XFOIL Version 6.96 Calculated polar for: GIII BL430 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 ------ -------- --------- --------- -------- -------- -------- -10.750 -0.5986 0.12005 0.11829 0.0226 1.0000 0.0099 -10.500 -0.5957 0.11607 0.11431 0.0208 1.0000 0.0100 -9.000 -0.8337 0.01803 0.01349 -0.0218 1.0000 0.0137 -8.750 -0.8099 0.01712 0.01249 -0.0212 1.0000 0.0140 -8.500 -0.7849 0.01659 0.01192 -0.0208 1.0000 0.0142 -8.250 -0.7598 0.01610 0.01139 -0.0203 1.0000 0.0145 -8.000 -0.7348 0.01559 0.01083 -0.0199 1.0000 0.0148 -7.750 -0.7099 0.01504 0.01022 -0.0193 1.0000 0.0151 -7.500 -0.6853 0.01444 0.00955 -0.0188 1.0000 0.0154 -7.250 -0.6548 0.01374 0.00875 -0.0195 0.9927 0.0159 -7.000 -0.6224 0.01306 0.00796 -0.0206 0.9793 0.0163 -6.750 -0.5897 0.01251 0.00733 -0.0217 0.9630 0.0167 -6.500 -0.5596 0.01223 0.00702 -0.0221 0.9441 0.0170 -6.250 -0.5326 0.01204 0.00678 -0.0218 0.9234 0.0174 -6.000 -0.5067 0.01184 0.00651 -0.0212 0.9038 0.0177 -5.750 -0.4808 0.01160 0.00618 -0.0206 0.8866 0.0182 -5.500 -0.4547 0.01131 0.00580 -0.0201 0.8715 0.0186 -5.250 -0.4284 0.01101 0.00540 -0.0197 0.8586 0.0191 -5.000 -0.4019 0.01075 0.00505 -0.0193 0.8469 0.0195 -4.750 -0.3751 0.01046 0.00472 -0.0190 0.8359 0.0200 -4.500 -0.3478 0.01032 0.00456 -0.0187 0.8255 0.0205 -4.250 -0.3205 0.01017 0.00437 -0.0184 0.8146 0.0209 -4.000 -0.2932 0.01000 0.00416 -0.0182 0.8039 0.0215 -3.750 -0.2659 0.00982 0.00393 -0.0179 0.7931 0.0221 -3.500 -0.2388 0.00960 0.00365 -0.0176 0.7812 0.0226 -3.250 -0.2117 0.00939 0.00337 -0.0173 0.7685 0.0230 -3.000 -0.1848 0.00914 0.00307 -0.0170 0.7546 0.0235 -2.750 -0.1576 0.00898 0.00288 -0.0167 0.7395 0.0241 -2.500 -0.1303 0.00885 0.00270 -0.0165 0.7223 0.0246 -2.250 -0.1033 0.00874 0.00251 -0.0161 0.6976 0.0252 -2.000 -0.0766 0.00868 0.00232 -0.0158 0.6641 0.0257 -1.750 -0.0497 0.00862 0.00215 -0.0154 0.6319 0.0263 -1.500 -0.0228 0.00860 0.00201 -0.0151 0.5984 0.0269 -1.250 0.0041 0.00858 0.00185 -0.0148 0.5641 0.0275 -1.000 0.0312 0.00853 0.00173 -0.0146 0.5396 0.0284 -0.750 0.0586 0.00850 0.00164 -0.0144 0.5181 0.0291 -0.500 0.0862 0.00847 0.00156 -0.0142 0.5023 0.0299 -0.250 0.1139 0.00842 0.00148 -0.0141 0.4906 0.0309 0.000 0.1417 0.00840 0.00141 -0.0139 0.4777 0.0317 0.250 0.1693 0.00836 0.00134 -0.0137 0.4626 0.0330 0.500 0.1969 0.00838 0.00131 -0.0136 0.4442 0.0346 0.750 0.2246 0.00839 0.00128 -0.0134 0.4276 0.0361 1.000 0.2523 0.00841 0.00126 -0.0133 0.4111 0.0376 1.250 0.2800 0.00842 0.00124 -0.0131 0.3941 0.0401 1.500 0.3074 0.00851 0.00125 -0.0130 0.3637 0.0428 1.750 0.3339 0.00873 0.00129 -0.0127 0.3114 0.0461 2.000 0.3606 0.00896 0.00137 -0.0125 0.2685 0.0497 2.250 0.3875 0.00914 0.00144 -0.0123 0.2364 0.0540 2.750 0.4391 0.00859 0.00158 -0.0119 0.1995 0.4194 3.000 0.4589 0.00764 0.00168 -0.0106 0.1863 0.7855 3.250 0.4822 0.00755 0.00181 -0.0094 0.1707 0.8663 3.500 0.5058 0.00758 0.00194 -0.0082 0.1557 0.9237 3.750 0.5357 0.00774 0.00208 -0.0085 0.1384 0.9625 4.000 0.5723 0.00798 0.00223 -0.0104 0.1199 0.9836 4.250 0.6079 0.00821 0.00238 -0.0122 0.1066 0.9932 4.500 0.6427 0.00844 0.00253 -0.0138 0.0963 0.9984 4.750 0.6712 0.00865 0.00269 -0.0140 0.0887 1.0000 5.000 0.6965 0.00883 0.00284 -0.0134 0.0832 1.0000 5.250 0.7217 0.00905 0.00301 -0.0129 0.0766 1.0000 5.500 0.7473 0.00924 0.00318 -0.0124 0.0721 1.0000 5.750 0.7729 0.00946 0.00336 -0.0120 0.0674 1.0000 6.000 0.7987 0.00968 0.00356 -0.0116 0.0632 1.0000 6.250 0.8245 0.00991 0.00376 -0.0112 0.0590 1.0000 6.500 0.8502 0.01016 0.00398 -0.0108 0.0551 1.0000 6.750 0.8762 0.01038 0.00419 -0.0105 0.0522 1.0000 7.000 0.9019 0.01065 0.00444 -0.0102 0.0484 1.0000 7.250 0.9278 0.01090 0.00469 -0.0098 0.0458 1.0000 7.500 0.9536 0.01117 0.00494 -0.0095 0.0432 1.0000 7.750 0.9791 0.01147 0.00523 -0.0092 0.0404 1.0000 8.000 1.0049 0.01174 0.00551 -0.0089 0.0388 1.0000 8.250 1.0305 0.01203 0.00580 -0.0086 0.0368 1.0000 8.500 1.0557 0.01237 0.00613 -0.0083 0.0346 1.0000 8.750 1.0811 0.01268 0.00646 -0.0080 0.0333 1.0000 9.000 1.1065 0.01300 0.00679 -0.0077 0.0321 1.0000 9.250 1.1315 0.01334 0.00715 -0.0073 0.0308 1.0000 9.500 1.1562 0.01373 0.00754 -0.0070 0.0296 1.0000 9.750 1.1807 0.01413 0.00796 -0.0066 0.0286 1.0000 10.000 1.2055 0.01448 0.00835 -0.0063 0.0279 1.0000 10.250 1.2300 0.01485 0.00876 -0.0059 0.0271 1.0000 10.500 1.2542 0.01526 0.00919 -0.0055 0.0263 1.0000 10.750 1.2779 0.01570 0.00965 -0.0051 0.0255 1.0000 11.000 1.3011 0.01620 0.01018 -0.0047 0.0246 1.0000 11.250 1.3241 0.01670 0.01072 -0.0042 0.0239 1.0000 11.500 1.3474 0.01714 0.01121 -0.0037 0.0235 1.0000 11.750 1.3702 0.01762 0.01174 -0.0033 0.0231 1.0000 12.000 1.3926 0.01812 0.01229 -0.0027 0.0225 1.0000 12.250 1.4145 0.01866 0.01287 -0.0022 0.0220 1.0000 12.500 1.4357 0.01923 0.01349 -0.0016 0.0216 1.0000 12.750 1.4563 0.01985 0.01415 -0.0009 0.0211 1.0000 13.000 1.4757 0.02054 0.01489 -0.0001 0.0206 1.0000 13.250 1.4937 0.02134 0.01575 0.0008 0.0201 1.0000 13.500 1.5128 0.02196 0.01645 0.0016 0.0198 1.0000 13.750 1.5307 0.02265 0.01721 0.0025 0.0195 1.0000 14.000 1.5474 0.02340 0.01803 0.0035 0.0193 1.0000 14.250 1.5618 0.02419 0.01890 0.0048 0.0190 1.0000 14.500 1.5739 0.02504 0.01982 0.0063 0.0187 1.0000 14.750 1.5846 0.02599 0.02085 0.0078 0.0184 1.0000 15.000 1.5938 0.02709 0.02202 0.0091 0.0181 1.0000 15.250 1.6017 0.02838 0.02339 0.0103 0.0178 1.0000 15.500 1.6081 0.02990 0.02499 0.0112 0.0176 1.0000 15.750 1.6130 0.03169 0.02686 0.0118 0.0173 1.0000 16.000 1.6156 0.03382 0.02909 0.0121 0.0171 1.0000 16.250 1.6155 0.03641 0.03178 0.0120 0.0168 1.0000 16.500 1.6130 0.03949 0.03497 0.0114 0.0166 1.0000 16.750 1.6129 0.04246 0.03806 0.0105 0.0165 1.0000 17.000 1.6111 0.04584 0.04156 0.0093 0.0164 1.0000 17.250 1.6061 0.04979 0.04563 0.0077 0.0163 1.0000 17.500 1.5979 0.05433 0.05031 0.0056 0.0162 1.0000 17.750 1.5854 0.05960 0.05572 0.0031 0.0161 1.0000 18.000 1.5689 0.06553 0.06178 0.0003 0.0160 1.0000 18.250 1.5472 0.07236 0.06876 -0.0030 0.0160 1.0000 18.500 1.5204 0.08024 0.07679 -0.0069 0.0160 1.0000 18.750 1.4884 0.08933 0.08605 -0.0116 0.0160 1.0000 19.000 1.4520 0.09956 0.09644 -0.0168 0.0160 1.0000 19.250 1.4129 0.11051 0.10754 -0.0225 0.0160 1.0000