XFOIL Version 6.96 Calculated polar for: MH 108 11.98% 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 ------ -------- --------- --------- -------- -------- -------- -15.000 -0.9964 0.08329 0.07989 0.0002 1.0000 0.0034 -14.750 -1.0240 0.07406 0.07050 -0.0052 1.0000 0.0033 -14.500 -1.0504 0.06507 0.06135 -0.0107 1.0000 0.0033 -14.250 -1.0710 0.05720 0.05333 -0.0159 1.0000 0.0033 -14.000 -1.0868 0.05058 0.04652 -0.0203 1.0000 0.0033 -13.750 -1.1005 0.04501 0.04078 -0.0237 1.0000 0.0033 -13.500 -1.1100 0.04084 0.03646 -0.0256 1.0000 0.0034 -13.250 -1.1166 0.03764 0.03313 -0.0262 1.0000 0.0035 -13.000 -1.1236 0.03491 0.03024 -0.0255 1.0000 0.0034 -12.750 -1.1277 0.03277 0.02798 -0.0239 1.0000 0.0034 -12.500 -1.1271 0.03116 0.02625 -0.0220 1.0000 0.0035 -12.250 -1.1274 0.02961 0.02457 -0.0193 1.0000 0.0035 -12.000 -1.1245 0.02834 0.02319 -0.0165 1.0000 0.0036 -11.750 -1.1187 0.02721 0.02195 -0.0139 1.0000 0.0037 -11.500 -1.1086 0.02605 0.02068 -0.0118 1.0000 0.0038 -11.250 -1.0961 0.02498 0.01950 -0.0100 1.0000 0.0039 -11.000 -1.0819 0.02395 0.01837 -0.0084 1.0000 0.0040 -10.750 -1.0667 0.02295 0.01725 -0.0068 1.0000 0.0041 -10.500 -1.0497 0.02204 0.01622 -0.0054 1.0000 0.0043 -10.250 -1.0317 0.02119 0.01527 -0.0041 1.0000 0.0044 -10.000 -1.0126 0.02040 0.01439 -0.0028 1.0000 0.0046 -9.750 -0.9929 0.01964 0.01353 -0.0017 1.0000 0.0047 -9.500 -0.9738 0.01876 0.01256 -0.0004 1.0000 0.0049 -9.250 -0.9533 0.01802 0.01175 0.0007 1.0000 0.0053 -9.000 -0.9317 0.01739 0.01106 0.0016 1.0000 0.0056 -8.750 -0.9095 0.01679 0.01038 0.0026 1.0000 0.0060 -8.500 -0.8868 0.01626 0.00979 0.0034 1.0000 0.0065 -8.250 -0.8643 0.01569 0.00917 0.0044 1.0000 0.0072 -8.000 -0.8416 0.01513 0.00858 0.0052 1.0000 0.0084 -7.750 -0.8182 0.01465 0.00805 0.0061 1.0000 0.0095 -7.500 -0.7955 0.01410 0.00750 0.0070 1.0000 0.0116 -7.250 -0.7722 0.01362 0.00699 0.0079 1.0000 0.0143 -7.000 -0.7489 0.01316 0.00654 0.0087 1.0000 0.0186 -6.750 -0.7225 0.01268 0.00610 0.0089 0.9919 0.0254 -6.500 -0.6783 0.01216 0.00561 0.0053 0.9260 0.0368 -6.250 -0.6511 0.01192 0.00524 0.0056 0.8582 0.0470 -6.000 -0.6286 0.01172 0.00491 0.0069 0.8113 0.0572 -5.750 -0.6050 0.01151 0.00461 0.0079 0.7747 0.0682 -5.500 -0.5807 0.01129 0.00433 0.0086 0.7430 0.0816 -5.250 -0.5559 0.01107 0.00406 0.0093 0.7149 0.0961 -5.000 -0.5306 0.01087 0.00381 0.0099 0.6894 0.1095 -4.750 -0.5049 0.01069 0.00357 0.0104 0.6664 0.1227 -4.500 -0.4790 0.01051 0.00335 0.0109 0.6455 0.1369 -4.250 -0.4530 0.01034 0.00315 0.0114 0.6255 0.1532 -4.000 -0.4269 0.01018 0.00296 0.0118 0.6059 0.1703 -3.750 -0.4005 0.01003 0.00278 0.0122 0.5878 0.1863 -3.500 -0.3743 0.00986 0.00261 0.0126 0.5715 0.2057 -3.250 -0.3478 0.00972 0.00246 0.0129 0.5550 0.2253 -3.000 -0.3214 0.00958 0.00232 0.0133 0.5387 0.2466 -2.750 -0.2949 0.00945 0.00219 0.0137 0.5233 0.2686 -2.500 -0.2683 0.00931 0.00208 0.0140 0.5095 0.2918 -2.250 -0.2418 0.00918 0.00197 0.0143 0.4959 0.3183 -2.000 -0.2153 0.00905 0.00188 0.0147 0.4821 0.3467 -1.750 -0.1887 0.00893 0.00180 0.0150 0.4688 0.3739 -1.500 -0.1622 0.00882 0.00173 0.0154 0.4562 0.4033 -1.250 -0.1357 0.00870 0.00166 0.0157 0.4450 0.4343 -0.750 -0.0829 0.00849 0.00157 0.0165 0.4230 0.4971 -0.500 -0.0567 0.00838 0.00153 0.0170 0.4121 0.5325 -0.250 -0.0308 0.00827 0.00151 0.0175 0.4022 0.5700 0.000 -0.0050 0.00816 0.00150 0.0180 0.3930 0.6104 0.250 0.0205 0.00804 0.00150 0.0186 0.3847 0.6525 0.500 0.0459 0.00795 0.00151 0.0193 0.3762 0.6938 0.750 0.0713 0.00785 0.00154 0.0200 0.3677 0.7356 1.000 0.0969 0.00778 0.00157 0.0207 0.3599 0.7758 1.250 0.1229 0.00771 0.00163 0.0214 0.3528 0.8155 1.500 0.1502 0.00770 0.00170 0.0218 0.3460 0.8520 1.750 0.1803 0.00773 0.00179 0.0216 0.3387 0.8834 2.000 0.2139 0.00782 0.00190 0.0206 0.3318 0.9083 2.250 0.2498 0.00793 0.00200 0.0191 0.3249 0.9260 2.500 0.2859 0.00808 0.00212 0.0175 0.3180 0.9387 2.750 0.3224 0.00819 0.00222 0.0158 0.3116 0.9475 3.000 0.3552 0.00834 0.00233 0.0149 0.3050 0.9561 3.250 0.3900 0.00846 0.00244 0.0136 0.2992 0.9621 3.500 0.4205 0.00860 0.00256 0.0131 0.2930 0.9693 3.750 0.4560 0.00874 0.00267 0.0115 0.2872 0.9731 4.000 0.4892 0.00886 0.00280 0.0105 0.2811 0.9781 4.250 0.5210 0.00902 0.00293 0.0097 0.2753 0.9826 4.500 0.5575 0.00913 0.00305 0.0078 0.2694 0.9856 4.750 0.5936 0.00926 0.00318 0.0061 0.2631 0.9895 5.000 0.6284 0.00941 0.00333 0.0046 0.2572 0.9933 5.250 0.6643 0.00952 0.00345 0.0029 0.2503 0.9958 5.500 0.6987 0.00966 0.00358 0.0014 0.2435 0.9981 5.750 0.7324 0.00979 0.00372 0.0001 0.2362 1.0000 6.000 0.7563 0.00995 0.00388 0.0009 0.2293 1.0000 6.250 0.7803 0.01011 0.00406 0.0016 0.2212 1.0000 6.500 0.8042 0.01029 0.00424 0.0023 0.2139 1.0000 6.750 0.8279 0.01051 0.00444 0.0031 0.2042 1.0000 7.000 0.8516 0.01072 0.00466 0.0039 0.1945 1.0000 7.250 0.8750 0.01097 0.00491 0.0046 0.1837 1.0000 7.500 0.8980 0.01127 0.00519 0.0054 0.1719 1.0000 7.750 0.9207 0.01161 0.00550 0.0063 0.1599 1.0000 8.000 0.9430 0.01199 0.00584 0.0072 0.1481 1.0000 8.250 0.9652 0.01237 0.00620 0.0080 0.1362 1.0000 8.500 0.9871 0.01279 0.00661 0.0090 0.1243 1.0000 8.750 1.0089 0.01321 0.00702 0.0099 0.1139 1.0000 9.000 1.0303 0.01365 0.00745 0.0108 0.1048 1.0000 9.250 1.0510 0.01415 0.00793 0.0118 0.0949 1.0000 9.500 1.0715 0.01467 0.00843 0.0129 0.0843 1.0000 9.750 1.0915 0.01522 0.00896 0.0139 0.0740 1.0000 10.000 1.1110 0.01580 0.00954 0.0151 0.0648 1.0000 10.250 1.1293 0.01645 0.01017 0.0163 0.0551 1.0000 10.500 1.1470 0.01715 0.01084 0.0175 0.0468 1.0000 10.750 1.1633 0.01791 0.01159 0.0189 0.0385 1.0000 11.000 1.1797 0.01864 0.01232 0.0203 0.0321 1.0000 11.250 1.1943 0.01946 0.01315 0.0219 0.0263 1.0000 11.500 1.2075 0.02034 0.01403 0.0235 0.0218 1.0000 11.750 1.2203 0.02118 0.01494 0.0252 0.0185 1.0000 12.000 1.2306 0.02214 0.01593 0.0271 0.0156 1.0000 12.250 1.2377 0.02318 0.01700 0.0292 0.0130 1.0000 12.500 1.2393 0.02423 0.01811 0.0322 0.0116 1.0000 12.750 1.2401 0.02552 0.01949 0.0344 0.0102 1.0000 13.000 1.2403 0.02723 0.02128 0.0356 0.0095 1.0000 13.250 1.2396 0.02947 0.02361 0.0358 0.0088 1.0000 13.500 1.2397 0.03200 0.02625 0.0353 0.0081 1.0000 13.750 1.2382 0.03501 0.02938 0.0342 0.0076 1.0000 14.000 1.2334 0.03861 0.03308 0.0328 0.0069 1.0000 14.250 1.2255 0.04273 0.03730 0.0310 0.0064 1.0000 14.500 1.2173 0.04692 0.04161 0.0292 0.0062 1.0000 14.750 1.2088 0.05121 0.04601 0.0274 0.0060 1.0000 15.000 1.1979 0.05582 0.05074 0.0255 0.0060 1.0000 15.250 1.1868 0.06049 0.05552 0.0236 0.0057 1.0000 15.500 1.1736 0.06550 0.06063 0.0215 0.0056 1.0000 15.750 1.1617 0.07040 0.06563 0.0194 0.0054 1.0000 16.000 1.1471 0.07591 0.07124 0.0170 0.0051 1.0000 16.250 1.1344 0.08130 0.07675 0.0146 0.0050 1.0000 16.500 1.1234 0.08652 0.08206 0.0123 0.0050 1.0000 16.750 1.1100 0.09224 0.08788 0.0097 0.0048 1.0000 17.000 1.1009 0.09738 0.09312 0.0074 0.0049 1.0000 17.250 1.0871 0.10340 0.09923 0.0046 0.0047 1.0000 17.500 1.0745 0.10934 0.10525 0.0018 0.0045 1.0000 17.750 1.0636 0.11511 0.11111 -0.0010 0.0044 1.0000