XFOIL Version 6.96 Calculated polar for: GOE 601 AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.750 -0.8259 0.12018 0.11673 -0.0565 1.0000 0.0206 -19.500 -0.8440 0.11333 0.10977 -0.0600 1.0000 0.0207 -19.250 -0.8577 0.10725 0.10360 -0.0632 1.0000 0.0210 -19.000 -0.8722 0.10123 0.09749 -0.0663 1.0000 0.0213 -18.750 -0.8858 0.09556 0.09172 -0.0691 1.0000 0.0215 -18.500 -0.8980 0.09020 0.08624 -0.0718 1.0000 0.0217 -18.250 -0.9092 0.08513 0.08108 -0.0742 1.0000 0.0219 -18.000 -0.9196 0.08026 0.07611 -0.0765 1.0000 0.0221 -17.750 -0.9292 0.07564 0.07137 -0.0786 1.0000 0.0224 -17.500 -0.9376 0.07129 0.06691 -0.0805 1.0000 0.0226 -17.250 -0.9456 0.06721 0.06273 -0.0822 1.0000 0.0227 -17.000 -0.9524 0.06335 0.05876 -0.0837 1.0000 0.0230 -16.750 -0.9593 0.05971 0.05502 -0.0849 1.0000 0.0232 -16.500 -0.9672 0.05616 0.05142 -0.0859 1.0000 0.0235 -16.250 -0.9732 0.05299 0.04818 -0.0866 1.0000 0.0236 -16.000 -0.9798 0.04989 0.04502 -0.0871 1.0000 0.0238 -15.750 -0.9837 0.04715 0.04222 -0.0874 1.0000 0.0241 -15.500 -0.9883 0.04449 0.03948 -0.0874 1.0000 0.0242 -15.250 -0.9912 0.04211 0.03704 -0.0872 1.0000 0.0245 -15.000 -0.9939 0.03990 0.03476 -0.0868 1.0000 0.0248 -14.750 -0.9969 0.03783 0.03262 -0.0860 1.0000 0.0251 -14.500 -1.0004 0.03589 0.03060 -0.0848 1.0000 0.0254 -14.250 -0.9896 0.03395 0.02858 -0.0861 0.9990 0.0259 -14.000 -0.9730 0.03210 0.02663 -0.0881 0.9969 0.0264 -13.750 -0.9557 0.03047 0.02489 -0.0898 0.9942 0.0268 -13.500 -0.9397 0.02901 0.02332 -0.0909 0.9913 0.0271 -13.250 -0.9269 0.02730 0.02155 -0.0919 0.9879 0.0276 -13.000 -0.9097 0.02584 0.02005 -0.0932 0.9849 0.0282 -12.750 -0.8885 0.02463 0.01877 -0.0947 0.9826 0.0287 -12.500 -0.8730 0.02361 0.01770 -0.0945 0.9778 0.0291 -12.250 -0.8527 0.02266 0.01668 -0.0951 0.9743 0.0296 -12.000 -0.8286 0.02179 0.01574 -0.0961 0.9716 0.0303 -11.750 -0.8066 0.02101 0.01489 -0.0965 0.9678 0.0309 -11.500 -0.7848 0.02031 0.01412 -0.0966 0.9627 0.0314 -11.250 -0.7572 0.01959 0.01332 -0.0978 0.9595 0.0319 -11.000 -0.7332 0.01865 0.01236 -0.0986 0.9557 0.0328 -10.750 -0.7166 0.01802 0.01168 -0.0973 0.9474 0.0334 -10.500 -0.6893 0.01736 0.01098 -0.0982 0.9426 0.0341 -10.250 -0.6747 0.01690 0.01046 -0.0961 0.9318 0.0346 -10.000 -0.6542 0.01642 0.00993 -0.0952 0.9230 0.0353 -9.750 -0.6327 0.01598 0.00941 -0.0945 0.9123 0.0360 -9.500 -0.6118 0.01558 0.00895 -0.0935 0.8990 0.0367 -9.250 -0.5898 0.01511 0.00840 -0.0928 0.8855 0.0374 -9.000 -0.5679 0.01466 0.00788 -0.0920 0.8727 0.0384 -8.750 -0.5458 0.01429 0.00742 -0.0912 0.8609 0.0394 -8.500 -0.5239 0.01397 0.00702 -0.0903 0.8502 0.0405 -8.250 -0.5025 0.01370 0.00667 -0.0892 0.8412 0.0419 -8.000 -0.4808 0.01343 0.00632 -0.0882 0.8335 0.0435 -7.750 -0.4599 0.01313 0.00599 -0.0871 0.8267 0.0458 -7.500 -0.4382 0.01287 0.00569 -0.0860 0.8203 0.0487 -7.250 -0.4165 0.01258 0.00538 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0.00247 -0.0714 0.7271 0.3212 -2.250 0.0617 0.00898 0.00240 -0.0707 0.7210 0.3384 -2.000 0.0861 0.00884 0.00234 -0.0700 0.7158 0.3614 -1.750 0.1100 0.00870 0.00229 -0.0692 0.7107 0.3945 -1.500 0.1341 0.00859 0.00228 -0.0684 0.7042 0.4236 -1.250 0.1589 0.00854 0.00226 -0.0677 0.6973 0.4449 -1.000 0.1843 0.00851 0.00224 -0.0672 0.6913 0.4612 -0.750 0.2098 0.00848 0.00223 -0.0666 0.6844 0.4736 -0.500 0.2348 0.00848 0.00220 -0.0660 0.6768 0.4842 -0.250 0.2598 0.00845 0.00219 -0.0653 0.6681 0.4938 0.000 0.2848 0.00846 0.00218 -0.0646 0.6607 0.5042 0.250 0.3093 0.00844 0.00218 -0.0639 0.6512 0.5143 0.500 0.3333 0.00846 0.00217 -0.0630 0.6398 0.5223 0.750 0.3565 0.00848 0.00217 -0.0620 0.6279 0.5298 1.000 0.3803 0.00850 0.00219 -0.0611 0.6159 0.5387 1.250 0.4034 0.00852 0.00221 -0.0601 0.6044 0.5479 1.500 0.4258 0.00857 0.00224 -0.0589 0.5907 0.5583 1.750 0.4468 0.00861 0.00228 -0.0575 0.5752 0.5706 2.000 0.4671 0.00867 0.00234 -0.0559 0.5585 0.5860 2.250 0.4862 0.00871 0.00241 -0.0540 0.5414 0.6112 2.500 0.5034 0.00875 0.00251 -0.0518 0.5214 0.6434 2.750 0.5189 0.00885 0.00262 -0.0492 0.4980 0.6741 3.000 0.5322 0.00901 0.00275 -0.0462 0.4692 0.7010 3.250 0.5399 0.00922 0.00290 -0.0421 0.4324 0.7289 3.500 0.5469 0.00947 0.00310 -0.0378 0.3951 0.7602 3.750 0.5559 0.00972 0.00335 -0.0340 0.3652 0.7977 4.000 0.5691 0.00995 0.00363 -0.0311 0.3434 0.8436 4.250 0.5953 0.01025 0.00397 -0.0310 0.3228 0.8933 4.500 0.6424 0.01066 0.00436 -0.0355 0.3065 0.9268 4.750 0.6915 0.01103 0.00469 -0.0405 0.2936 0.9459 5.000 0.7357 0.01137 0.00499 -0.0443 0.2829 0.9595 5.250 0.7720 0.01168 0.00526 -0.0465 0.2746 0.9713 5.750 0.8348 0.01223 0.00577 -0.0487 0.2596 0.9901 6.000 0.8637 0.01256 0.00607 -0.0493 0.2516 0.9989 6.250 0.8828 0.01280 0.00628 -0.0478 0.2436 1.0000 6.500 0.8944 0.01304 0.00650 -0.0449 0.2382 1.0000 6.750 0.9092 0.01325 0.00671 -0.0425 0.2319 1.0000 7.000 0.9229 0.01353 0.00696 -0.0400 0.2247 1.0000 7.250 0.9377 0.01381 0.00723 -0.0377 0.2174 1.0000 7.500 0.9512 0.01416 0.00754 -0.0353 0.2073 1.0000 7.750 0.9667 0.01449 0.00785 -0.0333 0.1984 1.0000 8.000 0.9807 0.01489 0.00821 -0.0311 0.1879 1.0000 8.250 0.9937 0.01538 0.00863 -0.0288 0.1733 1.0000 8.500 1.0024 0.01609 0.00919 -0.0260 0.1484 1.0000 8.750 0.9961 0.01762 0.01032 -0.0214 0.0872 1.0000 9.000 0.9938 0.01910 0.01154 -0.0174 0.0450 1.0000 9.250 1.0053 0.01988 0.01228 -0.0154 0.0381 1.0000 9.500 1.0198 0.02051 0.01292 -0.0139 0.0358 1.0000 9.750 1.0340 0.02119 0.01361 -0.0123 0.0343 1.0000 10.000 1.0478 0.02191 0.01435 -0.0108 0.0329 1.0000 10.250 1.0612 0.02267 0.01514 -0.0093 0.0319 1.0000 10.500 1.0755 0.02340 0.01592 -0.0080 0.0314 1.0000 10.750 1.0893 0.02419 0.01674 -0.0067 0.0307 1.0000 11.000 1.1025 0.02502 0.01762 -0.0053 0.0300 1.0000 11.250 1.1151 0.02592 0.01856 -0.0040 0.0293 1.0000 11.500 1.1267 0.02691 0.01959 -0.0027 0.0287 1.0000 11.750 1.1371 0.02802 0.02073 -0.0014 0.0282 1.0000 12.000 1.1464 0.02921 0.02197 0.0000 0.0277 1.0000 12.250 1.1535 0.03061 0.02342 0.0014 0.0272 1.0000 12.500 1.1637 0.03180 0.02467 0.0026 0.0270 1.0000 12.750 1.1738 0.03304 0.02598 0.0036 0.0267 1.0000 13.000 1.1821 0.03443 0.02744 0.0047 0.0264 1.0000 13.250 1.1904 0.03587 0.02894 0.0057 0.0260 1.0000 13.500 1.1971 0.03748 0.03062 0.0066 0.0257 1.0000 13.750 1.2041 0.03912 0.03232 0.0075 0.0253 1.0000 14.000 1.2094 0.04095 0.03421 0.0083 0.0250 1.0000 14.250 1.2147 0.04283 0.03616 0.0090 0.0246 1.0000 14.500 1.2182 0.04494 0.03834 0.0096 0.0243 1.0000 14.750 1.2214 0.04715 0.04062 0.0101 0.0240 1.0000 15.000 1.2219 0.04970 0.04323 0.0105 0.0237 1.0000 15.250 1.2217 0.05240 0.04601 0.0108 0.0235 1.0000 15.500 1.2177 0.05560 0.04927 0.0109 0.0231 1.0000 15.750 1.2166 0.05859 0.05234 0.0109 0.0229 1.0000 16.000 1.2177 0.06140 0.05525 0.0108 0.0227 1.0000 16.250 1.2179 0.06436 0.05830 0.0105 0.0225 1.0000 16.500 1.2172 0.06751 0.06154 0.0101 0.0224 1.0000 16.750 1.2162 0.07077 0.06489 0.0096 0.0222 1.0000 17.000 1.2141 0.07421 0.06843 0.0090 0.0220 1.0000 17.250 1.2123 0.07769 0.07200 0.0082 0.0217 1.0000 17.500 1.2101 0.08125 0.07565 0.0073 0.0214 1.0000 17.750 1.2066 0.08505 0.07954 0.0064 0.0212 1.0000 18.000 1.2040 0.08880 0.08338 0.0053 0.0209 1.0000 18.250 1.2002 0.09274 0.08739 0.0041 0.0207 1.0000 18.500 1.1968 0.09662 0.09135 0.0029 0.0205 1.0000