XFOIL Version 6.96 Calculated polar for: MH 24 9.01% 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -10.000 -0.4798 0.09542 0.09315 -0.0327 1.0000 0.0084 -9.750 -0.4821 0.09187 0.08963 -0.0336 1.0000 0.0086 -9.250 -0.4954 0.08436 0.08220 -0.0349 1.0000 0.0086 -6.750 -0.4444 0.03509 0.03158 -0.0591 0.9703 0.0067 -6.500 -0.4386 0.03053 0.02662 -0.0567 0.9665 0.0061 -6.250 -0.4281 0.02714 0.02287 -0.0541 0.9625 0.0057 -6.000 -0.4128 0.02359 0.01887 -0.0519 0.9596 0.0052 -5.750 -0.3933 0.01988 0.01461 -0.0499 0.9575 0.0045 -5.500 -0.3688 0.01764 0.01199 -0.0490 0.9560 0.0042 -5.250 -0.3474 0.01644 0.01057 -0.0476 0.9533 0.0041 -5.000 -0.3251 0.01534 0.00927 -0.0463 0.9505 0.0040 -4.750 -0.3010 0.01446 0.00826 -0.0455 0.9481 0.0039 -4.500 -0.2762 0.01364 0.00733 -0.0449 0.9460 0.0039 -4.250 -0.2513 0.01279 0.00638 -0.0443 0.9440 0.0039 -4.000 -0.2271 0.01209 0.00560 -0.0435 0.9417 0.0039 -3.750 -0.2068 0.01155 0.00497 -0.0419 0.9374 0.0039 -3.500 -0.1834 0.01103 0.00436 -0.0409 0.9341 0.0040 -3.250 -0.1577 0.01064 0.00387 -0.0404 0.9315 0.0042 -3.000 -0.1309 0.01030 0.00341 -0.0400 0.9292 0.0047 -2.750 -0.1080 0.01011 0.00315 -0.0389 0.9247 0.0052 -2.500 -0.0844 0.00970 0.00285 -0.0380 0.9207 0.0338 -2.250 -0.0620 0.00902 0.00260 -0.0371 0.9172 0.1421 -2.000 -0.0483 0.00790 0.00241 -0.0348 0.9119 0.3853 -1.750 -0.0366 0.00690 0.00223 -0.0317 0.9063 0.6046 -1.500 -0.0176 0.00633 0.00207 -0.0297 0.9026 0.7263 -1.250 0.0029 0.00609 0.00221 -0.0276 0.8965 0.8312 -1.000 0.0301 0.00607 0.00223 -0.0271 0.8917 0.8690 -0.750 0.0556 0.00606 0.00220 -0.0264 0.8861 0.8877 -0.500 0.0818 0.00610 0.00223 -0.0257 0.8792 0.9041 -0.250 0.1081 0.00615 0.00226 -0.0250 0.8720 0.9180 0.000 0.1337 0.00617 0.00225 -0.0243 0.8634 0.9274 0.250 0.1623 0.00620 0.00226 -0.0243 0.8526 0.9324 0.500 0.1902 0.00621 0.00224 -0.0241 0.8394 0.9377 0.750 0.2172 0.00621 0.00219 -0.0237 0.8222 0.9434 1.000 0.2511 0.00628 0.00216 -0.0247 0.7970 0.9470 1.250 0.2810 0.00640 0.00214 -0.0250 0.7636 0.9513 1.500 0.3041 0.00658 0.00214 -0.0238 0.7252 0.9563 1.750 0.3340 0.00680 0.00219 -0.0243 0.6819 0.9579 2.000 0.3617 0.00706 0.00226 -0.0244 0.6360 0.9598 2.250 0.3882 0.00734 0.00234 -0.0243 0.5889 0.9618 2.500 0.4127 0.00762 0.00243 -0.0237 0.5410 0.9645 2.750 0.4293 0.00787 0.00252 -0.0215 0.5008 0.9690 3.000 0.4582 0.00817 0.00267 -0.0220 0.4527 0.9700 3.250 0.4865 0.00851 0.00281 -0.0225 0.4042 0.9711 3.500 0.5143 0.00882 0.00297 -0.0229 0.3588 0.9724 3.750 0.5413 0.00914 0.00313 -0.0231 0.3166 0.9738 4.000 0.5674 0.00951 0.00332 -0.0232 0.2713 0.9755 4.250 0.5928 0.00983 0.00353 -0.0230 0.2353 0.9774 4.500 0.6162 0.01018 0.00375 -0.0224 0.1991 0.9798 4.750 0.6393 0.01052 0.00398 -0.0218 0.1673 0.9821 5.000 0.6669 0.01094 0.00425 -0.0222 0.1300 0.9830 5.250 0.6937 0.01142 0.00455 -0.0226 0.0934 0.9841 5.500 0.7206 0.01184 0.00487 -0.0228 0.0691 0.9854 5.750 0.7476 0.01220 0.00525 -0.0231 0.0531 0.9867 6.000 0.7744 0.01259 0.00561 -0.0233 0.0403 0.9883 6.250 0.8003 0.01302 0.00602 -0.0233 0.0289 0.9901 6.500 0.8249 0.01350 0.00645 -0.0231 0.0182 0.9919 6.750 0.8492 0.01396 0.00691 -0.0228 0.0132 0.9936 7.000 0.8759 0.01436 0.00736 -0.0231 0.0103 0.9948 7.250 0.9021 0.01487 0.00788 -0.0232 0.0061 0.9963 7.500 0.9273 0.01549 0.00853 -0.0232 0.0034 0.9979 7.750 0.9528 0.01617 0.00931 -0.0232 0.0026 0.9995 8.000 0.9697 0.01681 0.01011 -0.0214 0.0021 1.0000 8.250 0.9817 0.01740 0.01081 -0.0185 0.0020 1.0000 8.500 0.9929 0.01802 0.01154 -0.0155 0.0019 1.0000 8.750 1.0024 0.01877 0.01241 -0.0123 0.0018 1.0000 9.000 1.0117 0.01955 0.01332 -0.0090 0.0017 1.0000 9.250 1.0192 0.02054 0.01446 -0.0055 0.0016 1.0000 9.500 1.0262 0.02162 0.01569 -0.0020 0.0016 1.0000 9.750 1.0321 0.02288 0.01714 0.0016 0.0016 1.0000 10.000 1.0386 0.02395 0.01835 0.0049 0.0016 1.0000 10.250 1.0418 0.02532 0.01992 0.0087 0.0015 1.0000 10.500 1.0401 0.02731 0.02216 0.0130 0.0015 1.0000 10.750 1.0447 0.02866 0.02368 0.0160 0.0015 1.0000 11.000 1.0396 0.03100 0.02631 0.0200 0.0015 1.0000 11.250 1.0408 0.03266 0.02815 0.0228 0.0015 1.0000 11.500 1.0321 0.03530 0.03106 0.0263 0.0015 1.0000 11.750 1.0293 0.03734 0.03329 0.0288 0.0015 1.0000 12.000 1.0166 0.04047 0.03666 0.0313 0.0015 1.0000 12.250 1.0023 0.04397 0.04040 0.0330 0.0015 1.0000 12.500 0.9929 0.04722 0.04386 0.0336 0.0015 1.0000 12.750 0.9740 0.05215 0.04901 0.0329 0.0015 1.0000 13.000 0.9556 0.05787 0.05489 0.0306 0.0015 1.0000 13.250 0.9424 0.06372 0.06089 0.0272 0.0015 1.0000 13.500 0.9293 0.07044 0.06776 0.0227 0.0015 1.0000 13.750 0.9121 0.07901 0.07647 0.0171 0.0015 1.0000 14.000 0.9005 0.08668 0.08425 0.0124 0.0016 1.0000 14.250 0.8760 0.09773 0.09540 0.0062 0.0016 1.0000 14.500 0.8597 0.10659 0.10432 0.0019 0.0016 1.0000 14.750 0.8319 0.11857 0.11636 -0.0037 0.0016 1.0000