XFOIL Version 6.96 Calculated polar for: 12% JOUKOWSKI AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -16.750 -1.0043 0.12810 0.12391 0.0296 1.0000 0.0267 -16.500 -1.0489 0.11304 0.10859 0.0199 1.0000 0.0266 -16.250 -1.0759 0.10274 0.09807 0.0133 1.0000 0.0268 -16.000 -1.0963 0.09430 0.08944 0.0080 1.0000 0.0269 -15.750 -1.1143 0.08668 0.08162 0.0032 1.0000 0.0271 -15.500 -1.1290 0.08005 0.07479 -0.0009 1.0000 0.0274 -15.250 -1.1421 0.07402 0.06857 -0.0045 1.0000 0.0276 -15.000 -1.1491 0.06934 0.06382 -0.0070 1.0000 0.0279 -14.750 -1.1554 0.06485 0.05924 -0.0095 1.0000 0.0282 -14.500 -1.1609 0.06058 0.05487 -0.0118 1.0000 0.0285 -14.250 -1.1653 0.05658 0.05077 -0.0138 1.0000 0.0289 -14.000 -1.1688 0.05283 0.04691 -0.0157 1.0000 0.0293 -13.750 -1.1713 0.04934 0.04330 -0.0173 1.0000 0.0298 -13.500 -1.1725 0.04614 0.03998 -0.0186 1.0000 0.0304 -13.250 -1.1729 0.04320 0.03690 -0.0195 1.0000 0.0311 -13.000 -1.1719 0.04055 0.03407 -0.0201 1.0000 0.0319 -12.750 -1.1695 0.03820 0.03154 -0.0203 1.0000 0.0325 -12.500 -1.1679 0.03599 0.02930 -0.0202 1.0000 0.0331 -12.250 -1.1646 0.03414 0.02738 -0.0197 1.0000 0.0338 -12.000 -1.1599 0.03257 0.02573 -0.0187 1.0000 0.0346 -11.750 -1.1540 0.03119 0.02426 -0.0173 1.0000 0.0356 -11.500 -1.1446 0.02995 0.02290 -0.0159 1.0000 0.0367 -11.250 -1.1311 0.02880 0.02159 -0.0149 1.0000 0.0380 -11.000 -1.1181 0.02756 0.02033 -0.0139 1.0000 0.0393 -10.750 -1.1019 0.02654 0.01926 -0.0131 1.0000 0.0408 -10.500 -1.0842 0.02558 0.01821 -0.0123 1.0000 0.0426 -10.250 -1.0650 0.02468 0.01716 -0.0116 1.0000 0.0445 -10.000 -1.0468 0.02366 0.01615 -0.0109 1.0000 0.0464 -9.750 -1.0263 0.02285 0.01528 -0.0103 1.0000 0.0489 -9.500 -1.0046 0.02210 0.01443 -0.0097 1.0000 0.0516 -9.250 -0.9837 0.02124 0.01356 -0.0092 1.0000 0.0543 -9.000 -0.9612 0.02054 0.01281 -0.0087 1.0000 0.0576 -8.750 -0.9381 0.01986 0.01206 -0.0083 1.0000 0.0613 -8.500 -0.9152 0.01915 0.01136 -0.0078 1.0000 0.0653 -8.250 -0.8909 0.01859 0.01071 -0.0075 1.0000 0.0699 -8.000 -0.8673 0.01791 0.01007 -0.0071 1.0000 0.0752 -7.750 -0.8425 0.01738 0.00949 -0.0068 1.0000 0.0810 -7.500 -0.8180 0.01679 0.00892 -0.0065 1.0000 0.0879 -7.250 -0.7929 0.01626 0.00840 -0.0062 1.0000 0.0953 -7.000 -0.7674 0.01579 0.00792 -0.0059 1.0000 0.1042 -6.750 -0.7422 0.01528 0.00745 -0.0057 1.0000 0.1141 -6.500 -0.7165 0.01482 0.00702 -0.0054 1.0000 0.1248 -6.250 -0.6907 0.01438 0.00662 -0.0052 1.0000 0.1369 -6.000 -0.6647 0.01397 0.00624 -0.0050 1.0000 0.1501 -5.750 -0.6387 0.01357 0.00590 -0.0048 1.0000 0.1647 -5.500 -0.6125 0.01319 0.00558 -0.0046 1.0000 0.1802 -5.250 -0.5864 0.01283 0.00529 -0.0044 1.0000 0.1967 -5.000 -0.5603 0.01249 0.00502 -0.0042 1.0000 0.2141 -4.750 -0.5343 0.01217 0.00478 -0.0039 1.0000 0.2321 -4.500 -0.5021 0.01189 0.00456 -0.0049 0.9806 0.2526 -4.250 -0.4656 0.01163 0.00438 -0.0067 0.9536 0.2743 -4.000 -0.4318 0.01141 0.00421 -0.0078 0.9279 0.2958 -3.750 -0.4022 0.01124 0.00405 -0.0079 0.9022 0.3165 -3.500 -0.3751 0.01109 0.00392 -0.0075 0.8780 0.3362 -3.250 -0.3491 0.01095 0.00379 -0.0068 0.8548 0.3555 -3.000 -0.3234 0.01083 0.00366 -0.0060 0.8327 0.3749 -2.750 -0.2976 0.01072 0.00355 -0.0052 0.8117 0.3943 -2.500 -0.2715 0.01063 0.00344 -0.0045 0.7916 0.4136 -2.250 -0.2449 0.01054 0.00334 -0.0039 0.7716 0.4331 -2.000 -0.2182 0.01046 0.00325 -0.0034 0.7520 0.4521 -1.750 -0.1913 0.01039 0.00318 -0.0029 0.7327 0.4710 -1.500 -0.1643 0.01032 0.00311 -0.0024 0.7137 0.4900 -1.250 -0.1372 0.01027 0.00305 -0.0020 0.6948 0.5088 -1.000 -0.1099 0.01024 0.00300 -0.0015 0.6762 0.5276 -0.750 -0.0825 0.01021 0.00297 -0.0011 0.6576 0.5465 -0.500 -0.0551 0.01019 0.00294 -0.0007 0.6392 0.5651 -0.250 -0.0276 0.01018 0.00292 -0.0004 0.6208 0.5837 0.000 0.0000 0.01017 0.00291 0.0000 0.6024 0.6024 0.250 0.0276 0.01018 0.00292 0.0004 0.5837 0.6209 0.500 0.0550 0.01019 0.00294 0.0007 0.5651 0.6392 0.750 0.0825 0.01021 0.00297 0.0011 0.5464 0.6577 1.000 0.1098 0.01024 0.00300 0.0015 0.5277 0.6762 1.250 0.1371 0.01027 0.00305 0.0020 0.5088 0.6948 1.500 0.1643 0.01032 0.00311 0.0024 0.4900 0.7137 1.750 0.1913 0.01039 0.00318 0.0029 0.4710 0.7326 2.000 0.2182 0.01046 0.00325 0.0034 0.4521 0.7520 2.250 0.2449 0.01054 0.00334 0.0040 0.4331 0.7716 2.500 0.2715 0.01063 0.00344 0.0045 0.4136 0.7916 2.750 0.2976 0.01072 0.00355 0.0052 0.3943 0.8117 3.000 0.3234 0.01083 0.00366 0.0060 0.3749 0.8327 3.250 0.3491 0.01095 0.00379 0.0068 0.3554 0.8548 3.500 0.3751 0.01109 0.00392 0.0075 0.3363 0.8779 3.750 0.4021 0.01124 0.00405 0.0080 0.3165 0.9023 4.000 0.4318 0.01141 0.00421 0.0078 0.2958 0.9279 4.250 0.4656 0.01163 0.00438 0.0067 0.2743 0.9536 4.500 0.5021 0.01189 0.00456 0.0049 0.2526 0.9806 4.750 0.5343 0.01217 0.00478 0.0039 0.2321 1.0000 5.000 0.5603 0.01249 0.00502 0.0042 0.2142 1.0000 5.250 0.5864 0.01283 0.00529 0.0044 0.1966 1.0000 5.500 0.6125 0.01319 0.00558 0.0046 0.1802 1.0000 5.750 0.6386 0.01357 0.00590 0.0048 0.1646 1.0000 6.000 0.6647 0.01397 0.00625 0.0050 0.1501 1.0000 6.250 0.6907 0.01438 0.00662 0.0052 0.1369 1.0000 6.500 0.7165 0.01482 0.00702 0.0054 0.1248 1.0000 6.750 0.7421 0.01528 0.00745 0.0057 0.1141 1.0000 7.000 0.7674 0.01579 0.00792 0.0059 0.1042 1.0000 7.250 0.7929 0.01627 0.00840 0.0062 0.0953 1.0000 7.500 0.8180 0.01679 0.00892 0.0065 0.0879 1.0000 7.750 0.8424 0.01738 0.00949 0.0068 0.0810 1.0000 8.000 0.8672 0.01791 0.01007 0.0071 0.0752 1.0000 8.500 0.9151 0.01915 0.01136 0.0079 0.0653 1.0000 8.750 0.9381 0.01986 0.01206 0.0083 0.0613 1.0000 9.000 0.9611 0.02054 0.01281 0.0087 0.0577 1.0000 9.250 0.9836 0.02124 0.01355 0.0092 0.0543 1.0000 9.500 1.0044 0.02210 0.01442 0.0098 0.0516 1.0000 9.750 1.0261 0.02284 0.01527 0.0103 0.0488 1.0000 10.000 1.0467 0.02366 0.01615 0.0109 0.0464 1.0000 10.250 1.0649 0.02467 0.01715 0.0116 0.0445 1.0000 10.500 1.0840 0.02558 0.01820 0.0123 0.0426 1.0000 10.750 1.1018 0.02653 0.01925 0.0131 0.0408 1.0000 11.000 1.1179 0.02755 0.02032 0.0139 0.0393 1.0000 11.250 1.1308 0.02878 0.02157 0.0149 0.0380 1.0000 11.500 1.1442 0.02994 0.02289 0.0160 0.0367 1.0000 11.750 1.1536 0.03118 0.02424 0.0173 0.0355 1.0000 12.000 1.1596 0.03255 0.02571 0.0188 0.0346 1.0000 12.250 1.1643 0.03412 0.02736 0.0197 0.0338 1.0000 12.500 1.1676 0.03597 0.02927 0.0202 0.0331 1.0000 12.750 1.1693 0.03816 0.03151 0.0204 0.0325 1.0000 13.000 1.1716 0.04053 0.03406 0.0202 0.0318 1.0000 13.250 1.1728 0.04316 0.03686 0.0196 0.0311 1.0000 13.500 1.1726 0.04609 0.03992 0.0186 0.0304 1.0000 13.750 1.1714 0.04929 0.04326 0.0173 0.0298 1.0000 14.000 1.1691 0.05276 0.04684 0.0157 0.0293 1.0000 14.250 1.1657 0.05651 0.05069 0.0138 0.0289 1.0000 14.500 1.1615 0.06050 0.05478 0.0118 0.0285 1.0000 14.750 1.1559 0.06476 0.05914 0.0095 0.0282 1.0000 15.000 1.1498 0.06923 0.06370 0.0071 0.0279 1.0000 15.250 1.1416 0.07414 0.06871 0.0044 0.0275 1.0000 15.500 1.1292 0.08003 0.07478 0.0009 0.0273 1.0000 15.750 1.1145 0.08664 0.08158 -0.0032 0.0271 1.0000 16.000 1.0967 0.09419 0.08933 -0.0079 0.0269 1.0000 16.250 1.0759 0.10270 0.09803 -0.0133 0.0267 1.0000 16.500 1.0497 0.11276 0.10830 -0.0197 0.0266 1.0000 16.750 1.0040 0.12803 0.12384 -0.0295 0.0267 1.0000