XFOIL Version 6.96 Calculated polar for: EPPLER 793 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 ------ -------- --------- --------- -------- -------- -------- -18.750 -0.6241 0.15313 0.15097 -0.0276 1.0000 0.0101 -18.500 -0.6719 0.13829 0.13595 -0.0350 1.0000 0.0103 -18.250 -0.6973 0.12913 0.12668 -0.0395 1.0000 0.0103 -18.000 -0.7149 0.12181 0.11928 -0.0432 1.0000 0.0104 -17.750 -0.7314 0.11493 0.11231 -0.0466 1.0000 0.0104 -17.500 -0.7448 0.10876 0.10607 -0.0497 1.0000 0.0104 -17.250 -0.7603 0.10236 0.09959 -0.0529 1.0000 0.0105 -17.000 -0.7736 0.09649 0.09365 -0.0559 1.0000 0.0105 -16.750 -0.7888 0.09048 0.08756 -0.0589 1.0000 0.0105 -16.500 -0.8034 0.08472 0.08171 -0.0618 1.0000 0.0105 -16.250 -0.8142 0.07959 0.07652 -0.0643 1.0000 0.0106 -16.000 -0.8263 0.07446 0.07131 -0.0669 1.0000 0.0106 -15.750 -0.8404 0.06921 0.06598 -0.0695 1.0000 0.0107 -15.500 -0.8528 0.06439 0.06109 -0.0718 1.0000 0.0107 -15.250 -0.8653 0.05982 0.05644 -0.0740 1.0000 0.0108 -15.000 -0.8810 0.05507 0.05161 -0.0761 1.0000 0.0108 -14.750 -0.8958 0.05061 0.04706 -0.0779 1.0000 0.0108 -14.500 -0.9051 0.04690 0.04329 -0.0793 1.0000 0.0108 -14.250 -0.9198 0.04279 0.03909 -0.0806 1.0000 0.0108 -14.000 -0.9305 0.03927 0.03550 -0.0814 1.0000 0.0109 -13.750 -0.9282 0.03545 0.03158 -0.0853 0.9990 0.0110 -13.500 -0.9134 0.03215 0.02818 -0.0903 0.9968 0.0111 -13.250 -0.8961 0.02893 0.02486 -0.0958 0.9941 0.0112 -13.000 -0.8824 0.02620 0.02203 -0.1000 0.9898 0.0113 -12.750 -0.8601 0.02401 0.01974 -0.1046 0.9854 0.0115 -12.250 -0.8142 0.02147 0.01703 -0.1080 0.9768 0.0118 -11.750 -0.7689 0.01959 0.01501 -0.1092 0.9641 0.0121 -11.250 -0.7169 0.01797 0.01326 -0.1107 0.9487 0.0123 -11.000 -0.6800 0.01718 0.01240 -0.1135 0.9427 0.0124 -10.750 -0.6376 0.01635 0.01150 -0.1174 0.9350 0.0125 -10.500 -0.5949 0.01530 0.01035 -0.1217 0.9226 0.0129 -10.250 -0.5582 0.01465 0.00958 -0.1242 0.9015 0.0132 -10.000 -0.5308 0.01421 0.00901 -0.1246 0.8777 0.0134 -9.750 -0.5067 0.01385 0.00852 -0.1242 0.8554 0.0136 -9.500 -0.4832 0.01352 0.00808 -0.1236 0.8345 0.0138 -9.250 -0.4596 0.01322 0.00766 -0.1230 0.8158 0.0141 -9.000 -0.4355 0.01292 0.00726 -0.1225 0.7986 0.0143 -8.750 -0.4108 0.01265 0.00690 -0.1220 0.7826 0.0147 -8.500 -0.3858 0.01239 0.00655 -0.1216 0.7675 0.0150 -8.250 -0.3606 0.01215 0.00621 -0.1212 0.7520 0.0152 -8.000 -0.3349 0.01192 0.00589 -0.1208 0.7381 0.0154 -7.750 -0.3095 0.01161 0.00551 -0.1205 0.7247 0.0158 -7.500 -0.2839 0.01134 0.00515 -0.1201 0.7107 0.0162 -7.250 -0.2575 0.01111 0.00485 -0.1199 0.6974 0.0167 -7.000 -0.2309 0.01090 0.00458 -0.1197 0.6850 0.0172 -6.750 -0.2042 0.01072 0.00433 -0.1194 0.6728 0.0177 -6.500 -0.1775 0.01057 0.00410 -0.1192 0.6598 0.0182 -6.250 -0.1502 0.01042 0.00388 -0.1191 0.6475 0.0187 -6.000 -0.1231 0.01024 0.00365 -0.1189 0.6359 0.0198 -5.750 -0.0959 0.01009 0.00344 -0.1187 0.6242 0.0211 -5.500 -0.0684 0.00995 0.00326 -0.1186 0.6127 0.0230 -5.250 -0.0410 0.00978 0.00306 -0.1185 0.6016 0.0271 -5.000 -0.0139 0.00956 0.00285 -0.1184 0.5909 0.0400 -4.750 0.0137 0.00935 0.00267 -0.1184 0.5805 0.0547 -4.500 0.0413 0.00920 0.00252 -0.1183 0.5707 0.0685 -4.250 0.0689 0.00903 0.00237 -0.1183 0.5598 0.0861 -4.000 0.0967 0.00881 0.00223 -0.1183 0.5508 0.1112 -3.750 0.1242 0.00864 0.00210 -0.1183 0.5414 0.1384 -3.500 0.1522 0.00844 0.00199 -0.1184 0.5322 0.1704 -3.250 0.1801 0.00834 0.00192 -0.1184 0.5231 0.1927 -3.000 0.2083 0.00825 0.00185 -0.1184 0.5149 0.2130 -2.750 0.2363 0.00818 0.00181 -0.1184 0.5067 0.2343 -2.500 0.2646 0.00812 0.00177 -0.1184 0.4984 0.2531 -2.250 0.2926 0.00808 0.00176 -0.1184 0.4904 0.2777 -2.000 0.3210 0.00804 0.00174 -0.1184 0.4832 0.2959 -1.750 0.3491 0.00806 0.00174 -0.1183 0.4754 0.3070 -1.500 0.3775 0.00806 0.00173 -0.1183 0.4685 0.3165 -1.250 0.4056 0.00809 0.00174 -0.1183 0.4610 0.3260 -1.000 0.4339 0.00811 0.00175 -0.1183 0.4550 0.3354 -0.500 0.4901 0.00818 0.00178 -0.1181 0.4410 0.3537 -0.250 0.5185 0.00820 0.00180 -0.1181 0.4354 0.3620 0.000 0.5466 0.00824 0.00184 -0.1181 0.4291 0.3718 0.250 0.5746 0.00829 0.00187 -0.1180 0.4231 0.3805 0.500 0.6028 0.00832 0.00191 -0.1180 0.4170 0.3903 0.750 0.6306 0.00838 0.00196 -0.1179 0.4110 0.3997 1.000 0.6586 0.00844 0.00201 -0.1178 0.4059 0.4096 1.250 0.6866 0.00848 0.00206 -0.1178 0.4000 0.4198 1.500 0.7141 0.00856 0.00213 -0.1177 0.3938 0.4300 1.750 0.7420 0.00861 0.00220 -0.1176 0.3890 0.4412 2.000 0.7699 0.00866 0.00227 -0.1175 0.3838 0.4521 2.250 0.7973 0.00875 0.00235 -0.1174 0.3777 0.4640 2.500 0.8249 0.00881 0.00243 -0.1173 0.3726 0.4766 2.750 0.8525 0.00888 0.00252 -0.1172 0.3673 0.4890 3.000 0.8797 0.00897 0.00262 -0.1170 0.3620 0.5016 3.250 0.9070 0.00905 0.00272 -0.1169 0.3572 0.5159 3.500 0.9344 0.00913 0.00283 -0.1168 0.3518 0.5298 3.750 0.9612 0.00923 0.00294 -0.1165 0.3461 0.5436 4.000 0.9882 0.00932 0.00306 -0.1164 0.3418 0.5588 4.250 1.0153 0.00941 0.00318 -0.1162 0.3370 0.5743 4.500 1.0418 0.00953 0.00332 -0.1159 0.3313 0.5892 4.750 1.0683 0.00964 0.00346 -0.1157 0.3264 0.6057 5.000 1.0951 0.00973 0.00360 -0.1155 0.3220 0.6244 5.250 1.1212 0.00985 0.00376 -0.1151 0.3163 0.6431 5.500 1.1470 0.00999 0.00392 -0.1148 0.3108 0.6616 5.750 1.1731 0.01010 0.00409 -0.1145 0.3051 0.6829 6.000 1.1984 0.01025 0.00427 -0.1140 0.2988 0.7076 6.250 1.2238 0.01037 0.00446 -0.1136 0.2936 0.7327 6.500 1.2489 0.01049 0.00465 -0.1131 0.2876 0.7622 6.750 1.2727 0.01065 0.00487 -0.1124 0.2812 0.7988 7.000 1.2961 0.01072 0.00507 -0.1115 0.2760 0.8471 7.250 1.3146 0.01069 0.00524 -0.1095 0.2691 1.0000 7.500 1.3387 0.01093 0.00546 -0.1089 0.2628 1.0000 7.750 1.3628 0.01116 0.00567 -0.1083 0.2563 1.0000 8.000 1.3857 0.01144 0.00592 -0.1075 0.2498 1.0000 8.250 1.4093 0.01166 0.00615 -0.1068 0.2438 1.0000 8.500 1.4310 0.01197 0.00643 -0.1058 0.2364 1.0000 8.750 1.4529 0.01223 0.00668 -0.1049 0.2300 1.0000 9.000 1.4724 0.01255 0.00697 -0.1034 0.2224 1.0000 9.250 1.4920 0.01284 0.00726 -0.1021 0.2158 1.0000 9.500 1.5097 0.01322 0.00761 -0.1004 0.2074 1.0000 9.750 1.5279 0.01357 0.00795 -0.0988 0.1998 1.0000 10.000 1.5438 0.01403 0.00837 -0.0969 0.1905 1.0000 10.250 1.5598 0.01448 0.00879 -0.0951 0.1809 1.0000 10.500 1.5744 0.01500 0.00927 -0.0931 0.1706 1.0000 10.750 1.5864 0.01564 0.00985 -0.0907 0.1589 1.0000 11.000 1.5974 0.01633 0.01050 -0.0883 0.1477 1.0000 11.250 1.6083 0.01704 0.01117 -0.0860 0.1379 1.0000 11.500 1.6194 0.01775 0.01186 -0.0838 0.1295 1.0000 11.750 1.6261 0.01870 0.01277 -0.0811 0.1183 1.0000 12.000 1.6334 0.01967 0.01371 -0.0786 0.1101 1.0000 12.250 1.6421 0.02060 0.01465 -0.0765 0.1031 1.0000 12.500 1.6480 0.02174 0.01577 -0.0742 0.0958 1.0000 12.750 1.6535 0.02297 0.01700 -0.0720 0.0891 1.0000 13.000 1.6605 0.02418 0.01822 -0.0702 0.0846 1.0000 13.250 1.6616 0.02586 0.01988 -0.0680 0.0767 1.0000 13.500 1.6695 0.02715 0.02121 -0.0666 0.0743 1.0000 13.750 1.6725 0.02887 0.02296 -0.0650 0.0692 1.0000 14.000 1.6744 0.03079 0.02489 -0.0636 0.0648 1.0000 14.250 1.6758 0.03284 0.02697 -0.0623 0.0601 1.0000 14.500 1.6755 0.03515 0.02930 -0.0612 0.0563 1.0000 14.750 1.6780 0.03730 0.03152 -0.0604 0.0536 1.0000 15.000 1.6769 0.03991 0.03416 -0.0596 0.0504 1.0000 15.250 1.6750 0.04270 0.03699 -0.0591 0.0473 1.0000 15.500 1.6728 0.04565 0.03999 -0.0587 0.0443 1.0000 16.000 1.6646 0.05230 0.04675 -0.0586 0.0390 1.0000 16.250 1.6600 0.05585 0.05037 -0.0588 0.0367 1.0000 16.500 1.6536 0.05975 0.05434 -0.0592 0.0349 1.0000 16.750 1.6499 0.06343 0.05808 -0.0597 0.0333 1.0000 17.000 1.6442 0.06744 0.06217 -0.0604 0.0317 1.0000 17.250 1.6359 0.07191 0.06671 -0.0613 0.0300 1.0000 17.500 1.6300 0.07617 0.07105 -0.0623 0.0287 1.0000 17.750 1.6239 0.08051 0.07547 -0.0635 0.0274 1.0000 18.000 1.6155 0.08529 0.08031 -0.0648 0.0259 1.0000 18.500 1.6007 0.09479 0.08997 -0.0678 0.0233 1.0000 18.750 1.5937 0.09955 0.09480 -0.0695 0.0224 1.0000