XFOIL Version 6.96 Calculated polar for: MB253515 15.0% smoothed 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -11.750 -0.3184 0.09344 0.09137 -0.0517 1.0000 0.0268 -11.500 -0.5450 0.06339 0.06088 -0.0715 1.0000 0.0185 -11.250 -0.5697 0.05837 0.05577 -0.0735 1.0000 0.0184 -11.000 -0.5943 0.05442 0.05170 -0.0735 1.0000 0.0184 -10.750 -0.6158 0.05155 0.04874 -0.0716 1.0000 0.0183 -10.500 -0.6488 0.04899 0.04606 -0.0665 1.0000 0.0184 -10.250 -0.6589 0.04423 0.04101 -0.0667 0.9855 0.0183 -10.000 -0.6577 0.03878 0.03511 -0.0676 0.9711 0.0184 -9.750 -0.6474 0.03403 0.02979 -0.0684 0.9585 0.0187 -9.500 -0.6336 0.02920 0.02443 -0.0694 0.9450 0.0195 -9.250 -0.6057 0.02738 0.02245 -0.0710 0.9320 0.0200 -9.000 -0.5775 0.02692 0.02195 -0.0721 0.9172 0.0208 -8.750 -0.5578 0.02565 0.02046 -0.0714 0.9016 0.0215 -8.500 -0.5397 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0.00763 0.00255 -0.0332 0.6270 0.8670 1.250 0.3373 0.00769 0.00256 -0.0329 0.6215 0.8786 1.500 0.3645 0.00770 0.00262 -0.0327 0.6149 0.8892 1.750 0.3925 0.00774 0.00266 -0.0327 0.6087 0.8994 2.000 0.4196 0.00779 0.00272 -0.0326 0.6025 0.9107 2.250 0.4485 0.00785 0.00279 -0.0328 0.5953 0.9212 2.500 0.4802 0.00795 0.00288 -0.0337 0.5883 0.9295 2.750 0.5080 0.00802 0.00295 -0.0337 0.5808 0.9396 3.000 0.5446 0.00814 0.00306 -0.0357 0.5731 0.9441 3.250 0.5783 0.00825 0.00317 -0.0370 0.5642 0.9502 3.500 0.6106 0.00836 0.00328 -0.0381 0.5552 0.9563 3.750 0.6490 0.00851 0.00340 -0.0406 0.5459 0.9590 4.000 0.6861 0.00864 0.00354 -0.0428 0.5347 0.9624 4.250 0.7170 0.00878 0.00367 -0.0436 0.5234 0.9686 4.500 0.7540 0.00893 0.00381 -0.0459 0.5110 0.9713 4.750 0.7910 0.00910 0.00396 -0.0481 0.4973 0.9741 5.000 0.8255 0.00928 0.00412 -0.0499 0.4819 0.9782 5.250 0.8571 0.00949 0.00431 -0.0510 0.4660 0.9833 5.500 0.8931 0.00974 0.00449 -0.0532 0.4445 0.9862 5.750 0.9263 0.01008 0.00471 -0.0549 0.4157 0.9903 6.000 0.9587 0.01043 0.00498 -0.0565 0.3910 0.9944 6.250 0.9935 0.01078 0.00524 -0.0586 0.3697 0.9978 6.500 1.0215 0.01110 0.00550 -0.0593 0.3494 1.0000 6.750 1.0312 0.01134 0.00570 -0.0561 0.3355 1.0000 7.000 1.0403 0.01161 0.00594 -0.0528 0.3198 1.0000 7.250 1.0489 0.01192 0.00619 -0.0493 0.3024 1.0000 7.500 1.0553 0.01231 0.00649 -0.0455 0.2810 1.0000 7.750 1.0567 0.01288 0.00688 -0.0408 0.2427 1.0000 8.000 1.0386 0.01395 0.00753 -0.0326 0.1770 1.0000 8.250 1.0082 0.01548 0.00858 -0.0227 0.0975 1.0000 8.500 0.9920 0.01702 0.00982 -0.0160 0.0455 1.0000 8.750 0.9932 0.01805 0.01081 -0.0122 0.0320 1.0000 9.000 0.9975 0.01905 0.01184 -0.0092 0.0273 1.0000 9.250 1.0069 0.01986 0.01271 -0.0070 0.0251 1.0000 9.500 1.0146 0.02083 0.01373 -0.0048 0.0234 1.0000 9.750 1.0138 0.02241 0.01537 -0.0019 0.0215 1.0000 10.000 1.0259 0.02326 0.01628 -0.0006 0.0205 1.0000 10.250 1.0334 0.02446 0.01755 0.0011 0.0196 1.0000 10.500 1.0387 0.02589 0.01904 0.0028 0.0188 1.0000 10.750 1.0454 0.02727 0.02047 0.0041 0.0180 1.0000 11.000 1.0470 0.02910 0.02238 0.0057 0.0175 1.0000 11.250 1.0420 0.03155 0.02491 0.0075 0.0169 1.0000 11.500 1.0415 0.03373 0.02718 0.0089 0.0164 1.0000 11.750 1.0452 0.03563 0.02915 0.0099 0.0161 1.0000 12.000 1.0499 0.03747 0.03107 0.0107 0.0157 1.0000 12.250 1.0525 0.03954 0.03321 0.0116 0.0154 1.0000 12.500 1.0558 0.04160 0.03534 0.0123 0.0151 1.0000 12.750 1.0595 0.04367 0.03748 0.0130 0.0146 1.0000 13.000 1.0626 0.04580 0.03968 0.0137 0.0144 1.0000 13.250 1.0671 0.04787 0.04179 0.0141 0.0139 1.0000 13.500 1.0703 0.05008 0.04402 0.0146 0.0134 1.0000 13.750 1.0728 0.05219 0.04616 0.0155 0.0131 1.0000 14.000 1.0777 0.05397 0.04799 0.0171 0.0127 1.0000 14.250 1.0861 0.05563 0.04972 0.0178 0.0127 1.0000 14.500 1.0920 0.05776 0.05197 0.0179 0.0124 1.0000 14.750 1.0999 0.05952 0.05383 0.0187 0.0122 1.0000 15.000 1.1058 0.06163 0.05604 0.0191 0.0120 1.0000 15.250 1.1131 0.06355 0.05807 0.0199 0.0118 1.0000 15.500 1.1178 0.06588 0.06052 0.0202 0.0115 1.0000 15.750 1.1230 0.06814 0.06292 0.0209 0.0115 1.0000 16.000 1.1252 0.07087 0.06578 0.0212 0.0114 1.0000 16.250 1.1255 0.07389 0.06896 0.0213 0.0114 1.0000 16.500 1.1235 0.07725 0.07245 0.0209 0.0111 1.0000 16.750 1.1204 0.08077 0.07611 0.0203 0.0110 1.0000 17.000 1.1174 0.08435 0.07980 0.0195 0.0107 1.0000 17.250 1.1011 0.09023 0.08600 0.0189 0.0112 1.0000 17.500 1.0928 0.09480 0.09071 0.0173 0.0110 1.0000 17.750 1.1075 0.09556 0.09131 0.0161 0.0103 1.0000 18.000 1.0965 0.10068 0.09660 0.0145 0.0103 1.0000 18.250 1.0851 0.10603 0.10212 0.0124 0.0103 1.0000 18.500 1.0454 0.11697 0.11348 0.0078 0.0107 1.0000 18.750 1.0054 0.12868 0.12552 0.0022 0.0111 1.0000