XFOIL Version 6.96 Calculated polar for: GIII BL369 AIRFOIL 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 ------ -------- --------- --------- -------- -------- -------- -9.250 -0.8469 0.02161 0.01760 -0.0251 1.0000 0.0104 -9.000 -0.8319 0.01893 0.01454 -0.0237 1.0000 0.0106 -8.750 -0.8115 0.01767 0.01311 -0.0227 1.0000 0.0107 -8.500 -0.7900 0.01678 0.01210 -0.0218 1.0000 0.0109 -8.250 -0.7682 0.01605 0.01127 -0.0209 1.0000 0.0110 -8.000 -0.7463 0.01540 0.01054 -0.0199 1.0000 0.0112 -7.750 -0.7223 0.01476 0.00982 -0.0193 0.9994 0.0113 -7.500 -0.6919 0.01413 0.00910 -0.0201 0.9968 0.0115 -7.250 -0.6610 0.01350 0.00839 -0.0210 0.9943 0.0117 -7.000 -0.6308 0.01292 0.00773 -0.0217 0.9901 0.0119 -6.750 -0.5989 0.01236 0.00710 -0.0228 0.9858 0.0121 -6.500 -0.5684 0.01184 0.00651 -0.0235 0.9789 0.0123 -6.250 -0.5376 0.01135 0.00596 -0.0242 0.9714 0.0126 -6.000 -0.5075 0.01091 0.00545 -0.0248 0.9626 0.0129 -5.750 -0.4794 0.01053 0.00501 -0.0248 0.9512 0.0131 -5.500 -0.4528 0.01016 0.00459 -0.0246 0.9387 0.0135 -5.250 -0.4265 0.00993 0.00432 -0.0241 0.9243 0.0141 -5.000 -0.4004 0.00975 0.00410 -0.0237 0.9091 0.0147 -4.750 -0.3742 0.00955 0.00385 -0.0232 0.8954 0.0153 -4.500 -0.3479 0.00934 0.00358 -0.0228 0.8838 0.0159 -4.250 -0.3215 0.00915 0.00332 -0.0224 0.8720 0.0165 -4.000 -0.2948 0.00894 0.00308 -0.0221 0.8601 0.0173 -3.750 -0.2677 0.00882 0.00295 -0.0219 0.8489 0.0181 -3.500 -0.2406 0.00870 0.00279 -0.0217 0.8374 0.0190 -3.250 -0.2136 0.00858 0.00262 -0.0214 0.8249 0.0199 -3.000 -0.1864 0.00846 0.00246 -0.0212 0.8125 0.0205 -2.750 -0.1595 0.00828 0.00223 -0.0209 0.8003 0.0214 -2.500 -0.1324 0.00815 0.00208 -0.0207 0.7878 0.0224 -2.250 -0.1052 0.00807 0.00197 -0.0205 0.7753 0.0233 -2.000 -0.0779 0.00800 0.00187 -0.0203 0.7628 0.0246 -1.750 -0.0507 0.00796 0.00178 -0.0201 0.7478 0.0256 -1.500 -0.0235 0.00790 0.00166 -0.0199 0.7309 0.0261 -1.250 0.0034 0.00775 0.00145 -0.0196 0.7143 0.0276 -1.000 0.0306 0.00767 0.00134 -0.0194 0.6986 0.0290 -0.750 0.0579 0.00762 0.00124 -0.0192 0.6805 0.0302 -0.500 0.0851 0.00760 0.00116 -0.0190 0.6573 0.0314 -0.250 0.1119 0.00764 0.00108 -0.0187 0.6253 0.0326 0.000 0.1385 0.00772 0.00103 -0.0184 0.5858 0.0340 0.250 0.1651 0.00778 0.00100 -0.0181 0.5502 0.0387 0.500 0.1922 0.00781 0.00098 -0.0180 0.5251 0.0476 0.750 0.2123 0.00652 0.00088 -0.0172 0.5031 0.4976 1.000 0.2335 0.00592 0.00091 -0.0160 0.4761 0.7204 1.250 0.2589 0.00592 0.00096 -0.0155 0.4507 0.7723 1.500 0.2846 0.00595 0.00102 -0.0149 0.4254 0.8094 1.750 0.3100 0.00597 0.00108 -0.0143 0.3982 0.8454 2.000 0.3355 0.00605 0.00115 -0.0137 0.3713 0.8743 2.250 0.3608 0.00624 0.00124 -0.0131 0.3301 0.8956 2.500 0.3856 0.00650 0.00137 -0.0124 0.2830 0.9206 2.750 0.4114 0.00679 0.00152 -0.0120 0.2354 0.9458 3.000 0.4397 0.00711 0.00167 -0.0122 0.1931 0.9582 3.250 0.4698 0.00736 0.00180 -0.0128 0.1666 0.9678 3.500 0.5003 0.00761 0.00194 -0.0134 0.1416 0.9760 3.750 0.5318 0.00790 0.00210 -0.0144 0.1151 0.9819 4.000 0.5629 0.00817 0.00227 -0.0153 0.0955 0.9872 4.250 0.5947 0.00840 0.00243 -0.0163 0.0831 0.9914 4.500 0.6260 0.00862 0.00260 -0.0172 0.0737 0.9952 4.750 0.6583 0.00882 0.00277 -0.0183 0.0662 0.9981 5.000 0.6878 0.00906 0.00296 -0.0188 0.0585 1.0000 5.250 0.7121 0.00928 0.00314 -0.0181 0.0524 1.0000 5.500 0.7365 0.00951 0.00334 -0.0175 0.0469 1.0000 5.750 0.7610 0.00975 0.00355 -0.0169 0.0424 1.0000 6.000 0.7858 0.00998 0.00378 -0.0164 0.0392 1.0000 6.250 0.8109 0.01021 0.00400 -0.0159 0.0373 1.0000 6.500 0.8358 0.01047 0.00425 -0.0154 0.0347 1.0000 6.750 0.8607 0.01077 0.00454 -0.0149 0.0318 1.0000 7.000 0.8862 0.01100 0.00478 -0.0146 0.0309 1.0000 7.250 0.9115 0.01125 0.00505 -0.0142 0.0298 1.0000 7.500 0.9367 0.01153 0.00534 -0.0138 0.0287 1.0000 7.750 0.9618 0.01183 0.00565 -0.0135 0.0275 1.0000 8.000 0.9866 0.01218 0.00601 -0.0131 0.0262 1.0000 8.250 1.0114 0.01252 0.00638 -0.0127 0.0252 1.0000 8.500 1.0366 0.01281 0.00670 -0.0123 0.0246 1.0000 8.750 1.0616 0.01311 0.00704 -0.0120 0.0238 1.0000 9.000 1.0864 0.01344 0.00739 -0.0116 0.0228 1.0000 9.250 1.1109 0.01379 0.00775 -0.0113 0.0217 1.0000 9.500 1.1348 0.01422 0.00819 -0.0108 0.0204 1.0000 9.750 1.1591 0.01459 0.00861 -0.0104 0.0197 1.0000 10.000 1.1833 0.01496 0.00902 -0.0101 0.0189 1.0000 10.250 1.2071 0.01536 0.00944 -0.0096 0.0179 1.0000 10.500 1.2306 0.01579 0.00990 -0.0092 0.0170 1.0000 10.750 1.2532 0.01632 0.01045 -0.0086 0.0159 1.0000 11.000 1.2763 0.01677 0.01096 -0.0081 0.0154 1.0000 11.250 1.2989 0.01725 0.01149 -0.0076 0.0147 1.0000 11.500 1.3210 0.01777 0.01206 -0.0070 0.0140 1.0000 11.750 1.3425 0.01834 0.01266 -0.0064 0.0134 1.0000 12.000 1.3631 0.01898 0.01334 -0.0057 0.0129 1.0000 12.250 1.3829 0.01967 0.01410 -0.0048 0.0124 1.0000 12.500 1.4030 0.02029 0.01479 -0.0041 0.0121 1.0000 12.750 1.4224 0.02095 0.01552 -0.0032 0.0118 1.0000 13.000 1.4409 0.02164 0.01630 -0.0023 0.0115 1.0000 13.250 1.4584 0.02239 0.01712 -0.0013 0.0112 1.0000 13.500 1.4747 0.02319 0.01799 -0.0002 0.0109 1.0000 13.750 1.4891 0.02404 0.01891 0.0012 0.0106 1.0000 14.000 1.5005 0.02498 0.01992 0.0029 0.0104 1.0000 14.250 1.5095 0.02605 0.02108 0.0048 0.0101 1.0000 14.500 1.5159 0.02734 0.02246 0.0066 0.0099 1.0000 14.750 1.5209 0.02879 0.02401 0.0083 0.0097 1.0000 15.000 1.5281 0.03015 0.02549 0.0095 0.0095 1.0000 15.250 1.5340 0.03171 0.02716 0.0105 0.0094 1.0000 15.500 1.5383 0.03352 0.02908 0.0113 0.0093 1.0000 15.750 1.5413 0.03559 0.03126 0.0118 0.0091 1.0000 16.000 1.5424 0.03801 0.03380 0.0119 0.0090 1.0000 16.250 1.5416 0.04079 0.03670 0.0116 0.0089 1.0000 16.500 1.5386 0.04404 0.04008 0.0109 0.0088 1.0000 16.750 1.5331 0.04780 0.04397 0.0097 0.0087 1.0000 17.000 1.5246 0.05224 0.04855 0.0079 0.0086 1.0000 17.250 1.5125 0.05747 0.05392 0.0054 0.0085 1.0000 17.500 1.4961 0.06367 0.06027 0.0022 0.0085 1.0000 17.750 1.4738 0.07098 0.06774 -0.0016 0.0085 1.0000 18.000 1.4450 0.07971 0.07664 -0.0063 0.0085 1.0000 18.250 1.4072 0.09038 0.08750 -0.0120 0.0086 1.0000 18.500 1.3600 0.10324 0.10055 -0.0188 0.0087 1.0000 18.750 1.3045 0.11805 0.11555 -0.0266 0.0088 1.0000 19.000 1.2496 0.13332 0.13099 -0.0349 0.0090 1.0000