XFOIL Version 6.96 Calculated polar for: WB-135/35 13.5% 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 ------ -------- --------- --------- -------- -------- -------- -12.250 -0.6652 0.05261 0.04947 -0.0799 1.0000 0.0136 -12.000 -0.6887 0.04675 0.04339 -0.0843 1.0000 0.0134 -11.750 -0.7052 0.04299 0.03950 -0.0865 1.0000 0.0133 -11.500 -0.7278 0.04097 0.03740 -0.0847 1.0000 0.0132 -11.250 -0.7500 0.03934 0.03567 -0.0807 0.9984 0.0133 -11.000 -0.7350 0.03490 0.03093 -0.0851 0.9921 0.0134 -10.750 -0.7160 0.03172 0.02752 -0.0878 0.9864 0.0136 -10.500 -0.6920 0.02900 0.02456 -0.0903 0.9824 0.0137 -10.250 -0.6683 0.02740 0.02285 -0.0916 0.9759 0.0142 -10.000 -0.6402 0.02546 0.02075 -0.0935 0.9721 0.0144 -9.750 -0.6123 0.02396 0.01912 -0.0949 0.9674 0.0149 -9.500 -0.5842 0.02252 0.01753 -0.0962 0.9616 0.0154 -9.250 -0.5522 0.02115 0.01600 -0.0980 0.9575 0.0159 -9.000 -0.5232 0.02020 0.01490 -0.0989 0.9499 0.0166 -8.750 -0.4944 0.01861 0.01317 -0.1001 0.9430 0.0174 -8.500 -0.4710 0.01730 0.01179 -0.1000 0.9327 0.0180 -8.250 -0.4444 0.01644 0.01085 -0.1003 0.9235 0.0188 -8.000 -0.4197 0.01574 0.01004 -0.1000 0.9131 0.0198 -7.750 -0.3973 0.01511 0.00931 -0.0992 0.9016 0.0206 -7.500 -0.3737 0.01460 0.00868 -0.0984 0.8909 0.0215 -7.250 -0.3537 0.01373 0.00767 -0.0972 0.8801 0.0231 -7.000 -0.3318 0.01319 0.00707 -0.0961 0.8689 0.0247 -6.750 -0.3083 0.01278 0.00655 -0.0953 0.8586 0.0267 -6.500 -0.2848 0.01228 0.00592 -0.0945 0.8495 0.0290 -6.250 -0.2621 0.01175 0.00531 -0.0935 0.8394 0.0333 -6.000 -0.2388 0.01123 0.00473 -0.0926 0.8301 0.0427 -5.750 -0.2203 0.01011 0.00404 -0.0913 0.8213 0.1351 -5.500 -0.1948 0.00990 0.00387 -0.0908 0.8125 0.1633 -5.250 -0.1680 0.00980 0.00371 -0.0905 0.8054 0.1786 -5.000 -0.1417 0.00970 0.00359 -0.0901 0.7973 0.1910 -4.500 -0.0885 0.00952 0.00334 -0.0895 0.7831 0.2133 -4.250 -0.0617 0.00944 0.00322 -0.0892 0.7767 0.2248 -4.000 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0.00235 -0.0819 0.6422 0.5276 1.250 0.5220 0.00836 0.00238 -0.0814 0.6356 0.5516 1.500 0.5472 0.00831 0.00241 -0.0808 0.6279 0.5776 1.750 0.5721 0.00825 0.00244 -0.0801 0.6200 0.6078 2.000 0.5960 0.00815 0.00247 -0.0792 0.6114 0.6478 2.250 0.6164 0.00787 0.00252 -0.0775 0.6028 0.7359 2.500 0.7314 0.00760 0.00274 -0.0965 0.5854 0.9962 2.750 0.7645 0.00770 0.00278 -0.0977 0.5705 1.0000 3.000 0.7870 0.00782 0.00284 -0.0966 0.5532 1.0000 3.250 0.8087 0.00798 0.00291 -0.0953 0.5315 1.0000 3.500 0.8286 0.00821 0.00301 -0.0936 0.4999 1.0000 3.750 0.8449 0.00861 0.00318 -0.0913 0.4548 1.0000 4.000 0.8604 0.00909 0.00343 -0.0890 0.4137 1.0000 4.500 0.8970 0.00986 0.00394 -0.0854 0.3692 1.0000 4.750 0.9165 0.01019 0.00419 -0.0838 0.3553 1.0000 5.250 0.9572 0.01077 0.00467 -0.0809 0.3315 1.0000 5.500 0.9776 0.01104 0.00490 -0.0795 0.3216 1.0000 5.750 0.9975 0.01133 0.00515 -0.0781 0.3127 1.0000 6.000 1.0188 0.01155 0.00538 -0.0769 0.3047 1.0000 6.500 1.0594 0.01206 0.00587 -0.0741 0.2883 1.0000 6.750 1.0781 0.01236 0.00614 -0.0724 0.2802 1.0000 7.000 1.0981 0.01260 0.00638 -0.0710 0.2696 1.0000 7.250 1.1169 0.01288 0.00664 -0.0694 0.2565 1.0000 7.500 1.1337 0.01322 0.00692 -0.0675 0.2398 1.0000 7.750 1.1461 0.01365 0.00723 -0.0647 0.2129 1.0000 8.000 1.1506 0.01442 0.00772 -0.0607 0.1704 1.0000 8.250 1.1415 0.01594 0.00878 -0.0548 0.1020 1.0000 8.500 1.1262 0.01805 0.01041 -0.0486 0.0277 1.0000 8.750 1.1371 0.01886 0.01122 -0.0462 0.0216 1.0000 9.000 1.1489 0.01964 0.01206 -0.0441 0.0195 1.0000 9.250 1.1599 0.02052 0.01303 -0.0419 0.0179 1.0000 9.500 1.1722 0.02135 0.01393 -0.0401 0.0172 1.0000 9.750 1.1835 0.02226 0.01492 -0.0382 0.0167 1.0000 10.000 1.1923 0.02338 0.01612 -0.0362 0.0159 1.0000 10.250 1.2010 0.02454 0.01736 -0.0344 0.0155 1.0000 10.500 1.2080 0.02587 0.01878 -0.0325 0.0152 1.0000 10.750 1.2105 0.02759 0.02058 -0.0305 0.0146 1.0000 11.000 1.2088 0.02973 0.02282 -0.0284 0.0140 1.0000 11.250 1.2063 0.03205 0.02524 -0.0265 0.0138 1.0000 11.500 1.2089 0.03403 0.02731 -0.0252 0.0134 1.0000 11.750 1.2122 0.03603 0.02940 -0.0241 0.0132 1.0000 12.000 1.2156 0.03806 0.03152 -0.0231 0.0130 1.0000 12.250 1.2157 0.04048 0.03402 -0.0220 0.0128 1.0000 12.500 1.2172 0.04281 0.03644 -0.0212 0.0125 1.0000 12.750 1.2176 0.04533 0.03904 -0.0205 0.0125 1.0000 13.000 1.2175 0.04796 0.04176 -0.0198 0.0124 1.0000 13.250 1.2175 0.05063 0.04451 -0.0193 0.0121 1.0000 13.500 1.2170 0.05340 0.04736 -0.0187 0.0120 1.0000 13.750 1.2174 0.05612 0.05014 -0.0183 0.0117 1.0000 14.000 1.2185 0.05881 0.05289 -0.0179 0.0115 1.0000 14.250 1.2204 0.06140 0.05554 -0.0176 0.0114 1.0000 14.500 1.2226 0.06396 0.05816 -0.0172 0.0113 1.0000 14.750 1.2251 0.06651 0.06076 -0.0168 0.0111 1.0000 15.000 1.2287 0.06878 0.06303 -0.0162 0.0107 1.0000 15.250 1.2376 0.07017 0.06441 -0.0146 0.0105 1.0000 15.500 1.2585 0.07017 0.06441 -0.0110 0.0102 1.0000 15.750 1.2489 0.07449 0.06892 -0.0126 0.0100 1.0000 16.000 1.2490 0.07762 0.07218 -0.0129 0.0100 1.0000 16.250 1.2537 0.08005 0.07471 -0.0125 0.0100 1.0000 16.500 1.2509 0.08370 0.07849 -0.0133 0.0099 1.0000 16.750 1.2499 0.08710 0.08202 -0.0138 0.0098 1.0000 17.000 1.2480 0.09071 0.08577 -0.0143 0.0098 1.0000 17.250 1.2456 0.09441 0.08961 -0.0148 0.0098 1.0000 17.500 1.2472 0.09747 0.09278 -0.0144 0.0100 1.0000 17.750 1.2412 0.10186 0.09731 -0.0156 0.0100 1.0000