XFOIL Version 6.96 Calculated polar for: NACA M3 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -15.750 -0.8710 0.12388 0.12132 0.0042 1.0000 0.0250 -15.500 -1.0296 0.08375 0.08067 -0.0219 1.0000 0.0232 -15.250 -1.0697 0.07282 0.06947 -0.0292 1.0000 0.0231 -15.000 -1.0957 0.06531 0.06174 -0.0336 1.0000 0.0231 -14.750 -1.1142 0.05954 0.05578 -0.0365 1.0000 0.0232 -14.500 -1.1290 0.05481 0.05085 -0.0383 1.0000 0.0234 -14.250 -1.1411 0.05079 0.04664 -0.0391 1.0000 0.0236 -14.000 -1.1512 0.04732 0.04299 -0.0391 1.0000 0.0239 -13.750 -1.1592 0.04441 0.03987 -0.0384 1.0000 0.0242 -13.500 -1.1653 0.04194 0.03720 -0.0370 1.0000 0.0246 -13.250 -1.1697 0.03996 0.03501 -0.0351 1.0000 0.0249 -13.000 -1.1725 0.03854 0.03338 -0.0325 1.0000 0.0252 -12.750 -1.1779 0.03616 0.03077 -0.0294 1.0000 0.0256 -12.500 -1.1708 0.03388 0.02841 -0.0277 1.0000 0.0262 -12.250 -1.1615 0.03269 0.02718 -0.0257 1.0000 0.0266 -12.000 -1.1505 0.03160 0.02600 -0.0239 1.0000 0.0271 -11.750 -1.1371 0.03054 0.02485 -0.0224 1.0000 0.0277 -11.500 -1.1227 0.02946 0.02367 -0.0209 1.0000 0.0283 -11.250 -1.1075 0.02845 0.02254 -0.0194 1.0000 0.0290 -11.000 -1.0914 0.02756 0.02151 -0.0180 1.0000 0.0297 -10.750 -1.0745 0.02690 0.02069 -0.0165 1.0000 0.0302 -10.500 -1.0578 0.02510 0.01874 -0.0153 1.0000 0.0309 -10.250 -1.0393 0.02365 0.01727 -0.0143 1.0000 0.0316 -10.000 -1.0202 0.02277 0.01637 -0.0132 1.0000 0.0323 -9.750 -1.0007 0.02206 0.01561 -0.0121 1.0000 0.0331 -9.500 -0.9809 0.02137 0.01488 -0.0109 1.0000 0.0340 -9.250 -0.9611 0.02068 0.01412 -0.0097 1.0000 0.0347 -9.000 -0.9414 0.01999 0.01337 -0.0084 1.0000 0.0354 -8.750 -0.9218 0.01940 0.01270 -0.0070 1.0000 0.0359 -8.500 -0.9034 0.01866 0.01190 -0.0054 1.0000 0.0365 -8.250 -0.8885 0.01755 0.01077 -0.0033 1.0000 0.0376 -8.000 -0.8711 0.01691 0.01013 -0.0016 1.0000 0.0385 -7.750 -0.8533 0.01637 0.00957 0.0002 1.0000 0.0393 -7.500 -0.8354 0.01588 0.00905 0.0020 1.0000 0.0402 -7.250 -0.8175 0.01542 0.00856 0.0038 1.0000 0.0411 -7.000 -0.7992 0.01502 0.00812 0.0055 1.0000 0.0421 -6.750 -0.7805 0.01468 0.00773 0.0072 1.0000 0.0429 -6.500 -0.7641 0.01408 0.00711 0.0092 1.0000 0.0442 -6.250 -0.7463 0.01360 0.00663 0.0110 1.0000 0.0457 -6.000 -0.7272 0.01326 0.00628 0.0126 1.0000 0.0473 -5.750 -0.7075 0.01297 0.00596 0.0140 1.0000 0.0492 -5.500 -0.6743 0.01258 0.00556 0.0126 0.9982 0.0522 -5.250 -0.6389 0.01216 0.00519 0.0108 0.9958 0.0586 -5.000 -0.6033 0.01163 0.00478 0.0088 0.9938 0.0775 -4.750 -0.5706 0.01098 0.00440 0.0074 0.9905 0.1234 -4.500 -0.5363 0.01043 0.00410 0.0055 0.9873 0.1721 -4.250 -0.5005 0.00992 0.00384 0.0035 0.9847 0.2260 -4.000 -0.4638 0.00942 0.00361 0.0012 0.9828 0.2850 -3.750 -0.4322 0.00899 0.00340 0.0001 0.9778 0.3375 -3.500 -0.3969 0.00858 0.00321 -0.0017 0.9745 0.3910 -3.250 -0.3604 0.00817 0.00304 -0.0038 0.9719 0.4502 -3.000 -0.3258 0.00783 0.00289 -0.0053 0.9684 0.5003 -2.750 -0.2968 0.00750 0.00277 -0.0056 0.9614 0.5501 -2.500 -0.2645 0.00722 0.00264 -0.0064 0.9566 0.5926 -2.250 -0.2375 0.00701 0.00256 -0.0060 0.9481 0.6312 -2.000 -0.2089 0.00679 0.00247 -0.0059 0.9409 0.6668 -1.750 -0.1837 0.00663 0.00242 -0.0050 0.9303 0.7007 -1.500 -0.1575 0.00649 0.00236 -0.0043 0.9205 0.7300 -1.250 -0.1314 0.00638 0.00231 -0.0035 0.9095 0.7521 -1.000 -0.1054 0.00630 0.00227 -0.0028 0.8974 0.7726 -0.750 -0.0791 0.00624 0.00224 -0.0021 0.8854 0.7928 -0.500 -0.0528 0.00619 0.00222 -0.0014 0.8730 0.8117 -0.250 -0.0265 0.00617 0.00220 -0.0007 0.8595 0.8288 0.000 0.0000 0.00616 0.00220 0.0000 0.8446 0.8446 0.250 0.0264 0.00617 0.00220 0.0007 0.8288 0.8595 0.500 0.0528 0.00619 0.00222 0.0014 0.8117 0.8729 0.750 0.0791 0.00624 0.00224 0.0021 0.7928 0.8854 1.000 0.1054 0.00630 0.00227 0.0028 0.7726 0.8974 1.250 0.1314 0.00638 0.00231 0.0035 0.7521 0.9096 1.500 0.1574 0.00649 0.00236 0.0043 0.7299 0.9205 1.750 0.1837 0.00663 0.00242 0.0050 0.7008 0.9303 2.000 0.2089 0.00679 0.00247 0.0059 0.6670 0.9409 2.250 0.2375 0.00701 0.00256 0.0060 0.6311 0.9481 2.500 0.2645 0.00722 0.00264 0.0064 0.5925 0.9566 2.750 0.2968 0.00750 0.00277 0.0056 0.5499 0.9615 3.000 0.3258 0.00783 0.00289 0.0053 0.4999 0.9685 3.250 0.3605 0.00817 0.00304 0.0038 0.4502 0.9719 3.500 0.3969 0.00858 0.00321 0.0017 0.3910 0.9745 3.750 0.4322 0.00899 0.00340 -0.0001 0.3374 0.9779 4.000 0.4639 0.00942 0.00361 -0.0012 0.2850 0.9828 4.250 0.5006 0.00992 0.00384 -0.0035 0.2261 0.9847 4.500 0.5364 0.01043 0.00410 -0.0056 0.1721 0.9873 4.750 0.5707 0.01098 0.00439 -0.0074 0.1234 0.9906 5.000 0.6034 0.01162 0.00478 -0.0088 0.0775 0.9939 5.250 0.6390 0.01215 0.00518 -0.0108 0.0586 0.9959 5.500 0.6744 0.01258 0.00556 -0.0126 0.0523 0.9982 5.750 0.7073 0.01296 0.00596 -0.0140 0.0492 1.0000 6.000 0.7271 0.01325 0.00627 -0.0125 0.0474 1.0000 6.250 0.7462 0.01360 0.00663 -0.0110 0.0457 1.0000 6.500 0.7640 0.01407 0.00710 -0.0092 0.0442 1.0000 6.750 0.7804 0.01468 0.00773 -0.0072 0.0429 1.0000 7.000 0.7991 0.01502 0.00812 -0.0055 0.0421 1.0000 7.250 0.8174 0.01542 0.00855 -0.0038 0.0411 1.0000 7.500 0.8353 0.01588 0.00905 -0.0020 0.0402 1.0000 7.750 0.8532 0.01637 0.00957 -0.0002 0.0393 1.0000 8.000 0.8710 0.01691 0.01013 0.0016 0.0385 1.0000 8.250 0.8884 0.01754 0.01077 0.0034 0.0376 1.0000 8.500 0.9033 0.01867 0.01190 0.0054 0.0365 1.0000 8.750 0.9218 0.01940 0.01269 0.0070 0.0359 1.0000 9.000 0.9415 0.01999 0.01337 0.0084 0.0354 1.0000 9.250 0.9612 0.02067 0.01411 0.0097 0.0347 1.0000 9.500 0.9810 0.02137 0.01488 0.0109 0.0340 1.0000 9.750 1.0008 0.02206 0.01561 0.0120 0.0331 1.0000 10.000 1.0204 0.02277 0.01637 0.0131 0.0323 1.0000 10.250 1.0395 0.02365 0.01727 0.0142 0.0316 1.0000 10.500 1.0580 0.02511 0.01875 0.0152 0.0309 1.0000 10.750 1.0747 0.02689 0.02068 0.0165 0.0302 1.0000 11.000 1.0917 0.02757 0.02151 0.0179 0.0297 1.0000 11.250 1.1078 0.02844 0.02253 0.0194 0.0289 1.0000 11.500 1.1231 0.02946 0.02367 0.0208 0.0282 1.0000 11.750 1.1375 0.03054 0.02485 0.0223 0.0276 1.0000 12.000 1.1509 0.03160 0.02600 0.0239 0.0271 1.0000 12.250 1.1621 0.03269 0.02717 0.0256 0.0266 1.0000 12.500 1.1716 0.03388 0.02841 0.0276 0.0262 1.0000 12.750 1.1784 0.03625 0.03086 0.0293 0.0256 1.0000 13.000 1.1732 0.03852 0.03337 0.0324 0.0252 1.0000 13.250 1.1703 0.03998 0.03503 0.0350 0.0249 1.0000 13.500 1.1661 0.04196 0.03722 0.0369 0.0246 1.0000 13.750 1.1600 0.04442 0.03989 0.0382 0.0242 1.0000 14.000 1.1521 0.04735 0.04301 0.0389 0.0239 1.0000 14.250 1.1422 0.05079 0.04665 0.0389 0.0236 1.0000 14.500 1.1305 0.05477 0.05082 0.0381 0.0234 1.0000 14.750 1.1162 0.05946 0.05569 0.0363 0.0232 1.0000 15.000 1.0980 0.06518 0.06160 0.0335 0.0231 1.0000 15.250 1.0723 0.07266 0.06930 0.0290 0.0230 1.0000 15.500 1.0308 0.08385 0.08078 0.0215 0.0232 1.0000