XFOIL Version 6.96 Calculated polar for: GOE 766 AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -18.250 -1.1300 0.09612 0.09349 -0.0160 1.0000 0.0205 -18.000 -1.1767 0.08372 0.08090 -0.0236 1.0000 0.0205 -17.750 -1.2111 0.07385 0.07085 -0.0299 1.0000 0.0205 -17.500 -1.2377 0.06554 0.06237 -0.0353 1.0000 0.0206 -17.250 -1.2579 0.05854 0.05521 -0.0398 1.0000 0.0206 -17.000 -1.2661 0.05364 0.05018 -0.0430 1.0000 0.0208 -16.750 -1.2773 0.04871 0.04510 -0.0458 1.0000 0.0210 -16.500 -1.2810 0.04508 0.04134 -0.0476 1.0000 0.0211 -16.250 -1.2813 0.04208 0.03823 -0.0488 1.0000 0.0213 -16.000 -1.2807 0.03942 0.03544 -0.0495 1.0000 0.0215 -15.750 -1.2782 0.03716 0.03307 -0.0498 1.0000 0.0216 -15.500 -1.2896 0.03377 0.02952 -0.0494 1.0000 0.0219 -15.250 -1.2911 0.03159 0.02725 -0.0485 1.0000 0.0221 -15.000 -1.2864 0.03011 0.02572 -0.0473 1.0000 0.0224 -14.750 -1.2792 0.02894 0.02449 -0.0459 1.0000 0.0226 -14.500 -1.2712 0.02790 0.02340 -0.0443 1.0000 0.0229 -14.250 -1.2595 0.02722 0.02269 -0.0427 1.0000 0.0232 -14.000 -1.2506 0.02634 0.02174 -0.0407 1.0000 0.0235 -13.750 -1.2400 0.02565 0.02099 -0.0386 1.0000 0.0238 -13.500 -1.2303 0.02492 0.02018 -0.0362 1.0000 0.0241 -13.250 -1.2202 0.02429 0.01947 -0.0336 1.0000 0.0244 -13.000 -1.2094 0.02368 0.01879 -0.0310 1.0000 0.0247 -12.750 -1.1951 0.02308 0.01812 -0.0290 1.0000 0.0250 -12.500 -1.1783 0.02263 0.01759 -0.0273 1.0000 0.0252 -12.250 -1.1694 0.02125 0.01611 -0.0247 1.0000 0.0257 -12.000 -1.1547 0.02045 0.01527 -0.0228 1.0000 0.0261 -11.750 -1.1370 0.01991 0.01471 -0.0211 1.0000 0.0265 -11.500 -1.1178 0.01948 0.01427 -0.0197 1.0000 0.0269 -11.250 -1.0981 0.01909 0.01385 -0.0183 1.0000 0.0274 -11.000 -1.0785 0.01864 0.01336 -0.0168 1.0000 0.0278 -10.750 -1.0590 0.01816 0.01282 -0.0153 1.0000 0.0282 -10.500 -1.0392 0.01769 0.01230 -0.0138 1.0000 0.0286 -10.250 -1.0185 0.01730 0.01186 -0.0125 1.0000 0.0290 -10.000 -0.9972 0.01697 0.01148 -0.0111 1.0000 0.0292 -9.750 -0.9818 0.01599 0.01046 -0.0090 1.0000 0.0300 -9.500 -0.9624 0.01547 0.00992 -0.0074 1.0000 0.0305 -9.250 -0.9420 0.01506 0.00951 -0.0060 1.0000 0.0310 -9.000 -0.9213 0.01470 0.00913 -0.0045 1.0000 0.0315 -8.750 -0.9005 0.01434 0.00875 -0.0030 1.0000 0.0320 -8.500 -0.8794 0.01401 0.00840 -0.0016 1.0000 0.0326 -8.250 -0.8583 0.01372 0.00808 -0.0001 1.0000 0.0331 -8.000 -0.8375 0.01340 0.00773 0.0014 1.0000 0.0335 -7.750 -0.8168 0.01311 0.00741 0.0030 1.0000 0.0339 -7.500 -0.8004 0.01245 0.00673 0.0052 1.0000 0.0348 -7.250 -0.7812 0.01209 0.00638 0.0070 1.0000 0.0355 -7.000 -0.7488 0.01177 0.00606 0.0061 0.9986 0.0362 -6.750 -0.7129 0.01149 0.00578 0.0045 0.9962 0.0373 -6.500 -0.6764 0.01121 0.00549 0.0027 0.9936 0.0383 -6.250 -0.6429 0.01094 0.00521 0.0017 0.9900 0.0389 -6.000 -0.6096 0.01043 0.00471 0.0006 0.9857 0.0404 -5.750 -0.5728 0.01012 0.00441 -0.0012 0.9821 0.0419 -5.500 -0.5412 0.00986 0.00416 -0.0018 0.9744 0.0432 -5.250 -0.5019 0.00964 0.00393 -0.0040 0.9686 0.0447 -5.000 -0.4632 0.00923 0.00354 -0.0062 0.9549 0.0476 -4.750 -0.4207 0.00898 0.00325 -0.0090 0.9238 0.0504 -4.500 -0.3923 0.00883 0.00298 -0.0088 0.8764 0.0536 -4.250 -0.3695 0.00879 0.00277 -0.0074 0.8171 0.0573 -4.000 -0.3482 0.00883 0.00257 -0.0057 0.7449 0.0623 -3.750 -0.3255 0.00882 0.00240 -0.0044 0.6887 0.0701 -3.500 -0.3020 0.00870 0.00223 -0.0033 0.6460 0.0870 -3.250 -0.2781 0.00855 0.00211 -0.0024 0.6111 0.1161 -3.000 -0.2531 0.00847 0.00201 -0.0016 0.5807 0.1360 -2.750 -0.2274 0.00843 0.00192 -0.0010 0.5533 0.1499 -2.500 -0.2014 0.00839 0.00184 -0.0004 0.5300 0.1632 -2.250 -0.1754 0.00831 0.00175 0.0001 0.5111 0.1793 -2.000 -0.1498 0.00819 0.00166 0.0007 0.4950 0.2042 -1.750 -0.1249 0.00795 0.00157 0.0015 0.4812 0.2526 -1.500 -0.1017 0.00757 0.00147 0.0024 0.4694 0.3409 -1.250 -0.0776 0.00731 0.00140 0.0033 0.4580 0.4099 -1.000 -0.0541 0.00700 0.00133 0.0042 0.4474 0.4872 -0.750 -0.0317 0.00667 0.00131 0.0055 0.4375 0.5829 -0.500 -0.0076 0.00652 0.00130 0.0065 0.4272 0.6430 -0.250 0.0174 0.00641 0.00130 0.0074 0.4186 0.6838 0.000 0.0425 0.00634 0.00131 0.0082 0.4094 0.7193 0.250 0.0678 0.00626 0.00132 0.0091 0.4012 0.7537 0.500 0.0936 0.00624 0.00134 0.0098 0.3919 0.7792 0.750 0.1198 0.00621 0.00137 0.0105 0.3833 0.8037 1.000 0.1454 0.00620 0.00140 0.0113 0.3733 0.8323 1.250 0.1714 0.00617 0.00145 0.0120 0.3635 0.8639 1.500 0.1983 0.00620 0.00151 0.0126 0.3526 0.8909 1.750 0.2270 0.00626 0.00157 0.0127 0.3413 0.9093 2.000 0.2573 0.00633 0.00164 0.0125 0.3299 0.9253 2.250 0.2888 0.00645 0.00172 0.0120 0.3178 0.9396 2.500 0.3245 0.00662 0.00183 0.0105 0.3043 0.9493 2.750 0.3585 0.00677 0.00193 0.0094 0.2922 0.9579 3.000 0.3936 0.00695 0.00205 0.0081 0.2806 0.9652 3.250 0.4280 0.00714 0.00219 0.0069 0.2703 0.9707 3.500 0.4660 0.00731 0.00231 0.0049 0.2623 0.9732 3.750 0.5015 0.00748 0.00244 0.0034 0.2536 0.9761 4.000 0.5342 0.00765 0.00256 0.0025 0.2451 0.9804 4.250 0.5690 0.00782 0.00269 0.0011 0.2386 0.9831 4.500 0.6060 0.00793 0.00279 -0.0007 0.2326 0.9847 4.750 0.6408 0.00810 0.00291 -0.0022 0.2260 0.9866 5.000 0.6754 0.00821 0.00301 -0.0035 0.2211 0.9887 5.250 0.7089 0.00834 0.00312 -0.0046 0.2147 0.9912 5.500 0.7410 0.00852 0.00327 -0.0055 0.2081 0.9935 5.750 0.7765 0.00860 0.00336 -0.0070 0.2024 0.9948 6.000 0.8110 0.00877 0.00348 -0.0085 0.1940 0.9964 6.250 0.8456 0.00887 0.00358 -0.0099 0.1867 0.9981 6.500 0.8795 0.00905 0.00371 -0.0112 0.1771 0.9995 6.750 0.9062 0.00925 0.00385 -0.0111 0.1653 1.0000 7.000 0.9276 0.00949 0.00403 -0.0098 0.1515 1.0000 7.250 0.9483 0.00980 0.00426 -0.0085 0.1361 1.0000 7.500 0.9687 0.01014 0.00453 -0.0071 0.1213 1.0000 7.750 0.9890 0.01051 0.00483 -0.0057 0.1086 1.0000 8.000 1.0092 0.01089 0.00515 -0.0043 0.0975 1.0000 8.250 1.0292 0.01128 0.00549 -0.0028 0.0877 1.0000 8.500 1.0494 0.01166 0.00583 -0.0014 0.0797 1.0000 8.750 1.0702 0.01200 0.00615 -0.0001 0.0740 1.0000 9.000 1.0901 0.01241 0.00654 0.0013 0.0684 1.0000 9.250 1.1111 0.01272 0.00686 0.0026 0.0652 1.0000 9.500 1.1307 0.01316 0.00727 0.0040 0.0614 1.0000 9.750 1.1514 0.01350 0.00764 0.0053 0.0589 1.0000 10.000 1.1718 0.01385 0.00801 0.0066 0.0565 1.0000 10.250 1.1909 0.01431 0.00846 0.0081 0.0540 1.0000 10.500 1.2101 0.01475 0.00893 0.0095 0.0521 1.0000 10.750 1.2307 0.01508 0.00930 0.0108 0.0507 1.0000 11.000 1.2501 0.01549 0.00972 0.0121 0.0490 1.0000 11.250 1.2681 0.01599 0.01024 0.0137 0.0474 1.0000 11.500 1.2843 0.01660 0.01088 0.0154 0.0457 1.0000 11.750 1.3038 0.01696 0.01129 0.0167 0.0448 1.0000 12.000 1.3225 0.01738 0.01175 0.0181 0.0437 1.0000 12.250 1.3399 0.01785 0.01225 0.0196 0.0426 1.0000 12.500 1.3553 0.01842 0.01284 0.0213 0.0414 1.0000 12.750 1.3666 0.01919 0.01364 0.0236 0.0402 1.0000 13.000 1.3799 0.01980 0.01431 0.0256 0.0395 1.0000 13.250 1.3926 0.02026 0.01483 0.0278 0.0388 1.0000 13.500 1.4025 0.02081 0.01543 0.0303 0.0381 1.0000 13.750 1.4126 0.02144 0.01610 0.0326 0.0373 1.0000 14.000 1.4212 0.02223 0.01693 0.0347 0.0366 1.0000 14.250 1.4273 0.02326 0.01802 0.0367 0.0359 1.0000 14.500 1.4296 0.02467 0.01949 0.0385 0.0351 1.0000 14.750 1.4297 0.02647 0.02138 0.0397 0.0344 1.0000 15.000 1.4377 0.02788 0.02287 0.0402 0.0341 1.0000 15.250 1.4438 0.02964 0.02472 0.0403 0.0336 1.0000 15.500 1.4487 0.03175 0.02691 0.0399 0.0330 1.0000 15.750 1.4505 0.03445 0.02971 0.0390 0.0325 1.0000 16.000 1.4512 0.03746 0.03281 0.0376 0.0320 1.0000 16.250 1.4461 0.04137 0.03682 0.0358 0.0317 1.0000 16.500 1.4395 0.04548 0.04102 0.0338 0.0312 1.0000 16.750 1.4259 0.05050 0.04614 0.0316 0.0309 1.0000 17.000 1.4084 0.05594 0.05169 0.0292 0.0306 1.0000 17.250 1.3876 0.06181 0.05766 0.0267 0.0303 1.0000 17.500 1.3658 0.06779 0.06374 0.0241 0.0300 1.0000 17.750 1.3478 0.07339 0.06944 0.0218 0.0298 1.0000 18.000 1.3373 0.07821 0.07436 0.0196 0.0296 1.0000 18.250 1.3265 0.08313 0.07936 0.0175 0.0293 1.0000 18.500 1.3148 0.08822 0.08454 0.0152 0.0291 1.0000 18.750 1.3043 0.09324 0.08965 0.0130 0.0288 1.0000