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 = 0.100 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -11.500 -0.4230 0.09564 0.09070 -0.0535 1.0000 0.0313 -11.250 -0.4413 0.08642 0.08155 -0.0587 1.0000 0.0310 -10.750 -0.5538 0.06523 0.05991 -0.0716 1.0000 0.0281 -10.500 -0.5746 0.06232 0.05693 -0.0698 1.0000 0.0280 -10.250 -0.5963 0.06011 0.05466 -0.0665 1.0000 0.0280 -10.000 -0.6233 0.05871 0.05323 -0.0609 1.0000 0.0280 -9.750 -0.6444 0.05690 0.05133 -0.0563 0.9968 0.0280 -9.500 -0.6402 0.05237 0.04649 -0.0579 0.9827 0.0286 -9.250 -0.6195 0.05003 0.04414 -0.0600 0.9738 0.0301 -9.000 -0.6047 0.04726 0.04111 -0.0610 0.9629 0.0314 -8.750 -0.5916 0.04412 0.03756 -0.0613 0.9519 0.0325 -8.500 -0.5764 0.04091 0.03387 -0.0613 0.9419 0.0334 -8.250 -0.5560 0.03807 0.03047 -0.0616 0.9338 0.0347 -8.000 -0.5384 0.03639 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0.01596 0.00802 -0.0455 0.7780 0.5885 -2.750 -0.0705 0.01591 0.00809 -0.0439 0.7717 0.6493 -2.500 -0.0451 0.01593 0.00818 -0.0425 0.7671 0.7069 -2.250 -0.0243 0.01612 0.00842 -0.0405 0.7599 0.7500 -2.000 0.0025 0.01622 0.00845 -0.0397 0.7546 0.7779 -1.750 0.0315 0.01635 0.00849 -0.0395 0.7490 0.7978 -1.500 0.0585 0.01643 0.00849 -0.0391 0.7426 0.8126 -1.250 0.0889 0.01646 0.00840 -0.0394 0.7378 0.8267 -1.000 0.1149 0.01658 0.00845 -0.0390 0.7309 0.8406 -0.750 0.1474 0.01665 0.00842 -0.0396 0.7250 0.8523 -0.500 0.1799 0.01672 0.00840 -0.0404 0.7183 0.8631 -0.250 0.2105 0.01676 0.00836 -0.0408 0.7105 0.8745 0.000 0.2402 0.01679 0.00830 -0.0410 0.7031 0.8863 0.250 0.2775 0.01685 0.00829 -0.0428 0.6953 0.8946 0.500 0.3106 0.01691 0.00828 -0.0438 0.6882 0.9043 0.750 0.3444 0.01697 0.00829 -0.0451 0.6808 0.9134 1.000 0.3808 0.01702 0.00828 -0.0469 0.6740 0.9207 1.250 0.4140 0.01708 0.00832 -0.0481 0.6663 0.9291 1.500 0.4517 0.01711 0.00829 -0.0503 0.6596 0.9353 1.750 0.4862 0.01717 0.00835 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0.9592 0.01957 0.01130 -0.0428 0.4564 1.0000 7.000 0.9747 0.01992 0.01172 -0.0408 0.4464 1.0000 7.250 0.9921 0.02025 0.01209 -0.0390 0.4377 1.0000 7.500 1.0069 0.02061 0.01253 -0.0368 0.4269 1.0000 7.750 1.0184 0.02097 0.01291 -0.0341 0.4128 1.0000 8.000 1.0252 0.02134 0.01323 -0.0305 0.3939 1.0000 8.250 1.0270 0.02181 0.01365 -0.0261 0.3717 1.0000 8.500 1.0263 0.02237 0.01409 -0.0215 0.3500 1.0000 8.750 1.0250 0.02299 0.01470 -0.0169 0.3303 1.0000 9.000 1.0249 0.02373 0.01541 -0.0128 0.3102 1.0000 9.250 1.0243 0.02463 0.01633 -0.0091 0.2869 1.0000 9.500 1.0205 0.02583 0.01745 -0.0054 0.2543 1.0000 9.750 1.0090 0.02765 0.01899 -0.0013 0.1998 1.0000 10.000 0.9843 0.03074 0.02142 0.0029 0.1138 1.0000 10.250 0.9650 0.03399 0.02422 0.0061 0.0675 1.0000 10.500 0.9562 0.03668 0.02681 0.0083 0.0529 1.0000 10.750 0.9535 0.03900 0.02922 0.0099 0.0461 1.0000 11.000 0.9485 0.04163 0.03191 0.0113 0.0420 1.0000 11.250 0.9448 0.04426 0.03466 0.0123 0.0391 1.0000 11.500 0.9419 0.04691 0.03745 0.0131 0.0360 1.0000 11.750 0.9383 0.04973 0.04040 0.0137 0.0346 1.0000 12.000 0.9314 0.05302 0.04377 0.0141 0.0328 1.0000 12.250 0.9233 0.05655 0.04739 0.0144 0.0315 1.0000 12.500 0.9207 0.05962 0.05061 0.0145 0.0307 1.0000 12.750 0.9187 0.06265 0.05378 0.0146 0.0296 1.0000 13.000 0.9184 0.06548 0.05672 0.0148 0.0287 1.0000 13.250 0.9201 0.06807 0.05942 0.0150 0.0275 1.0000 13.500 0.9239 0.07038 0.06177 0.0153 0.0264 1.0000 13.750 0.9272 0.07267 0.06403 0.0155 0.0248 1.0000 14.000 0.9386 0.07385 0.06525 0.0166 0.0238 1.0000 14.250 0.9528 0.07486 0.06635 0.0177 0.0229 1.0000 14.500 0.9685 0.07581 0.06739 0.0190 0.0221 1.0000 14.750 0.9833 0.07707 0.06876 0.0200 0.0214 1.0000 15.000 0.9945 0.07890 0.07072 0.0206 0.0206 1.0000 15.250 1.0023 0.08119 0.07318 0.0208 0.0200 1.0000 15.500 1.0057 0.08396 0.07605 0.0205 0.0192 1.0000 15.750 1.0105 0.08664 0.07882 0.0203 0.0186 1.0000 16.000 1.0177 0.08926 0.08151 0.0205 0.0180 1.0000 16.250 1.0149 0.09317 0.08563 0.0197 0.0177 1.0000 16.500 1.0098 0.09748 0.09018 0.0186 0.0176 1.0000 16.750 1.0045 0.10187 0.09478 0.0172 0.0175 1.0000 17.000 0.9950 0.10703 0.10018 0.0152 0.0174 1.0000 17.250 0.9841 0.11253 0.10590 0.0128 0.0174 1.0000 17.500 0.9723 0.11837 0.11195 0.0101 0.0174 1.0000 17.750 0.9591 0.12466 0.11844 0.0068 0.0174 1.0000 18.000 0.9456 0.13127 0.12523 0.0032 0.0174 1.0000 18.250 0.9287 0.13895 0.13310 -0.0012 0.0174 1.0000 18.500 0.9145 0.14636 0.14066 -0.0056 0.0176 1.0000 18.750 0.9001 0.15416 0.14859 -0.0103 0.0177 1.0000 19.000 0.8826 0.16329 0.15783 -0.0158 0.0178 1.0000 19.250 0.8672 0.17257 0.16718 -0.0212 0.0179 1.0000