XFOIL Version 6.96 Calculated polar for: Rhode St. Genese 34 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.500 -0.4110 0.17882 0.17688 -0.0211 1.0000 0.0138 -19.250 -0.4024 0.17639 0.17445 -0.0223 1.0000 0.0140 -16.750 -0.8722 0.03375 0.03065 -0.1255 0.9515 0.0234 -16.500 -0.8274 0.02952 0.02613 -0.1380 0.9310 0.0235 -16.250 -0.7985 0.02739 0.02367 -0.1430 0.8847 0.0237 -16.000 -0.8021 0.02622 0.02228 -0.1399 0.8589 0.0238 -15.750 -0.8058 0.02514 0.02103 -0.1361 0.8467 0.0238 -15.500 -0.8038 0.02433 0.02010 -0.1327 0.8384 0.0240 -15.250 -0.7953 0.02348 0.01912 -0.1303 0.8324 0.0241 -15.000 -0.7843 0.02261 0.01815 -0.1281 0.8278 0.0242 -14.750 -0.7712 0.02179 0.01722 -0.1262 0.8237 0.0243 -14.500 -0.7557 0.02110 0.01642 -0.1244 0.8201 0.0244 -14.250 -0.7386 0.02047 0.01569 -0.1228 0.8166 0.0246 -14.000 -0.7208 0.01981 0.01493 -0.1213 0.8136 0.0248 -13.750 -0.7023 0.01916 0.01420 -0.1199 0.8097 0.0249 -13.500 -0.6828 0.01857 0.01351 -0.1185 0.8058 0.0250 -13.250 -0.6630 0.01803 0.01286 -0.1171 0.8007 0.0251 -13.000 -0.6424 0.01750 0.01223 -0.1159 0.7971 0.0252 -12.750 -0.6206 0.01698 0.01164 -0.1148 0.7947 0.0253 -12.500 -0.5983 0.01650 0.01109 -0.1137 0.7918 0.0254 -12.250 -0.5770 0.01591 0.01043 -0.1125 0.7883 0.0255 -12.000 -0.5555 0.01536 0.00981 -0.1113 0.7843 0.0257 -11.750 -0.5330 0.01489 0.00927 -0.1102 0.7809 0.0259 -11.500 -0.5094 0.01447 0.00880 -0.1093 0.7781 0.0261 -11.250 -0.4851 0.01409 0.00839 -0.1085 0.7751 0.0263 -11.000 -0.4606 0.01374 0.00800 -0.1076 0.7713 0.0265 -10.750 -0.4359 0.01342 0.00764 -0.1068 0.7675 0.0267 -10.500 -0.4110 0.01312 0.00729 -0.1060 0.7637 0.0270 -10.250 -0.3858 0.01281 0.00695 -0.1053 0.7596 0.0272 -10.000 -0.3605 0.01252 0.00661 -0.1046 0.7530 0.0274 -9.750 -0.3355 0.01224 0.00628 -0.1038 0.7469 0.0276 -9.500 -0.3098 0.01197 0.00596 -0.1031 0.7414 0.0279 -9.250 -0.2842 0.01171 0.00566 -0.1024 0.7335 0.0282 -9.000 -0.2587 0.01147 0.00536 -0.1016 0.7255 0.0284 -8.750 -0.2332 0.01125 0.00508 -0.1009 0.7140 0.0287 -8.500 -0.2082 0.01107 0.00482 -0.1000 0.6967 0.0289 -8.250 -0.1836 0.01095 0.00459 -0.0991 0.6747 0.0291 -8.000 -0.1599 0.01075 0.00429 -0.0980 0.6534 0.0296 -7.750 -0.1358 0.01064 0.00408 -0.0970 0.6324 0.0300 -7.500 -0.1113 0.01054 0.00390 -0.0961 0.6136 0.0304 -7.250 -0.0860 0.01044 0.00373 -0.0954 0.5996 0.0308 -7.000 -0.0606 0.01035 0.00358 -0.0946 0.5864 0.0312 -6.750 -0.0350 0.01026 0.00343 -0.0939 0.5717 0.0317 -6.500 -0.0097 0.01020 0.00329 -0.0932 0.5534 0.0322 -6.250 0.0150 0.01018 0.00316 -0.0923 0.5270 0.0327 -6.000 0.0343 0.01048 0.00312 -0.0905 0.4478 0.0331 -5.750 0.0567 0.01059 0.00306 -0.0893 0.4065 0.0336 -5.500 0.0809 0.01061 0.00299 -0.0884 0.3835 0.0344 -5.250 0.1059 0.01061 0.00292 -0.0877 0.3680 0.0352 -4.750 0.1573 0.01058 0.00279 -0.0864 0.3480 0.0372 -4.500 0.1830 0.01055 0.00273 -0.0858 0.3405 0.0384 -4.250 0.2090 0.01052 0.00268 -0.0852 0.3347 0.0399 -4.000 0.2353 0.01048 0.00264 -0.0847 0.3305 0.0414 -3.750 0.2614 0.01046 0.00259 -0.0842 0.3260 0.0429 -3.500 0.2872 0.01045 0.00256 -0.0837 0.3214 0.0449 -3.250 0.3131 0.01045 0.00255 -0.0831 0.3165 0.0471 -3.000 0.3395 0.01042 0.00252 -0.0827 0.3137 0.0492 -2.750 0.3654 0.01041 0.00251 -0.0822 0.3097 0.0519 -2.500 0.3915 0.01042 0.00250 -0.0817 0.3068 0.0545 -2.250 0.4172 0.01042 0.00250 -0.0811 0.3042 0.0579 -2.000 0.4430 0.01043 0.00251 -0.0806 0.3014 0.0608 -1.750 0.4687 0.01044 0.00252 -0.0801 0.2987 0.0647 -1.500 0.4949 0.01043 0.00252 -0.0797 0.2973 0.0688 -1.250 0.5207 0.01041 0.00252 -0.0792 0.2954 0.0755 -1.000 0.5454 0.01030 0.00256 -0.0786 0.2938 0.1223 -0.750 0.5710 0.01031 0.00261 -0.0781 0.2922 0.1409 -0.500 0.5966 0.01034 0.00266 -0.0776 0.2903 0.1489 -0.250 0.6221 0.01038 0.00271 -0.0771 0.2886 0.1549 0.000 0.6474 0.01044 0.00276 -0.0765 0.2867 0.1598 0.250 0.6724 0.01049 0.00282 -0.0760 0.2849 0.1654 0.500 0.6971 0.01056 0.00290 -0.0754 0.2828 0.1714 0.750 0.7218 0.01060 0.00297 -0.0747 0.2813 0.1819 1.000 0.7465 0.01058 0.00304 -0.0742 0.2804 0.2093 1.250 0.7667 0.01019 0.00315 -0.0729 0.2784 0.4098 1.500 0.7719 0.00927 0.00332 -0.0684 0.2765 0.8010 1.750 0.8778 0.00932 0.00370 -0.0855 0.2715 0.9876 2.000 0.9112 0.00949 0.00383 -0.0869 0.2690 0.9966 2.250 0.9485 0.00968 0.00397 -0.0892 0.2651 0.9999 2.500 0.9713 0.00978 0.00406 -0.0882 0.2633 1.0000 2.750 0.9925 0.00989 0.00416 -0.0870 0.2613 1.0000 3.000 1.0136 0.01000 0.00427 -0.0857 0.2591 1.0000 3.250 1.0342 0.01014 0.00438 -0.0844 0.2557 1.0000 3.500 1.0541 0.01030 0.00451 -0.0830 0.2516 1.0000 3.750 1.0747 0.01045 0.00464 -0.0817 0.2487 1.0000 4.000 1.0955 0.01059 0.00478 -0.0805 0.2450 1.0000 4.250 1.1152 0.01076 0.00492 -0.0790 0.2397 1.0000 4.500 1.1318 0.01096 0.00508 -0.0770 0.2326 1.0000 4.750 1.1467 0.01122 0.00527 -0.0747 0.2211 1.0000 5.000 1.1377 0.01242 0.00607 -0.0683 0.1543 1.0000 5.250 1.1454 0.01314 0.00665 -0.0650 0.1304 1.0000 5.500 1.1619 0.01351 0.00699 -0.0633 0.1234 1.0000 5.750 1.1785 0.01390 0.00735 -0.0617 0.1178 1.0000 6.000 1.1968 0.01422 0.00767 -0.0604 0.1144 1.0000 6.250 1.2150 0.01457 0.00801 -0.0591 0.1115 1.0000 6.500 1.2323 0.01497 0.00840 -0.0578 0.1080 1.0000 6.750 1.2498 0.01538 0.00880 -0.0565 0.1042 1.0000 7.000 1.2682 0.01576 0.00918 -0.0555 0.1014 1.0000 7.250 1.2853 0.01623 0.00964 -0.0543 0.0973 1.0000 7.500 1.3015 0.01675 0.01014 -0.0530 0.0925 1.0000 7.750 1.3085 0.01783 0.01105 -0.0508 0.0626 1.0000 8.000 1.3192 0.01874 0.01193 -0.0490 0.0542 1.0000 8.250 1.3341 0.01942 0.01262 -0.0479 0.0521 1.0000 8.500 1.3483 0.02015 0.01337 -0.0467 0.0505 1.0000 8.750 1.3625 0.02091 0.01415 -0.0456 0.0491 1.0000 9.000 1.3777 0.02162 0.01489 -0.0447 0.0483 1.0000 9.250 1.3926 0.02236 0.01567 -0.0438 0.0477 1.0000 9.500 1.4067 0.02316 0.01650 -0.0429 0.0471 1.0000 9.750 1.4202 0.02403 0.01741 -0.0420 0.0465 1.0000 10.000 1.4328 0.02497 0.01838 -0.0411 0.0458 1.0000 10.250 1.4448 0.02597 0.01942 -0.0401 0.0452 1.0000 10.500 1.4549 0.02712 0.02061 -0.0391 0.0445 1.0000 10.750 1.4640 0.02838 0.02190 -0.0381 0.0436 1.0000 11.000 1.4723 0.02973 0.02329 -0.0371 0.0428 1.0000 11.250 1.4829 0.03091 0.02453 -0.0364 0.0424 1.0000 11.500 1.4937 0.03212 0.02578 -0.0357 0.0418 1.0000 11.750 1.5025 0.03351 0.02723 -0.0350 0.0412 1.0000 12.000 1.5102 0.03506 0.02883 -0.0344 0.0407 1.0000 12.250 1.5171 0.03671 0.03053 -0.0338 0.0400 1.0000 12.500 1.5225 0.03855 0.03242 -0.0332 0.0394 1.0000 12.750 1.5270 0.04056 0.03449 -0.0327 0.0389 1.0000 13.000 1.5301 0.04279 0.03678 -0.0324 0.0385 1.0000 13.250 1.5310 0.04532 0.03938 -0.0321 0.0379 1.0000 13.500 1.5330 0.04779 0.04192 -0.0319 0.0374 1.0000 13.750 1.5349 0.05034 0.04454 -0.0319 0.0371 1.0000 14.000 1.5359 0.05304 0.04732 -0.0319 0.0368 1.0000 14.250 1.5357 0.05592 0.05028 -0.0321 0.0363 1.0000 14.500 1.5334 0.05909 0.05353 -0.0323 0.0360 1.0000 14.750 1.5291 0.06259 0.05713 -0.0326 0.0355 1.0000 15.000 1.5241 0.06626 0.06087 -0.0331 0.0350 1.0000 15.250 1.5166 0.07031 0.06501 -0.0336 0.0348 1.0000 15.500 1.5069 0.07476 0.06956 -0.0344 0.0345 1.0000 15.750 1.4963 0.07940 0.07429 -0.0353 0.0339 1.0000 16.000 1.4852 0.08416 0.07915 -0.0363 0.0336 1.0000 16.250 1.4727 0.08911 0.08418 -0.0374 0.0331 1.0000