XFOIL Version 6.94 Calculated polar for: AH 94-145 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.300 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- -19.500 -0.4573 0.22502 0.22201 -0.0015 1.0002 0.0174 -19.000 -0.4370 0.21882 0.21584 -0.0049 1.0002 0.0180 -18.500 -0.4172 0.21278 0.20983 -0.0090 1.0002 0.0189 -18.000 -0.3975 0.20640 0.20350 -0.0134 1.0002 0.0198 -17.000 -0.3666 0.19495 0.19180 -0.0207 0.8743 0.0221 -16.500 -0.3589 0.19011 0.18678 -0.0254 0.8472 0.0225 -16.000 -0.3503 0.18451 0.18104 -0.0298 0.8300 0.0226 -15.500 -0.1089 0.13325 0.12977 -0.0555 0.7811 0.0265 -15.000 -0.1013 0.12959 0.12609 -0.0588 0.7762 0.0289 -14.500 -0.1076 0.12829 0.12476 -0.0627 0.7724 0.0295 -14.000 -0.1036 0.12468 0.12110 -0.0651 0.7685 0.0296 -13.500 -0.2701 0.15121 0.14739 -0.0446 0.7848 0.0293 -13.000 -0.2608 0.14479 0.14099 -0.0495 0.7792 0.0295 -12.500 -0.0580 0.10870 0.10505 -0.0680 0.7565 0.0332 -12.000 -0.0537 0.10446 0.10080 -0.0696 0.7532 0.0352 -11.500 -0.0608 0.09988 0.09620 -0.0731 0.7502 0.0381 -11.000 -0.1935 0.11727 0.11336 -0.0573 0.7590 0.0340 -10.500 -0.1830 0.11065 0.10676 -0.0618 0.7547 0.0370 -10.000 -0.1786 0.10392 0.10003 -0.0701 0.7502 0.0386 -9.500 -0.1686 0.09650 0.09260 -0.0754 0.7458 0.0388 -9.000 -0.1607 0.08798 0.08406 -0.0758 0.7416 0.0406 -8.500 -0.1385 0.08335 0.07946 -0.0774 0.7380 0.0429 -8.000 -0.1246 0.07677 0.07293 -0.0828 0.7338 0.0462 -7.500 -0.1109 0.06534 0.06143 -0.1049 0.7291 0.0505 -7.000 -0.0900 0.05572 0.05141 -0.1149 0.7248 0.0509 -6.500 -0.0746 0.04291 0.03826 -0.1212 0.7209 0.0534 -6.000 -0.0410 0.02489 0.01856 -0.1262 0.7179 0.0350 -5.500 0.0143 0.02244 0.01560 -0.1271 0.7138 0.0381 -5.000 0.0693 0.01904 0.01171 -0.1279 0.7092 0.0412 -4.500 0.1264 0.01801 0.01055 -0.1285 0.7052 0.0463 -4.000 0.1837 0.01689 0.00925 -0.1291 0.7017 0.0548 -3.500 0.2412 0.01669 0.00898 -0.1297 0.6980 0.0656 -3.000 0.2987 0.01595 0.00829 -0.1307 0.6938 0.0833 -2.500 0.3567 0.01546 0.00782 -0.1316 0.6892 0.1046 -2.000 0.4155 0.01505 0.00746 -0.1327 0.6853 0.1347 -1.500 0.4761 0.01401 0.00726 -0.1348 0.6817 0.3732 -0.500 0.5714 0.01362 0.00828 -0.1311 0.6737 0.8579 0.000 0.6100 0.01391 0.00862 -0.1270 0.6690 0.9159 0.500 0.6490 0.01394 0.00860 -0.1230 0.6646 0.9627 1.000 0.7172 0.01395 0.00848 -0.1257 0.6608 0.9998 1.500 0.7780 0.01446 0.00885 -0.1274 0.6574 0.9998 2.000 0.8348 0.01499 0.00943 -0.1287 0.6520 0.9998 2.500 0.8933 0.01546 0.00988 -0.1301 0.6468 0.9998 3.000 0.9535 0.01570 0.01009 -0.1315 0.6424 0.9998 3.500 1.0144 0.01594 0.01028 -0.1329 0.6388 0.9998 4.000 1.0700 0.01659 0.01100 -0.1338 0.6334 0.9998 4.500 1.1247 0.01707 0.01156 -0.1344 0.6267 0.9998 5.000 1.1848 0.01703 0.01155 -0.1354 0.6215 0.9998 5.500 1.2475 0.01686 0.01133 -0.1367 0.6162 0.9998 6.000 1.3005 0.01668 0.01131 -0.1365 0.6050 0.9998 6.500 1.3644 0.01585 0.01042 -0.1376 0.5959 0.9998 7.000 1.4174 0.01557 0.01028 -0.1373 0.5833 0.9998 7.500 1.4707 0.01548 0.01032 -0.1371 0.5718 0.9998 8.000 1.5241 0.01521 0.01013 -0.1368 0.5571 0.9998 8.500 1.5687 0.01530 0.01038 -0.1352 0.5355 0.9998 9.000 1.6080 0.01571 0.01088 -0.1328 0.5078 0.9998 9.500 1.6293 0.01674 0.01185 -0.1276 0.4658 0.9998 10.000 1.6215 0.01966 0.01452 -0.1197 0.4031 0.9998 10.500 1.5918 0.02542 0.01993 -0.1122 0.3344 0.9998 11.000 1.5607 0.03218 0.02639 -0.1061 0.2753 0.9998 11.500 1.5362 0.03867 0.03264 -0.1009 0.2256 0.9998 12.000 1.5205 0.04477 0.03856 -0.0969 0.1840 0.9998 12.500 1.5120 0.05056 0.04422 -0.0938 0.1505 0.9998 13.500 1.5064 0.06167 0.05520 -0.0890 0.1042 0.9998 14.000 1.5063 0.06716 0.06068 -0.0870 0.0887 0.9998 14.500 1.5036 0.07309 0.06662 -0.0853 0.0761 0.9998 15.000 1.5116 0.07799 0.07165 -0.0842 0.0672 0.9998 15.500 1.5109 0.08383 0.07757 -0.0829 0.0600 0.9998 16.000 1.5159 0.08925 0.08315 -0.0822 0.0542 0.9998 16.500 1.5132 0.09538 0.08933 -0.0812 0.0487 0.9998 17.000 1.5202 0.10072 0.09490 -0.0810 0.0449 0.9998 17.500 1.5219 0.10675 0.10108 -0.0812 0.0414 0.9998 18.000 1.5216 0.11243 0.10683 -0.0806 0.0375 0.9998 18.500 1.5249 0.11862 0.11330 -0.0816 0.0352 0.9998 19.000 1.5260 0.12502 0.11989 -0.0828 0.0327 0.9998 19.500 1.5246 0.13177 0.12677 -0.0845 0.0305 0.9998 20.000 1.5227 0.13784 0.13302 -0.0853 0.0280 0.9998 20.500 1.5197 0.14558 0.14105 -0.0885 0.0267 0.9998 21.000 1.5143 0.15374 0.14951 -0.0922 0.0252 0.9998 21.500 1.5084 0.16215 0.15816 -0.0965 0.0238 0.9998 22.000 1.5023 0.17066 0.16684 -0.1013 0.0227 0.9998 22.500 1.4918 0.17997 0.17635 -0.1069 0.0215 0.9998 23.000 1.4605 0.19434 0.19111 -0.1162 0.0207 0.9998 23.500 1.4311 0.21072 0.20788 -0.1280 0.0204 0.9998 24.000 1.3345 0.25253 0.25025 -0.1577 0.0210 0.9998 24.500 0.7996 0.26263 0.26048 -0.1125 0.0337 0.9998 25.000 0.8069 0.26796 0.26585 -0.1146 0.0303 0.9998 25.500 0.8211 0.27199 0.26993 -0.1151 0.0288 0.9998 26.000 0.8216 0.28309 0.28103 -0.1181 0.0282 0.9998 26.500 0.8134 0.29337 0.29131 -0.1234 0.0257 0.9998 27.000 0.8180 0.29987 0.29784 -0.1258 0.0227 0.9998 27.500 0.8258 0.30477 0.30278 -0.1275 0.0214 0.9998 28.000 0.8338 0.31354 0.31157 -0.1288 0.0207 0.9998 28.500 0.8298 0.32264 0.32069 -0.1329 0.0203 0.9998 29.000 0.8295 0.33181 0.32987 -0.1364 0.0179 0.9998 29.500 0.8330 0.33854 0.33663 -0.1389 0.0163 0.9998 30.000 0.8383 0.34366 0.34178 -0.1407 0.0153 0.9998 30.500 0.8450 0.35188 0.35003 -0.1421 0.0148 0.9998 31.000 0.8412 0.36106 0.35922 -0.1460 0.0145 0.9998 31.500 0.8420 0.36996 0.36814 -0.1490 0.0128 0.9998 32.000 0.8442 0.37702 0.37522 -0.1514 0.0117 0.9998 32.500 0.8464 0.38333 0.38157 -0.1537 0.0110 0.9998 33.000 0.8495 0.38905 0.38733 -0.1556 0.0106 0.9998 33.500 0.8520 0.39746 0.39576 -0.1576 0.0103 0.9998 34.000 0.8494 0.40692 0.40523 -0.1611 0.0097 0.9998 34.500 0.8503 0.41456 0.41289 -0.1635 0.0087 0.9998 35.000 0.8510 0.42130 0.41966 -0.1658 0.0079 0.9998 35.500 0.8515 0.42728 0.42568 -0.1681 0.0074 0.9998 36.000 0.8526 0.43283 0.43127 -0.1700 0.0071 0.9998 36.500 0.8521 0.44097 0.43943 -0.1722 0.0070 0.9998 37.000 0.8504 0.44926 0.44774 -0.1750 0.0068 0.9998 37.500 0.8500 0.45693 0.45543 -0.1773 0.0063 0.9998 38.000 0.8491 0.46363 0.46216 -0.1796 0.0057 0.9998 38.500 0.8480 0.46964 0.46820 -0.1818 0.0052 0.9998 39.000 0.8464 0.47491 0.47351 -0.1840 0.0048 0.9998 39.500 0.8448 0.47986 0.47850 -0.1860 0.0046 0.9998 40.000 0.8427 0.48705 0.48570 -0.1882 0.0045 0.9998