XFOIL Version 6.94 Calculated polar for: AH 93-W-215 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 ------- -------- --------- --------- -------- ------- ------- 0.000 0.3352 0.01429 0.00771 -0.0688 0.5816 0.6599 0.500 0.3893 0.01429 0.00777 -0.0682 0.5753 0.6816 1.000 0.4442 0.01441 0.00787 -0.0678 0.5691 0.7017 1.500 0.4946 0.01486 0.00833 -0.0669 0.5631 0.7189 2.000 0.5432 0.01490 0.00853 -0.0653 0.5574 0.7365 2.500 0.5939 0.01485 0.00854 -0.0642 0.5499 0.7548 3.000 0.6472 0.01488 0.00858 -0.0635 0.5435 0.7723 3.500 0.7023 0.01495 0.00862 -0.0632 0.5360 0.7893 4.000 0.7488 0.01527 0.00903 -0.0614 0.5291 0.8094 4.500 0.7934 0.01545 0.00933 -0.0593 0.5225 0.8292 5.000 0.8411 0.01543 0.00941 -0.0575 0.5145 0.8480 5.500 0.8929 0.01512 0.00902 -0.0562 0.5037 0.8682 6.000 0.9369 0.01569 0.00970 -0.0542 0.4981 0.8901 6.500 0.9710 0.01570 0.00987 -0.0500 0.4903 0.9158 7.000 1.0179 0.01543 0.00966 -0.0481 0.4795 0.9413 7.500 1.0903 0.01565 0.00984 -0.0517 0.4688 0.9631 8.000 1.1670 0.01610 0.01046 -0.0571 0.4582 0.9818 8.500 1.2147 0.01630 0.01067 -0.0568 0.4474 1.0000 9.000 1.2469 0.01662 0.01083 -0.0530 0.4333 1.0000 9.500 1.2663 0.01716 0.01154 -0.0474 0.4228 1.0000 10.000 1.2961 0.01776 0.01207 -0.0437 0.4097 1.0000 10.500 1.3174 0.01876 0.01309 -0.0393 0.3955 1.0000 11.000 1.3377 0.02003 0.01440 -0.0353 0.3823 1.0000 11.500 1.3549 0.02171 0.01603 -0.0316 0.3668 1.0000 12.000 1.3703 0.02383 0.01831 -0.0285 0.3557 1.0000 12.500 1.3780 0.02650 0.02090 -0.0252 0.3367 1.0000 13.000 1.3839 0.02974 0.02426 -0.0228 0.3230 1.0000 13.500 1.3815 0.03361 0.02807 -0.0200 0.3035 1.0000 14.000 1.3863 0.03730 0.03183 -0.0179 0.2896 1.0000 14.500 1.3907 0.04107 0.03561 -0.0161 0.2753 1.0000 15.000 1.3880 0.04589 0.04046 -0.0146 0.2589 1.0000 15.500 1.3792 0.05133 0.04590 -0.0134 0.2400 1.0000 16.000 1.3891 0.05507 0.04969 -0.0124 0.2302 1.0000 16.500 1.3783 0.06132 0.05598 -0.0119 0.2117 1.0000 17.000 1.3777 0.06652 0.06115 -0.0115 0.1984 1.0000 17.500 1.3755 0.07221 0.06696 -0.0116 0.1862 1.0000 18.000 1.3708 0.07797 0.07263 -0.0117 0.1723 1.0000 18.500 1.3680 0.08401 0.07884 -0.0124 0.1616 1.0000 19.000 1.3453 0.09224 0.08702 -0.0136 0.1427 1.0000 19.500 1.3435 0.09810 0.09294 -0.0147 0.1334 1.0000 20.000 1.3345 0.10513 0.09996 -0.0163 0.1227 1.0000 20.500 1.3158 0.11371 0.10859 -0.0190 0.1078 1.0000 21.500 1.2983 0.12817 0.12316 -0.0241 0.0896 1.0000 22.000 1.2959 0.13442 0.12947 -0.0268 0.0821 1.0000 22.500 1.2875 0.14176 0.13691 -0.0304 0.0745 1.0000 23.000 1.2826 0.14824 0.14334 -0.0336 0.0673 1.0000 23.500 1.2851 0.15354 0.14880 -0.0369 0.0640 1.0000 24.000 1.2777 0.16057 0.15594 -0.0413 0.0588 1.0000 24.500 1.2761 0.16676 0.16212 -0.0452 0.0531 1.0000 25.000 1.2700 0.17423 0.16975 -0.0498 0.0491 1.0000 25.500 1.2558 0.18366 0.17927 -0.0556 0.0431 1.0000 26.000 1.2626 0.18899 0.18480 -0.0591 0.0437 1.0000 26.500 1.2575 0.19665 0.19244 -0.0637 0.0375 1.0000 27.000 1.2358 0.20921 0.20517 -0.0713 0.0329 1.0000 27.500 1.2274 0.21895 0.21504 -0.0770 0.0307 1.0000 28.000 1.2133 0.23025 0.22659 -0.0831 0.0309 1.0000 28.500 0.9611 0.33846 0.33530 -0.1136 0.0244 1.0000 30.000 0.9579 0.37754 0.37450 -0.1242 0.0284 1.0000 30.500 0.9683 0.38212 0.37913 -0.1256 0.0274 1.0000 32.000 0.7787 0.37948 0.37689 -0.1123 0.0216 1.0000 32.500 0.7720 0.38024 0.37770 -0.1135 0.0199 1.0000 33.000 0.7681 0.38117 0.37867 -0.1150 0.0190 1.0000 33.500 0.7655 0.38137 0.37891 -0.1163 0.0182 1.0000 34.000 0.7642 0.38109 0.37870 -0.1174 0.0177 1.0000 35.000 0.7492 0.38478 0.38246 -0.1196 0.0169 1.0000 35.500 0.7456 0.38696 0.38469 -0.1216 0.0169 1.0000 36.000 0.7423 0.38963 0.38740 -0.1238 0.0169 1.0000 36.500 0.7386 0.39257 0.39038 -0.1263 0.0167 1.0000 37.000 0.7354 0.39606 0.39390 -0.1289 0.0166 1.0000 37.500 0.7335 0.40140 0.39928 -0.1320 0.0156 1.0000 38.000 0.7321 0.40460 0.40253 -0.1344 0.0141 1.0000 38.500 0.7311 0.40694 0.40490 -0.1366 0.0120 1.0000 39.000 0.7317 0.40865 0.40665 -0.1388 0.0107 1.0000 39.500 0.7302 0.41075 0.40878 -0.1410 0.0106 1.0000