XFOIL Version 6.94 Calculated polar for: AH 95-160 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 ------- -------- --------- --------- -------- ------- ------- -20.000 -0.2044 0.17324 0.17012 -0.0379 0.8213 0.0225 -19.000 -0.4062 0.21672 0.21384 -0.0156 1.0002 0.0224 -18.500 -0.4008 0.21299 0.20982 -0.0184 0.8747 0.0226 -18.000 -0.3798 0.20356 0.20020 -0.0187 0.8447 0.0231 -17.500 -0.3605 0.19767 0.19415 -0.0207 0.8263 0.0237 -17.000 -0.3423 0.19190 0.18828 -0.0237 0.8129 0.0247 -16.500 -0.3249 0.18589 0.18217 -0.0271 0.8031 0.0261 -16.000 -0.3086 0.17952 0.17576 -0.0313 0.7949 0.0284 -15.500 -0.3049 0.17476 0.17094 -0.0381 0.7883 0.0294 -15.000 -0.2935 0.16840 0.16454 -0.0423 0.7825 0.0296 -14.500 -0.2738 0.15844 0.15457 -0.0440 0.7768 0.0303 -14.000 -0.2516 0.15235 0.14843 -0.0453 0.7707 0.0312 -13.500 -0.2344 0.14661 0.14262 -0.0476 0.7652 0.0325 -13.000 -0.2191 0.14047 0.13646 -0.0506 0.7608 0.0344 -12.500 -0.2114 0.13399 0.13000 -0.0559 0.7568 0.0378 -12.000 -0.2070 0.12755 0.12357 -0.0622 0.7529 0.0386 -11.500 -0.1967 0.12033 0.11633 -0.0666 0.7490 0.0388 -11.000 -0.1829 0.11183 0.10781 -0.0662 0.7452 0.0407 -10.500 -0.1631 0.10669 0.10264 -0.0678 0.7410 0.0424 -10.000 -0.1494 0.10052 0.09650 -0.0711 0.7373 0.0445 -9.500 -0.1409 0.09346 0.08947 -0.0761 0.7336 0.0478 -9.000 -0.1377 0.08524 0.08130 -0.0870 0.7298 0.0506 -8.500 -0.1356 0.07413 0.07020 -0.0989 0.7261 0.0509 -8.000 -0.1661 0.05674 0.05252 -0.1142 0.7227 0.0519 -7.500 -0.1894 0.03386 0.02850 -0.1214 0.7193 0.0353 -7.000 -0.1501 0.02819 0.02207 -0.1224 0.7154 0.0373 -6.500 -0.1009 0.02500 0.01829 -0.1228 0.7114 0.0387 -6.000 -0.0518 0.02103 0.01385 -0.1233 0.7076 0.0420 -5.500 0.0036 0.01999 0.01262 -0.1237 0.7037 0.0463 -5.000 0.0592 0.01902 0.01137 -0.1239 0.6999 0.0522 -4.500 0.1145 0.01810 0.01047 -0.1244 0.6965 0.0607 -4.000 0.1702 0.01730 0.00963 -0.1249 0.6926 0.0719 -3.500 0.2270 0.01701 0.00929 -0.1255 0.6882 0.0843 -3.000 0.2834 0.01633 0.00862 -0.1260 0.6842 0.1013 -2.500 0.3409 0.01593 0.00820 -0.1267 0.6810 0.1216 -2.000 0.3979 0.01584 0.00819 -0.1275 0.6776 0.1598 -1.500 0.4524 0.01453 0.00828 -0.1290 0.6734 0.5247 -1.000 0.5044 0.01435 0.00870 -0.1283 0.6687 0.7205 -0.500 0.5553 0.01451 0.00902 -0.1269 0.6648 0.8044 0.000 0.6047 0.01466 0.00919 -0.1252 0.6613 0.8589 0.500 0.6512 0.01488 0.00938 -0.1227 0.6579 0.9067 1.000 0.6971 0.01517 0.00979 -0.1202 0.6534 0.9825 1.500 0.7616 0.01564 0.01021 -0.1233 0.6484 0.9998 2.000 0.8206 0.01592 0.01041 -0.1249 0.6439 0.9998 2.500 0.8811 0.01616 0.01056 -0.1264 0.6404 0.9998 3.000 0.9421 0.01653 0.01083 -0.1278 0.6372 0.9998 3.500 0.9912 0.01742 0.01184 -0.1280 0.6309 0.9998 4.000 1.0463 0.01785 0.01230 -0.1286 0.6253 0.9998 4.500 1.1058 0.01795 0.01237 -0.1297 0.6213 0.9998 5.000 1.1683 0.01792 0.01230 -0.1310 0.6177 0.9998 5.500 1.2138 0.01871 0.01326 -0.1303 0.6096 0.9998 6.000 1.2735 0.01836 0.01293 -0.1311 0.6030 0.9998 6.500 1.3425 0.01745 0.01192 -0.1329 0.5969 0.9998 7.000 1.3900 0.01721 0.01185 -0.1318 0.5847 0.9998 7.500 1.4494 0.01668 0.01133 -0.1323 0.5756 0.9998 8.000 1.4989 0.01653 0.01132 -0.1315 0.5637 0.9998 8.500 1.5442 0.01662 0.01154 -0.1301 0.5505 0.9998 9.000 1.5870 0.01671 0.01175 -0.1283 0.5346 0.9998 9.500 1.6151 0.01723 0.01236 -0.1241 0.5125 0.9998 10.000 1.6333 0.01837 0.01349 -0.1190 0.4846 0.9998 10.500 1.6354 0.02103 0.01611 -0.1133 0.4459 0.9998 11.000 1.6189 0.02571 0.02061 -0.1070 0.3920 0.9998 11.500 1.5877 0.03204 0.02665 -0.1004 0.3355 0.9998 12.000 1.5574 0.03873 0.03308 -0.0947 0.2859 0.9998 12.500 1.5351 0.04532 0.03946 -0.0903 0.2416 0.9998 13.000 1.5191 0.05173 0.04569 -0.0868 0.2027 0.9998 13.500 1.5090 0.05786 0.05168 -0.0840 0.1704 0.9998 14.000 1.5027 0.06381 0.05753 -0.0817 0.1447 0.9998 14.500 1.4995 0.06958 0.06324 -0.0798 0.1250 0.9998 15.000 1.5004 0.07506 0.06873 -0.0783 0.1091 0.9998 15.500 1.5034 0.08043 0.07416 -0.0771 0.0962 0.9998 16.000 1.5060 0.08588 0.07969 -0.0761 0.0855 0.9998 16.500 1.5027 0.09207 0.08586 -0.0752 0.0759 0.9998 17.000 1.5098 0.09727 0.09125 -0.0749 0.0689 0.9998 17.500 1.5059 0.10357 0.09757 -0.0744 0.0617 0.9998 18.000 1.5132 0.10884 0.10306 -0.0746 0.0573 0.9998 18.500 1.5139 0.11499 0.10930 -0.0751 0.0526 0.9998 19.000 1.5152 0.12070 0.11511 -0.0753 0.0482 0.9998 19.500 1.5194 0.12655 0.12119 -0.0764 0.0451 0.9998 20.000 1.5205 0.13281 0.12760 -0.0779 0.0422 0.9998 20.500 1.5210 0.13873 0.13357 -0.0792 0.0387 0.9998 21.000 1.5225 0.14492 0.14004 -0.0811 0.0366 0.9998 21.500 1.5212 0.15207 0.14743 -0.0842 0.0346 0.9998 22.000 1.5192 0.15934 0.15490 -0.0876 0.0326 0.9998 22.500 1.5163 0.16681 0.16252 -0.0916 0.0308 0.9998 23.000 1.5096 0.17392 0.16979 -0.0950 0.0283 0.9998 23.500 1.4997 0.18359 0.17976 -0.1012 0.0275 0.9998 24.000 1.4863 0.19419 0.19067 -0.1083 0.0265 0.9998 24.500 1.4660 0.20682 0.20362 -0.1172 0.0255 0.9998 25.000 1.4343 0.22319 0.22035 -0.1292 0.0247 0.9998 27.000 0.7989 0.28126 0.27911 -0.1120 0.0291 0.9998 27.500 0.8032 0.29136 0.28922 -0.1141 0.0282 0.9998 28.000 0.7940 0.30169 0.29956 -0.1193 0.0261 0.9998 28.500 0.7980 0.30819 0.30611 -0.1218 0.0229 0.9998 29.000 0.8043 0.31313 0.31108 -0.1238 0.0216 0.9998 29.500 0.8142 0.32057 0.31854 -0.1247 0.0207 0.9998 30.000 0.8116 0.32924 0.32723 -0.1282 0.0205 0.9998 30.500 0.8082 0.33888 0.33689 -0.1322 0.0183 0.9998 31.000 0.8113 0.34526 0.34329 -0.1347 0.0164 0.9998 31.500 0.8156 0.35027 0.34833 -0.1367 0.0154 0.9998 32.000 0.8239 0.35714 0.35525 -0.1378 0.0148 0.9998 32.500 0.8203 0.36589 0.36402 -0.1413 0.0146 0.9998 33.000 0.8185 0.37531 0.37345 -0.1447 0.0132 0.9998 33.500 0.8202 0.38222 0.38039 -0.1471 0.0120 0.9998 34.000 0.8218 0.38833 0.38653 -0.1495 0.0112 0.9998 34.500 0.8240 0.39341 0.39164 -0.1516 0.0107 0.9998 35.000 0.8270 0.40056 0.39881 -0.1533 0.0103 0.9998 35.500 0.8238 0.40962 0.40789 -0.1566 0.0100 0.9998 36.000 0.8241 0.41745 0.41576 -0.1591 0.0088 0.9998 36.500 0.8243 0.42381 0.42215 -0.1614 0.0080 0.9998 37.000 0.8243 0.42939 0.42776 -0.1637 0.0075 0.9998 37.500 0.8245 0.43427 0.43268 -0.1658 0.0072 0.9998 38.000 0.8250 0.44096 0.43938 -0.1677 0.0070 0.9998 38.500 0.8222 0.44875 0.44720 -0.1704 0.0069 0.9998 39.000 0.8210 0.45658 0.45505 -0.1729 0.0062 0.9998 39.500 0.8198 0.46261 0.46112 -0.1751 0.0056 0.9998 40.000 0.8182 0.46798 0.46653 -0.1774 0.0051 0.9998