.006764),
(0.012285, -0.007827),
(0.016026, -0.008869),
(0.020254, -0.009890),
(0.024964, -0.010888),
(0.030154, -0.011861),
(0.035816, -0.012809),
(0.041946, -0.013731),
(0.048537, -0.014625),
(0.055582, -0.015489),
(0.063075, -0.016322),
(0.071008, -0.017124),
(0.079373, -0.017892),
(0.088162, -0.018626),
(0.097365, -0.019324),
(0.106973, -0.019985),
(0.116978, -0.020608),
(0.127368, -0.021192),
(0.138133, -0.021736),
(0.149263, -0.022240),
(0.160745, -0.022703),
(0.172570, -0.023123),
(0.184724, -0.023502),
(0.197195, -0.023838),
(0.209972, -0.024131),
(0.223040, -0.024382),
(0.236387, -0.024590),
(0.250000, -0.024755),
(0.263864, -0.024879),
(0.277967, -0.024961),
(0.292292, -0.025002),
(0.306827, -0.025003),
(0.321557, -0.024964),
(0.336466, -0.024887),
(0.351540, -0.024773),
(0.366763, -0.024622),
(0.382121, -0.024436),
(0.397597, -0.024216),
(0.413176, -0.023964),
(0.428843, -0.023680),
(0.444581, -0.023367),
(0.460375, -0.023026),
(0.476209, -0.022658),
(0.492067, -0.022264),
(0.507933, -0.021847),
(0.523791, -0.021408),
(0.539625, -0.020948),
(0.555419, -0.020468),
(0.571157, -0.019972),
(0.586824, -0.019459),
(0.602403, -0.018932),
(0.617879, -0.018391),
(0.633237, -0.017839),
(0.648460, -0.017276),
(0.663534, -0.016705),
(0.678443, -0.016126),
(0.693173, -0.015542),
(0.707708, -0.014952),
(0.722033, -0.014359),
(0.736136, -0.013764),
(0.750000, -0.013168),
(0.763613, -0.012572),
(0.776960, -0.011978),
(0.790028, -0.011387),
(0.802805, -0.010800),
(0.815276, -0.010218),
(0.827430, -0.009643),
(0.839255, -0.009075),
(0.850737, -0.008516),
(0.861867, -0.007967),
(0.872632, -0.007430),
(0.883022, -0.006904),
(0.893027, -0.006392),
(0.902635, -0.005895),
(0.911838, -0.005414),
(0.920627, -0.004949),
(0.928992, -0.004502),
(0.936925, -0.004075),
(0.944418, -0.003667),
(0.951463, -0.003280),
(0.958054, -0.002915),
(0.964184, -0.002574),
(0.969846, -0.002256),
(0.975036, -0.001962),
(0.979746, -0.001694),
(0.983974, -0.001453),
(0.987715, -0.001238),
(0.990964, -0.001050),
(0.993719, -0.000891),
(0.995977, -0.000760),
(0.997736, -0.000657),
(0.998993, -0.000584),
(0.999748, -0.000540),
(1.000000, -0.000525),
])
naca0005: AirfoilSeq = AirfoilSeq([
(1.000000, 0.000525),
(0.998459, 0.000615),
(0.993844, 0.000884),
(0.986185, 0.001326),
(0.975528, 0.001934),
(0.961940, 0.002699),
(0.945503, 0.003607),
(0.926320, 0.004645),
(0.904508, 0.005798),
(0.880203, 0.007048),
(0.853553, 0.008378),
(0.824724, 0.009772),
(0.793893, 0.011210),
(0.761249, 0.012676),
(0.726995, 0.014151),
(0.691342, 0.015615),
(0.654508, 0.017049),
(0.616723, 0.018432),
(0.578217, 0.019743),
(0.539230, 0.020959),
(0.500000, 0.022058),
(0.460770, 0.023017),
(0.421783, 0.023812),
(0.383277, 0.024421),
(0.345492, 0.024823),
(0.308658, 0.025000),
(0.273005, 0.024937),
(0.238751, 0.024622),
(0.206107, 0.024048),
(0.175276, 0.023212),
(0.146447, 0.022118),
(0.119797, 0.020772),
(0.095492, 0.019187),
(0.073680, 0.017377),
(0.054497, 0.015361),
(0.038060, 0.013158),
(0.024472, 0.010789),
(0.013815, 0.008272),
(0.006156, 0.005626),
(0.001541, 0.002865),
(0.000000, 0.000000),
(0.001541, -0.002865),
(0.006156, -0.005626),
(0.013815, -0.008272),
(0.024472, -0.010789),
(0.038060, -0.013158),
(0.054497, -0.015361),
(0.073680, -0.017377),
(0.095492, -0.019187),
(0.119797, -0.020772),
(0.146447, -0.022118),
(0.175276, -0.023212),
(0.206107, -0.024048),
(0.238751, -0.024622),
(0.273005, -0.024937),
(0.308658, -0.025000),
(0.345492, -0.024823),
(0.383277, -0.024421),
(0.421783, -0.023812),
(0.460770, -0.023017),
(0.500000, -0.022058),
(0.539230, -0.020959),
(0.578217, -0.019743),
(0.616723, -0.018432),
(0.654508, -0.017049),
(0.691342, -0.015615),
(0.726995, -0.014151),
(0.761249, -0.012676),
(0.793893, -0.011210),
(0.824724, -0.009772),
(0.853553, -0.008378),
(0.880203, -0.007048),
(0.904508, -0.005798),
(0.926320, -0.004645),
(0.945503, -0.003607),
(0.961940, -0.002699),
(0.975528, -0.001934),
(0.986185, -0.001326),
(0.993844, -0.000884),
(0.998459, -0.000615),
(1.000000, -0.000525),
])
mh49: AirfoilSeq = AirfoilSeq([
(1000, 0),
(996.64, -0.35),
(986.52, -1.22),
(969.69, -2.19),
(946.38, -2.94),
(916.87, -3.2201),
(881.52, -2.73),
(840.76, -1.08),
(795.4099, 2.3),
(746.78, 7.58),
(696.0499, 14.49),
(644.25, 22.63),
(592.43, 31.51),
(541.62, 40.22),
(492.05, 47.49),
(443.25, 52.85),
(395.16, 56.54),
(348.13, 58.73),
(302.52, 59.54),
(258.77, 59.09),
(217.31, 57.46),
(178.56, 54.73),
(142.88, 50.97),
(110.65, 46.27),
(82.14, 40.72),
(57.6, 34.42),
(37.22, 27.53),
(21.16, 20.24),
(9.5, 12.77),
(2.31, 5.52),
(0, -0.6401),
(3.58, -6.35),
(12.87, -12.61),
(26.91, -18.98),
(45.49, -25.06),
(68.4599, -30.6),
(95.67, -35.38),
(126.96, -39.27),
(162.17, -42.19),
(201.05, -44.17),
(243.26, -45.23),
(288.42, -45.47),
(336.07, -44.96),
(385.72, -43.7701),
(436.86, -42),
(488.92, -39.76),
(541.32, -37.15),
(593.43, -34.27),
(644.64, -31.2),
(694.34, -28),
(741.95, -24.73),
(786.9199, -21.44),
(828.74, -18.19),
(866.93, -15.06),
(900.97, -12.13),
(930.44, -9.4),
(954.97, -6.9),
(974.25, -4.6101),
(988.17, -2.44),
(996.89, -0.6801),
])
goe63: AirfoilSeq = AirfoilSeq(
[
[1000, 3.5],
[949.83, 15.03],
[899.71, 25.76],
[799.48, 45.61],
[699.25, 65.47],
[599.05, 83.43],
[498.88, 97.9899],
[398.8, 105.65],
[298.79, 106.21],
[198.86, 99.87],
[148.95, 91.8],
[99.0999, 79.03],
[74.2, 69.95],
[49.34, 57.66],
[24.55, 39.48],
[12.2, 26.64],
[0, 0],
[12.66, -14.26],
[25.15, -13.51],
[50.09, -7.73],
[75.02, -1.74],
[99.9599, 3.74],
[149.87, 11.31],
[199.8, 17.38],
[299.72, 24.42],
[399.68, 28.26],
[499.69, 27.3],
[599.72, 24.14],
[699.8, 17.88],
[799.88, 10.72],
[899.96, 3.56],
[949.99, 0.83],
]
)