XFOIL Version 6.96 Calculated polar for: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN 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 ------ -------- --------- --------- -------- -------- -------- -13.250 -0.1284 0.08514 0.08278 -0.0856 -0.0013 4.4329 -13.000 -0.1305 0.07769 0.07533 -0.0879 -0.0012 4.4216 -12.750 -0.1293 0.07284 0.07048 -0.0898 -0.0011 4.4216 -12.500 -0.1271 0.06908 0.06672 -0.0916 -0.0010 4.4210 -12.250 -0.1288 0.06444 0.06209 -0.0937 -0.0009 4.4209 -12.000 -0.1325 0.05940 0.05706 -0.0965 -0.0008 4.4207 -11.750 -0.1410 0.05352 0.05119 -0.1000 -0.0007 4.4205 -11.500 -0.1657 0.04371 0.04134 -0.1069 -0.0006 4.4195 -11.250 -0.1916 0.03867 0.03617 -0.1118 -0.0004 4.4190 -11.000 -0.2164 0.03525 0.03262 -0.1146 -0.0003 4.4184 -10.750 -0.2390 0.03261 0.02983 -0.1157 -0.0002 4.4182 -10.500 -0.2614 0.03047 0.02753 -0.1155 -0.0001 4.4181 -10.250 -0.2767 0.02848 0.02535 -0.1146 0.0000 4.4183 -10.000 -0.2834 0.02609 0.02271 -0.1137 0.0000 4.4185 -9.750 -0.2844 0.02398 0.02036 -0.1125 0.0000 4.4189 -9.500 -0.2809 0.02212 0.01826 -0.1112 -0.0001 4.4193 -9.250 -0.2736 0.02038 0.01627 -0.1099 -0.0002 4.4194 -9.000 -0.2625 0.01894 0.01459 -0.1088 -0.0002 4.4200 -8.750 -0.2487 0.01796 0.01331 -0.1077 -0.0003 4.4218 -8.500 -0.2346 0.01642 0.01152 -0.1068 -0.0004 4.4234 -8.250 -0.2169 0.01554 0.01063 -0.1063 -0.0004 4.4250 -8.000 -0.1984 0.01466 0.00962 -0.1056 -0.0004 4.4263 -7.750 -0.1788 0.01371 0.00852 -0.1049 -0.0004 4.4264 -7.500 -0.1583 0.01280 0.00747 -0.1043 -0.0004 4.4254 -7.250 -0.1507 0.01249 0.00710 -0.1017 -0.0004 4.4248 -7.000 -0.1358 0.01200 0.00652 -0.1002 -0.0001 4.4242 -6.750 -0.1172 0.01149 0.00593 -0.0992 0.0001 4.4237 -6.500 -0.0971 0.01100 0.00539 -0.0985 0.0002 4.4233 -6.250 -0.0764 0.01052 0.00487 -0.0980 0.0004 4.4231 -6.000 -0.0555 0.01008 0.00440 -0.0974 0.0006 4.4229 -5.750 -0.0347 0.00966 0.00395 -0.0969 0.0007 4.4228 -5.500 -0.0421 0.00988 0.00420 -0.0921 0.0039 4.4227 -5.250 -0.0234 0.00952 0.00383 -0.0913 0.0046 4.4227 -5.000 -0.0032 0.00915 0.00345 -0.0906 0.0051 4.4227 -4.750 0.0177 0.00881 0.00309 -0.0901 0.0055 4.4227 -4.500 0.0395 0.00848 0.00274 -0.0897 0.0058 4.4229 -4.250 0.0623 0.00818 0.00240 -0.0894 0.0061 4.4232 -4.000 0.0855 0.00792 0.00210 -0.0891 0.0064 4.4236 -3.750 0.1091 0.00768 0.00182 -0.0889 0.0066 4.4243 -3.500 0.0561 0.00852 0.00274 -0.0771 0.0225 4.4239 -3.250 0.0762 0.00832 0.00251 -0.0763 0.0238 4.4246 -3.000 0.0977 0.00813 0.00229 -0.0757 0.0247 4.4257 -2.750 0.1199 0.00794 0.00207 -0.0752 0.0254 4.4275 -2.500 0.1425 0.00777 0.00187 -0.0748 0.0260 4.4308 -2.250 0.1574 0.00667 0.00175 -0.0742 0.0266 3.8027 -2.000 0.1702 0.00583 0.00179 -0.0731 0.0271 2.8935 -1.750 0.2135 0.00638 0.00272 -0.0739 0.0270 2.3156 -1.500 0.2440 0.00663 0.00294 -0.0739 0.0272 2.2368 -1.250 0.2001 0.00763 0.00402 -0.0640 0.0467 2.2335 -1.000 0.2267 0.00775 0.00411 -0.0637 0.0485 2.2181 -0.750 0.2510 0.00772 0.00404 -0.0633 0.0500 2.2065 -0.500 0.2761 0.00763 0.00392 -0.0630 0.0511 2.1904 -0.250 0.2987 0.00750 0.00375 -0.0626 0.0523 2.1587 0.000 0.3026 0.00776 0.00402 -0.0593 0.0651 2.1522 0.250 0.3286 0.00766 0.00390 -0.0590 0.0670 2.1450 0.500 0.3547 0.00756 0.00378 -0.0588 0.0685 2.1365 0.750 0.3807 0.00744 0.00365 -0.0587 0.0698 2.1265 1.000 0.4062 0.00731 0.00351 -0.0585 0.0710 2.1158 1.250 0.4081 0.00761 0.00383 -0.0551 0.0868 2.1026 1.500 0.4310 0.00746 0.00367 -0.0546 0.0893 2.0905 1.750 0.4545 0.00728 0.00349 -0.0543 0.0914 2.0781 2.000 0.4765 0.00714 0.00334 -0.0537 0.0957 2.0689 2.250 0.4874 0.00718 0.00340 -0.0515 0.1114 2.0640 2.500 0.5143 0.00691 0.00313 -0.0515 0.1152 2.0591 2.750 0.5423 0.00663 0.00284 -0.0517 0.1182 2.0538 3.000 0.5709 0.00634 0.00256 -0.0520 0.1217 2.0482 3.250 0.5789 0.00645 0.00268 -0.0494 0.1429 2.0410 3.500 0.6099 0.00612 0.00236 -0.0500 0.1477 2.0345 3.750 0.6165 0.00629 0.00257 -0.0473 0.1703 2.0265 4.000 0.6418 0.00610 0.00239 -0.0472 0.1785 2.0199 4.250 0.6462 0.00632 0.00265 -0.0443 0.2056 2.0130 4.500 0.6574 0.00641 0.00277 -0.0423 0.2302 2.0069 4.750 0.6794 0.00629 0.00266 -0.0417 0.2474 2.0019 5.000 0.6917 0.00620 0.00258 -0.0400 0.2758 2.0009 5.250 0.7098 0.00596 0.00234 -0.0391 0.2993 2.0009 5.500 0.7304 0.00570 0.00205 -0.0386 0.3231 2.0009 5.750 0.7535 0.00529 0.00144 -0.0381 0.4380 2.0009 6.000 0.7508 0.00540 0.00138 -0.0344 0.5790 2.0009 6.250 0.7345 0.00574 0.00151 -0.0291 0.7663 2.0009 6.500 0.7133 0.00623 0.00176 -0.0234 0.9876 2.0009 6.750 0.6974 0.00669 0.00203 -0.0186 1.2090 2.0009 7.000 0.6830 0.00718 0.00233 -0.0141 1.4337 2.0009 7.250 0.6666 0.00775 0.00267 -0.0096 1.7404 2.0009 7.500 0.6521 0.00835 0.00300 -0.0055 2.1047 2.0009 7.750 0.6337 0.00913 0.00340 -0.0013 2.6718 2.0009 8.000 0.6121 0.01008 0.00393 0.0029 3.5291 2.0009 8.250 0.6038 0.01069 0.00437 0.0060 4.2725 2.0009 8.500 0.6088 0.01083 0.00457 0.0079 4.2872 2.0009 8.750 0.6141 0.01097 0.00476 0.0098 4.2941 2.0009 9.000 0.6188 0.01113 0.00499 0.0116 4.2996 2.0009 9.250 0.6231 0.01131 0.00523 0.0135 4.3029 2.0009 9.500 0.6270 0.01150 0.00549 0.0154 4.3058 2.0009 9.750 0.6297 0.01174 0.00580 0.0173 4.3077 2.0009 10.000 0.6329 0.01196 0.00610 0.0191 4.3086 2.0009 10.250 0.6353 0.01222 0.00643 0.0209 4.3094 2.0009 10.500 0.6379 0.01247 0.00675 0.0227 4.3097 2.0009 10.750 0.6392 0.01278 0.00713 0.0245 4.3108 2.0009 11.000 0.6405 0.01310 0.00753 0.0262 4.3109 2.0009 11.250 0.6409 0.01346 0.00796 0.0280 4.3111 2.0009 11.500 0.6406 0.01385 0.00842 0.0296 4.3114 2.0009 11.750 0.6398 0.01429 0.00894 0.0313 4.3115 2.0009 12.000 0.6377 0.01479 0.00950 0.0329 4.3118 2.0009 12.250 0.6356 0.01531 0.01009 0.0344 4.3120 2.0009 12.500 0.6329 0.01585 0.01071 0.0358 4.3120 2.0009 12.750 0.6295 0.01646 0.01139 0.0372 4.3121 2.0009 13.000 0.6260 0.01709 0.01209 0.0385 4.3120 2.0009 13.250 0.6230 0.01773 0.01280 0.0397 4.3120 2.0009 13.500 0.6194 0.01838 0.01352 0.0408 4.3120 2.0009 13.750 0.6158 0.01908 0.01429 0.0419 4.3117 2.0009 14.000 0.6123 0.01978 0.01506 0.0429 4.3117 2.0009 14.250 0.6100 0.02044 0.01578 0.0438 4.3115 2.0009 14.500 0.6076 0.02111 0.01651 0.0446 4.3114 2.0009 14.750 0.6062 0.02173 0.01718 0.0454 4.3112 2.0009 15.000 0.6057 0.02230 0.01780 0.0462 4.3110 2.0009 15.250 0.6063 0.02283 0.01838 0.0470 4.3107 2.0009 15.500 0.6076 0.02330 0.01889 0.0478 4.3104 2.0009 15.750 0.6102 0.02369 0.01933 0.0486 4.3102 2.0009 16.000 0.6149 0.02398 0.01965 0.0496 4.3098 2.0009 16.250 0.6215 0.02419 0.01989 0.0505 4.3093 2.0009 16.500 0.6341 0.02415 0.01985 0.0517 4.3085 2.0009 16.750 0.6411 0.02443 0.02017 0.0526 4.3078 2.0009 17.000 0.6401 0.02510 0.02094 0.0530 4.3073 2.0009 17.250 0.6367 0.02588 0.02183 0.0533 4.3064 2.0009 17.500 0.6335 0.02670 0.02276 0.0536 4.3053 2.0009 17.750 0.6264 0.02786 0.02412 0.0536 4.3025 2.0009 18.000 0.6241 0.02878 0.02517 0.0538 4.3001 2.0009 18.250 0.6226 0.02971 0.02623 0.0541 4.2974 2.0009 18.500 0.6192 0.03081 0.02744 0.0542 4.2951 2.0009 18.750 0.6141 0.03201 0.02876 0.0541 4.2938 2.0009 19.000 0.6080 0.03334 0.03020 0.0538 4.2924 2.0009 19.250 0.6015 0.03480 0.03178 0.0534 4.2907 2.0009