XFOIL Version 6.96 Calculated polar for: MH 93 15.98% 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.500 -0.9976 0.14591 0.14338 0.0330 1.0000 0.0047 -19.250 -1.0252 0.13491 0.13223 0.0262 1.0000 0.0047 -19.000 -1.0538 0.12406 0.12122 0.0195 1.0000 0.0047 -18.750 -1.0806 0.11392 0.11091 0.0133 1.0000 0.0046 -18.500 -1.1029 0.10493 0.10179 0.0079 1.0000 0.0047 -18.250 -1.1272 0.09595 0.09264 0.0026 1.0000 0.0046 -18.000 -1.1488 0.08776 0.08429 -0.0022 1.0000 0.0045 -17.750 -1.1659 0.08067 0.07706 -0.0062 1.0000 0.0046 -17.500 -1.1778 0.07463 0.07090 -0.0095 1.0000 0.0046 -17.250 -1.1919 0.06855 0.06469 -0.0127 1.0000 0.0046 -17.000 -1.2016 0.06339 0.05941 -0.0152 1.0000 0.0046 -16.750 -1.2098 0.05870 0.05460 -0.0172 1.0000 0.0046 -16.500 -1.2160 0.05451 0.05030 -0.0188 1.0000 0.0047 -16.250 -1.2212 0.05069 0.04637 -0.0200 1.0000 0.0047 -16.000 -1.2246 0.04728 0.04286 -0.0208 1.0000 0.0047 -15.750 -1.2251 0.04439 0.03988 -0.0211 1.0000 0.0048 -15.500 -1.2255 0.04169 0.03708 -0.0212 1.0000 0.0048 -15.250 -1.2238 0.03933 0.03464 -0.0210 1.0000 0.0048 -15.000 -1.2223 0.03708 0.03230 -0.0205 1.0000 0.0048 -14.750 -1.2189 0.03510 0.03024 -0.0198 1.0000 0.0049 -14.500 -1.2151 0.03324 0.02831 -0.0189 1.0000 0.0049 -14.250 -1.2102 0.03157 0.02655 -0.0178 1.0000 0.0050 -14.000 -1.2032 0.03011 0.02504 -0.0166 1.0000 0.0050 -13.750 -1.1969 0.02866 0.02351 -0.0153 1.0000 0.0050 -13.500 -1.1886 0.02742 0.02220 -0.0139 1.0000 0.0050 -13.250 -1.1799 0.02623 0.02095 -0.0123 1.0000 0.0050 -13.000 -1.1702 0.02516 0.01982 -0.0108 1.0000 0.0051 -12.750 -1.1587 0.02422 0.01883 -0.0092 1.0000 0.0053 -12.500 -1.1467 0.02333 0.01789 -0.0077 1.0000 0.0054 -12.250 -1.1345 0.02249 0.01700 -0.0060 1.0000 0.0054 -11.750 -1.1028 0.02098 0.01531 -0.0037 0.9157 0.0055 -11.500 -1.0934 0.02047 0.01462 -0.0009 0.8722 0.0055 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-0.6713 0.01241 0.00519 0.0261 0.5970 0.0100 -5.750 -0.6201 0.01196 0.00468 0.0270 0.5761 0.0120 -5.500 -0.5943 0.01175 0.00444 0.0275 0.5661 0.0139 -5.250 -0.5683 0.01154 0.00422 0.0279 0.5553 0.0164 -5.000 -0.5424 0.01133 0.00400 0.0283 0.5456 0.0207 -4.750 -0.5163 0.01112 0.00379 0.0287 0.5350 0.0261 -4.500 -0.4903 0.01089 0.00358 0.0291 0.5261 0.0346 -4.250 -0.4643 0.01067 0.00338 0.0294 0.5156 0.0459 -4.000 -0.4385 0.01042 0.00318 0.0299 0.5063 0.0626 -3.750 -0.4135 0.01010 0.00296 0.0304 0.4966 0.0906 -3.500 -0.3893 0.00969 0.00273 0.0310 0.4881 0.1354 -3.000 -0.3418 0.00883 0.00230 0.0323 0.4691 0.2500 -2.750 -0.3178 0.00844 0.00213 0.0329 0.4602 0.3116 -2.500 -0.2927 0.00813 0.00199 0.0334 0.4516 0.3611 -2.250 -0.2676 0.00786 0.00187 0.0339 0.4418 0.4119 -2.000 -0.2421 0.00759 0.00177 0.0343 0.4330 0.4630 -1.750 -0.2155 0.00744 0.00170 0.0346 0.4245 0.4969 -1.500 -0.1882 0.00733 0.00164 0.0348 0.4154 0.5221 -1.250 -0.1608 0.00725 0.00159 0.0349 0.4061 0.5464 -1.000 -0.1331 0.00717 0.00155 0.0351 0.3976 0.5698 -0.750 -0.1058 0.00710 0.00152 0.0352 0.3893 0.5939 -0.500 -0.0784 0.00702 0.00149 0.0354 0.3804 0.6204 -0.250 -0.0509 0.00698 0.00148 0.0355 0.3717 0.6445 0.000 -0.0231 0.00693 0.00148 0.0356 0.3643 0.6660 0.250 0.0048 0.00693 0.00149 0.0357 0.3557 0.6853 0.500 0.0331 0.00693 0.00151 0.0357 0.3477 0.7024 0.750 0.0613 0.00696 0.00154 0.0357 0.3398 0.7175 1.000 0.0899 0.00699 0.00156 0.0357 0.3329 0.7308 1.250 0.1183 0.00704 0.00161 0.0356 0.3248 0.7431 1.500 0.1469 0.00708 0.00165 0.0356 0.3183 0.7533 1.750 0.1756 0.00714 0.00170 0.0355 0.3114 0.7631 2.000 0.2040 0.00722 0.00176 0.0354 0.3043 0.7717 2.250 0.2328 0.00728 0.00181 0.0353 0.2980 0.7803 2.500 0.2612 0.00736 0.00188 0.0352 0.2918 0.7882 2.750 0.2898 0.00744 0.00195 0.0351 0.2867 0.7974 3.000 0.3182 0.00751 0.00203 0.0351 0.2810 0.8055 3.250 0.3465 0.00762 0.00212 0.0350 0.2743 0.8133 3.500 0.3752 0.00771 0.00220 0.0348 0.2693 0.8189 3.750 0.4036 0.00779 0.00229 0.0347 0.2645 0.8241 4.000 0.4319 0.00790 0.00238 0.0346 0.2592 0.8294 4.250 0.4604 0.00801 0.00248 0.0345 0.2544 0.8343 4.500 0.4888 0.00812 0.00258 0.0344 0.2490 0.8386 4.750 0.5168 0.00824 0.00269 0.0343 0.2436 0.8431 5.000 0.5449 0.00836 0.00282 0.0342 0.2393 0.8478 5.250 0.5732 0.00847 0.00292 0.0341 0.2350 0.8522 5.500 0.6011 0.00861 0.00305 0.0340 0.2296 0.8563 5.750 0.6285 0.00875 0.00320 0.0340 0.2245 0.8607 6.000 0.6563 0.00887 0.00333 0.0340 0.2209 0.8657 6.250 0.6839 0.00902 0.00347 0.0339 0.2161 0.8709 6.500 0.7109 0.00920 0.00364 0.0339 0.2105 0.8756 6.750 0.7381 0.00932 0.00379 0.0340 0.2069 0.8801 7.000 0.7653 0.00948 0.00396 0.0340 0.2023 0.8843 7.250 0.7920 0.00968 0.00414 0.0340 0.1971 0.8883 7.500 0.8190 0.00985 0.00431 0.0340 0.1927 0.8918 7.750 0.8452 0.01003 0.00450 0.0341 0.1873 0.8954 8.000 0.8708 0.01026 0.00472 0.0343 0.1814 0.8993 8.250 0.8972 0.01043 0.00491 0.0344 0.1780 0.9034 8.500 0.9234 0.01063 0.00512 0.0345 0.1740 0.9073 8.750 0.9483 0.01088 0.00536 0.0347 0.1689 0.9108 9.000 0.9733 0.01108 0.00559 0.0350 0.1653 0.9149 9.250 0.9983 0.01129 0.00582 0.0353 0.1615 0.9194 9.500 1.0227 0.01154 0.00607 0.0356 0.1573 0.9238 9.750 1.0462 0.01181 0.00635 0.0361 0.1529 0.9279 10.000 1.0700 0.01203 0.00661 0.0366 0.1499 0.9326 10.250 1.0928 0.01229 0.00689 0.0371 0.1457 0.9381 10.500 1.1142 0.01263 0.00722 0.0379 0.1409 0.9435 10.750 1.1366 0.01287 0.00751 0.0385 0.1379 0.9492 11.000 1.1580 0.01317 0.00783 0.0392 0.1338 0.9559 11.250 1.1795 0.01357 0.00823 0.0397 0.1289 0.9630 11.500 1.2032 0.01391 0.00861 0.0399 0.1251 0.9706 11.750 1.2304 0.01435 0.00906 0.0391 0.1201 0.9765 12.000 1.2571 0.01488 0.00958 0.0382 0.1151 0.9830 12.250 1.2856 0.01539 0.01011 0.0369 0.1101 0.9886 12.500 1.3098 0.01607 0.01078 0.0361 0.1048 1.0000 12.750 1.3154 0.01660 0.01134 0.0389 0.1016 1.0000 13.000 1.3223 0.01735 0.01209 0.0410 0.0975 1.0000 13.250 1.3294 0.01825 0.01301 0.0427 0.0936 1.0000 13.500 1.3377 0.01921 0.01398 0.0439 0.0893 1.0000 13.750 1.3432 0.02045 0.01522 0.0452 0.0850 1.0000 14.000 1.3515 0.02161 0.01642 0.0460 0.0817 1.0000 14.250 1.3576 0.02301 0.01784 0.0468 0.0783 1.0000 14.500 1.3620 0.02463 0.01948 0.0474 0.0753 1.0000 14.750 1.3688 0.02613 0.02103 0.0478 0.0730 1.0000 15.000 1.3742 0.02783 0.02278 0.0480 0.0709 1.0000 15.250 1.3755 0.02993 0.02491 0.0482 0.0683 1.0000 15.500 1.3770 0.03209 0.02712 0.0482 0.0661 1.0000 15.750 1.3793 0.03425 0.02934 0.0480 0.0641 1.0000 16.000 1.3788 0.03674 0.03189 0.0478 0.0622 1.0000 16.250 1.3753 0.03958 0.03478 0.0473 0.0603 1.0000 16.500 1.3709 0.04258 0.03783 0.0468 0.0587 1.0000 16.750 1.3695 0.04539 0.04072 0.0461 0.0574 1.0000 17.000 1.3643 0.04870 0.04410 0.0453 0.0555 1.0000 17.250 1.3584 0.05217 0.04764 0.0442 0.0545 1.0000 17.500 1.3458 0.05651 0.05203 0.0429 0.0523 1.0000 17.750 1.3385 0.06033 0.05594 0.0416 0.0517 1.0000 18.000 1.3315 0.06419 0.05987 0.0402 0.0504 1.0000 18.250 1.3224 0.06836 0.06412 0.0387 0.0492 1.0000 18.500 1.3117 0.07282 0.06867 0.0370 0.0481 1.0000 18.750 1.2976 0.07783 0.07374 0.0350 0.0466 1.0000 19.000 1.2843 0.08282 0.07881 0.0329 0.0457 1.0000