XFOIL Version 6.96 Calculated polar for: S1012 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 ------ -------- --------- --------- -------- -------- -------- -18.250 -1.0833 0.10294 0.09955 -0.0179 1.0000 0.0142 -18.000 -1.1205 0.09166 0.08808 -0.0245 1.0000 0.0141 -17.750 -1.1544 0.08113 0.07736 -0.0308 1.0000 0.0140 -17.500 -1.1801 0.07226 0.06831 -0.0363 1.0000 0.0140 -17.250 -1.2013 0.06467 0.06054 -0.0408 1.0000 0.0141 -17.000 -1.2163 0.05866 0.05436 -0.0441 1.0000 0.0142 -16.750 -1.2284 0.05361 0.04917 -0.0464 1.0000 0.0143 -16.500 -1.2364 0.04957 0.04499 -0.0478 1.0000 0.0144 -16.250 -1.2417 0.04619 0.04147 -0.0486 1.0000 0.0146 -16.000 -1.2445 0.04334 0.03850 -0.0488 1.0000 0.0149 -15.750 -1.2459 0.04079 0.03582 -0.0486 1.0000 0.0152 -15.500 -1.2446 0.03864 0.03356 -0.0481 1.0000 0.0155 -15.250 -1.2424 0.03666 0.03144 -0.0474 1.0000 0.0157 -15.000 -1.2409 0.03472 0.02940 -0.0464 1.0000 0.0160 -14.750 -1.2391 0.03288 0.02747 -0.0452 1.0000 0.0163 -14.500 -1.2340 0.03134 0.02586 -0.0441 1.0000 0.0167 -14.250 -1.2276 0.02996 0.02440 -0.0428 1.0000 0.0170 -14.000 -1.2194 0.02874 0.02310 -0.0415 1.0000 0.0175 -13.750 -1.2099 0.02763 0.02191 -0.0402 1.0000 0.0180 -13.500 -1.1992 0.02661 0.02082 -0.0389 1.0000 0.0186 -13.250 -1.1880 0.02565 0.01975 -0.0375 1.0000 0.0192 -13.000 -1.1757 0.02478 0.01879 -0.0361 1.0000 0.0196 -12.750 -1.1655 0.02377 0.01774 -0.0345 1.0000 0.0203 -12.500 -1.1527 0.02294 0.01687 -0.0330 1.0000 0.0210 -12.250 -1.1388 0.02220 0.01607 -0.0316 1.0000 0.0217 -12.000 -1.1240 0.02151 0.01533 -0.0303 1.0000 0.0225 -11.500 -1.0819 0.02015 0.01381 -0.0298 0.9607 0.0244 -11.250 -1.0565 0.01945 0.01306 -0.0304 0.9398 0.0259 -11.000 -1.0388 0.01894 0.01247 -0.0291 0.9232 0.0272 -10.500 -1.0061 0.01808 0.01141 -0.0257 0.9023 0.0296 -10.250 -0.9903 0.01763 0.01090 -0.0238 0.8950 0.0311 -10.000 -0.9721 0.01722 0.01046 -0.0224 0.8890 0.0328 -9.750 -0.9524 0.01686 0.01001 -0.0212 0.8840 0.0345 -9.250 -0.9114 0.01606 0.00913 -0.0191 0.8763 0.0384 -9.000 -0.8896 0.01570 0.00875 -0.0183 0.8728 0.0407 -8.750 -0.8673 0.01539 0.00837 -0.0175 0.8695 0.0426 -8.500 -0.8457 0.01501 0.00797 -0.0166 0.8666 0.0450 -8.000 -0.7997 0.01440 0.00729 -0.0152 0.8617 0.0504 -7.750 -0.7765 0.01407 0.00695 -0.0146 0.8592 0.0534 -7.500 -0.7530 0.01376 0.00665 -0.0140 0.8566 0.0571 -7.250 -0.7289 0.01350 0.00635 -0.0135 0.8541 0.0604 -7.000 -0.7052 0.01321 0.00605 -0.0129 0.8519 0.0641 -6.750 -0.6811 0.01294 0.00578 -0.0123 0.8501 0.0684 -6.500 -0.6563 0.01273 0.00552 -0.0118 0.8484 0.0721 -6.250 -0.6318 0.01244 0.00527 -0.0114 0.8466 0.0774 -6.000 -0.6067 0.01221 0.00504 -0.0110 0.8448 0.0825 -5.750 -0.5815 0.01197 0.00481 -0.0106 0.8430 0.0879 -5.500 -0.5563 0.01174 0.00460 -0.0103 0.8413 0.0948 -5.250 -0.5308 0.01153 0.00440 -0.0099 0.8396 0.1012 -5.000 -0.5054 0.01131 0.00421 -0.0096 0.8378 0.1095 -4.750 -0.4800 0.01109 0.00402 -0.0092 0.8360 0.1185 -4.500 -0.4542 0.01091 0.00384 -0.0089 0.8345 0.1274 -4.250 -0.4286 0.01071 0.00368 -0.0085 0.8332 0.1389 -4.000 -0.4029 0.01050 0.00353 -0.0082 0.8319 0.1528 -3.750 -0.3770 0.01029 0.00339 -0.0080 0.8304 0.1681 -3.500 -0.3511 0.01008 0.00326 -0.0077 0.8289 0.1866 -3.250 -0.3257 0.00983 0.00312 -0.0074 0.8271 0.2106 -3.000 -0.3003 0.00958 0.00300 -0.0071 0.8253 0.2384 -2.750 -0.2754 0.00929 0.00287 -0.0067 0.8238 0.2764 -2.500 -0.2509 0.00897 0.00274 -0.0062 0.8221 0.3226 -2.250 -0.2269 0.00862 0.00260 -0.0057 0.8204 0.3780 -2.000 -0.2044 0.00816 0.00245 -0.0048 0.8188 0.4529 -1.750 -0.1829 0.00765 0.00229 -0.0038 0.8171 0.5414 -1.500 -0.1624 0.00714 0.00225 -0.0024 0.8151 0.6464 -1.250 -0.1370 0.00706 0.00239 -0.0017 0.8129 0.7062 -1.000 -0.1095 0.00706 0.00244 -0.0015 0.8094 0.7288 -0.750 -0.0823 0.00703 0.00237 -0.0010 0.8018 0.7432 -0.500 -0.0553 0.00695 0.00226 -0.0006 0.7885 0.7536 -0.250 -0.0279 0.00692 0.00222 -0.0002 0.7773 0.7616 0.000 0.0000 0.00691 0.00218 0.0000 0.7698 0.7698 0.250 0.0279 0.00692 0.00222 0.0002 0.7618 0.7772 0.500 0.0553 0.00695 0.00226 0.0006 0.7535 0.7885 0.750 0.0822 0.00703 0.00237 0.0010 0.7431 0.8018 1.000 0.1095 0.00706 0.00244 0.0015 0.7290 0.8094 1.250 0.1370 0.00706 0.00239 0.0017 0.7064 0.8129 1.750 0.1828 0.00765 0.00229 0.0038 0.5403 0.8171 2.000 0.2043 0.00817 0.00245 0.0049 0.4516 0.8188 2.250 0.2270 0.00861 0.00260 0.0057 0.3784 0.8204 2.500 0.2509 0.00897 0.00274 0.0062 0.3226 0.8221 2.750 0.2754 0.00929 0.00287 0.0067 0.2771 0.8238 3.000 0.3003 0.00958 0.00300 0.0071 0.2387 0.8253 3.250 0.3257 0.00983 0.00312 0.0074 0.2107 0.8271 3.500 0.3511 0.01008 0.00326 0.0078 0.1864 0.8289 3.750 0.3770 0.01029 0.00339 0.0080 0.1681 0.8304 4.000 0.4029 0.01050 0.00353 0.0082 0.1528 0.8319 4.250 0.4286 0.01071 0.00368 0.0086 0.1388 0.8332 4.500 0.4542 0.01091 0.00384 0.0089 0.1273 0.8345 4.750 0.4800 0.01109 0.00402 0.0092 0.1184 0.8360 5.000 0.5054 0.01131 0.00421 0.0096 0.1094 0.8378 5.250 0.5308 0.01152 0.00440 0.0099 0.1013 0.8396 5.500 0.5563 0.01174 0.00460 0.0103 0.0948 0.8413 5.750 0.5815 0.01197 0.00481 0.0106 0.0879 0.8430 6.000 0.6066 0.01221 0.00504 0.0110 0.0825 0.8448 6.250 0.6318 0.01244 0.00527 0.0114 0.0774 0.8466 6.500 0.6563 0.01273 0.00552 0.0118 0.0721 0.8483 6.750 0.6810 0.01294 0.00578 0.0123 0.0685 0.8500 7.000 0.7052 0.01321 0.00605 0.0129 0.0643 0.8519 7.250 0.7289 0.01350 0.00635 0.0135 0.0603 0.8541 7.500 0.7530 0.01376 0.00664 0.0140 0.0571 0.8566 7.750 0.7765 0.01407 0.00695 0.0146 0.0534 0.8592 8.000 0.7998 0.01440 0.00729 0.0152 0.0505 0.8617 8.500 0.8457 0.01501 0.00797 0.0166 0.0450 0.8666 8.750 0.8673 0.01539 0.00837 0.0175 0.0426 0.8695 9.000 0.8897 0.01570 0.00874 0.0183 0.0407 0.8727 9.250 0.9115 0.01605 0.00913 0.0191 0.0383 0.8763 9.750 0.9525 0.01685 0.01001 0.0212 0.0344 0.8840 10.000 0.9722 0.01722 0.01045 0.0224 0.0328 0.8890 10.250 0.9904 0.01762 0.01090 0.0238 0.0311 0.8950 10.500 1.0063 0.01808 0.01140 0.0257 0.0296 0.9023 11.000 1.0389 0.01895 0.01247 0.0291 0.0272 0.9233 11.250 1.0568 0.01945 0.01305 0.0303 0.0259 0.9399 11.500 1.0823 0.02015 0.01381 0.0298 0.0244 0.9609 12.000 1.1243 0.02151 0.01532 0.0302 0.0226 1.0000 12.250 1.1391 0.02220 0.01607 0.0316 0.0217 1.0000 12.500 1.1530 0.02295 0.01687 0.0330 0.0210 1.0000 12.750 1.1658 0.02377 0.01774 0.0344 0.0203 1.0000 13.000 1.1763 0.02477 0.01877 0.0360 0.0196 1.0000 13.250 1.1882 0.02567 0.01977 0.0374 0.0191 1.0000 13.500 1.1999 0.02660 0.02080 0.0388 0.0185 1.0000 13.750 1.2109 0.02759 0.02187 0.0401 0.0180 1.0000 14.000 1.2200 0.02872 0.02308 0.0414 0.0175 1.0000 14.250 1.2279 0.02997 0.02441 0.0427 0.0172 1.0000 14.500 1.2348 0.03132 0.02584 0.0440 0.0167 1.0000 14.750 1.2395 0.03288 0.02748 0.0452 0.0163 1.0000 15.000 1.2408 0.03476 0.02944 0.0464 0.0159 1.0000 15.250 1.2426 0.03668 0.03147 0.0473 0.0157 1.0000 15.500 1.2462 0.03854 0.03346 0.0480 0.0154 1.0000 15.750 1.2471 0.04072 0.03575 0.0485 0.0151 1.0000 16.000 1.2461 0.04323 0.03839 0.0487 0.0149 1.0000 16.250 1.2427 0.04614 0.04143 0.0485 0.0146 1.0000 16.500 1.2380 0.04945 0.04486 0.0478 0.0144 1.0000 16.750 1.2287 0.05367 0.04922 0.0463 0.0143 1.0000 17.000 1.2173 0.05860 0.05431 0.0440 0.0142 1.0000 17.250 1.2040 0.06436 0.06022 0.0408 0.0140 1.0000 17.500 1.1835 0.07183 0.06787 0.0364 0.0140 1.0000 17.750 1.1564 0.08090 0.07713 0.0308 0.0140 1.0000 18.000 1.1221 0.09156 0.08798 0.0244 0.0140 1.0000 18.250 1.0853 0.10275 0.09934 0.0179 0.0142 1.0000