XFOIL Version 6.96 Calculated polar for: RUTAN WING 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 ------ -------- --------- --------- -------- -------- -------- -18.500 -1.3657 0.07342 0.07026 -0.0296 1.0000 0.0155 -18.250 -1.4175 0.06018 0.05673 -0.0385 1.0000 0.0155 -18.000 -1.4400 0.05334 0.04971 -0.0425 1.0000 0.0155 -17.750 -1.4529 0.04841 0.04463 -0.0448 1.0000 0.0156 -17.500 -1.4604 0.04455 0.04064 -0.0462 1.0000 0.0157 -17.250 -1.4641 0.04135 0.03733 -0.0470 1.0000 0.0158 -17.000 -1.4650 0.03864 0.03451 -0.0473 1.0000 0.0159 -16.750 -1.4635 0.03629 0.03206 -0.0473 1.0000 0.0161 -16.500 -1.4600 0.03427 0.02993 -0.0470 1.0000 0.0162 -16.250 -1.4550 0.03247 0.02804 -0.0465 1.0000 0.0164 -16.000 -1.4485 0.03088 0.02636 -0.0457 1.0000 0.0165 -15.750 -1.4408 0.02946 0.02484 -0.0448 1.0000 0.0167 -15.500 -1.4320 0.02819 0.02349 -0.0438 1.0000 0.0169 -15.250 -1.4222 0.02706 0.02227 -0.0425 1.0000 0.0170 -15.000 -1.4116 0.02606 0.02118 -0.0411 1.0000 0.0172 -14.750 -1.4002 0.02517 0.02021 -0.0395 1.0000 0.0173 -14.500 -1.3880 0.02425 0.01921 -0.0380 1.0000 0.0176 -14.250 -1.3721 0.02339 0.01830 -0.0369 1.0000 0.0178 -14.000 -1.3542 0.02264 0.01750 -0.0360 1.0000 0.0181 -13.750 -1.3349 0.02197 0.01678 -0.0353 1.0000 0.0185 -13.500 -1.3146 0.02133 0.01611 -0.0347 1.0000 0.0188 -13.250 -1.2936 0.02073 0.01546 -0.0341 1.0000 0.0192 -13.000 -1.2720 0.02015 0.01482 -0.0335 1.0000 0.0195 -12.750 -1.2500 0.01959 0.01420 -0.0330 1.0000 0.0198 -12.500 -1.2273 0.01905 0.01360 -0.0326 1.0000 0.0201 -12.250 -1.2042 0.01854 0.01304 -0.0322 1.0000 0.0203 -12.000 -1.1815 0.01794 0.01240 -0.0318 1.0000 0.0208 -11.750 -1.1578 0.01742 0.01186 -0.0314 1.0000 0.0212 -11.500 -1.1297 0.01695 0.01136 -0.0320 0.9804 0.0216 -11.250 -1.1032 0.01652 0.01089 -0.0321 0.9665 0.0221 -11.000 -1.0792 0.01614 0.01045 -0.0316 0.9538 0.0225 -10.500 -1.0318 0.01545 0.00963 -0.0304 0.9328 0.0234 -10.250 -1.0077 0.01512 0.00923 -0.0298 0.9245 0.0239 -10.000 -0.9832 0.01471 0.00879 -0.0294 0.9164 0.0245 -9.750 -0.9585 0.01437 0.00841 -0.0290 0.9089 0.0250 -9.500 -0.9328 0.01404 0.00805 -0.0287 0.9020 0.0255 -9.250 -0.9071 0.01374 0.00770 -0.0284 0.8951 0.0261 -9.000 -0.8810 0.01345 0.00736 -0.0282 0.8890 0.0267 -8.750 -0.8546 0.01317 0.00703 -0.0280 0.8826 0.0272 -8.500 -0.8284 0.01288 0.00670 -0.0278 0.8764 0.0278 -8.250 -0.8019 0.01257 0.00636 -0.0277 0.8710 0.0286 -8.000 -0.7750 0.01229 0.00607 -0.0276 0.8654 0.0294 -7.750 -0.7480 0.01204 0.00579 -0.0275 0.8600 0.0301 -7.500 -0.7209 0.01180 0.00551 -0.0274 0.8550 0.0308 -7.250 -0.6934 0.01157 0.00525 -0.0274 0.8498 0.0314 -7.000 -0.6661 0.01131 0.00497 -0.0273 0.8443 0.0324 -6.750 -0.6388 0.01107 0.00472 -0.0273 0.8392 0.0334 -6.500 -0.6110 0.01085 0.00449 -0.0273 0.8349 0.0344 -6.250 -0.5830 0.01065 0.00426 -0.0274 0.8303 0.0354 -6.000 -0.5550 0.01046 0.00405 -0.0274 0.8256 0.0363 -5.750 -0.5273 0.01024 0.00383 -0.0274 0.8211 0.0379 -5.500 -0.4991 0.01005 0.00363 -0.0275 0.8169 0.0394 -5.250 -0.4707 0.00988 0.00345 -0.0276 0.8121 0.0408 -5.000 -0.4425 0.00970 0.00327 -0.0276 0.8068 0.0427 -4.750 -0.4143 0.00954 0.00310 -0.0277 0.8018 0.0450 -4.500 -0.3857 0.00938 0.00295 -0.0278 0.7973 0.0474 -4.250 -0.3571 0.00921 0.00280 -0.0280 0.7925 0.0505 -4.000 -0.3284 0.00908 0.00266 -0.0281 0.7879 0.0533 -3.500 -0.2710 0.00880 0.00241 -0.0284 0.7792 0.0610 -3.250 -0.2421 0.00866 0.00230 -0.0286 0.7748 0.0658 -3.000 -0.2132 0.00854 0.00219 -0.0287 0.7704 0.0698 -2.750 -0.1844 0.00843 0.00209 -0.0289 0.7662 0.0751 -2.500 -0.1553 0.00831 0.00200 -0.0291 0.7622 0.0809 -2.250 -0.1262 0.00819 0.00192 -0.0293 0.7575 0.0877 -2.000 -0.0972 0.00807 0.00184 -0.0295 0.7529 0.0957 -1.750 -0.0681 0.00797 0.00177 -0.0297 0.7487 0.1048 -1.500 -0.0390 0.00785 0.00171 -0.0299 0.7449 0.1177 -1.250 -0.0098 0.00772 0.00165 -0.0302 0.7394 0.1351 -1.000 0.0189 0.00759 0.00158 -0.0303 0.7293 0.1613 -0.750 0.0477 0.00739 0.00151 -0.0305 0.7175 0.2014 -0.500 0.0762 0.00715 0.00143 -0.0308 0.7034 0.2619 -0.250 0.1034 0.00640 0.00127 -0.0311 0.6835 0.4546 0.000 0.1315 0.00605 0.00122 -0.0313 0.6657 0.5634 0.250 0.1600 0.00589 0.00122 -0.0315 0.6471 0.6284 0.500 0.1888 0.00588 0.00125 -0.0316 0.6279 0.6609 0.750 0.2173 0.00595 0.00128 -0.0317 0.5970 0.6851 1.000 0.2447 0.00624 0.00136 -0.0316 0.5259 0.7065 1.250 0.2683 0.00725 0.00166 -0.0313 0.3343 0.7235 1.500 0.2938 0.00788 0.00190 -0.0312 0.2177 0.7404 1.750 0.3211 0.00816 0.00206 -0.0311 0.1733 0.7620 2.000 0.3488 0.00838 0.00219 -0.0311 0.1440 0.7741 2.250 0.3771 0.00856 0.00229 -0.0312 0.1263 0.7805 2.500 0.4054 0.00873 0.00240 -0.0313 0.1118 0.7857 2.750 0.4334 0.00889 0.00252 -0.0313 0.0994 0.7916 3.000 0.4615 0.00906 0.00264 -0.0313 0.0899 0.7984 3.250 0.4898 0.00921 0.00276 -0.0314 0.0828 0.8043 3.500 0.5177 0.00937 0.00290 -0.0313 0.0763 0.8099 3.750 0.5456 0.00953 0.00304 -0.0313 0.0710 0.8155 4.000 0.5737 0.00970 0.00318 -0.0314 0.0672 0.8208 4.250 0.6013 0.00986 0.00334 -0.0313 0.0634 0.8265 4.500 0.6289 0.01003 0.00350 -0.0313 0.0599 0.8328 4.750 0.6567 0.01020 0.00367 -0.0312 0.0568 0.8387 5.000 0.6839 0.01040 0.00385 -0.0311 0.0537 0.8443 5.250 0.7113 0.01056 0.00404 -0.0310 0.0515 0.8505 5.500 0.7385 0.01077 0.00423 -0.0309 0.0487 0.8567 5.750 0.7652 0.01096 0.00444 -0.0307 0.0465 0.8633 6.000 0.7920 0.01116 0.00465 -0.0305 0.0446 0.8713 6.250 0.8184 0.01137 0.00487 -0.0303 0.0425 0.8794 6.500 0.8445 0.01159 0.00510 -0.0299 0.0408 0.8885 6.750 0.8707 0.01180 0.00534 -0.0296 0.0394 0.8964 7.000 0.8963 0.01203 0.00559 -0.0292 0.0378 0.9052 7.250 0.9214 0.01229 0.00585 -0.0287 0.0363 0.9140 7.500 0.9464 0.01252 0.00611 -0.0282 0.0353 0.9247 7.750 0.9703 0.01273 0.00638 -0.0274 0.0343 0.9381 8.000 0.9938 0.01297 0.00665 -0.0266 0.0333 0.9560 8.250 1.0203 0.01325 0.00693 -0.0264 0.0322 0.9814 8.500 1.0472 0.01357 0.00726 -0.0265 0.0312 1.0000 8.750 1.0729 0.01387 0.00758 -0.0262 0.0304 1.0000 9.000 1.0982 0.01419 0.00791 -0.0259 0.0295 1.0000 9.250 1.1231 0.01454 0.00826 -0.0256 0.0287 1.0000 9.500 1.1476 0.01492 0.00864 -0.0252 0.0279 1.0000 9.750 1.1716 0.01532 0.00905 -0.0247 0.0272 1.0000 10.000 1.1959 0.01568 0.00944 -0.0243 0.0267 1.0000 10.250 1.2198 0.01605 0.00983 -0.0238 0.0260 1.0000 10.500 1.2432 0.01645 0.01024 -0.0233 0.0253 1.0000 10.750 1.2661 0.01687 0.01067 -0.0227 0.0245 1.0000 11.000 1.2883 0.01734 0.01115 -0.0220 0.0238 1.0000 11.250 1.3102 0.01780 0.01165 -0.0212 0.0234 1.0000 11.500 1.3320 0.01825 0.01213 -0.0205 0.0229 1.0000 11.750 1.3531 0.01872 0.01264 -0.0196 0.0224 1.0000 12.000 1.3734 0.01921 0.01316 -0.0187 0.0219 1.0000 12.250 1.3927 0.01973 0.01371 -0.0176 0.0215 1.0000 12.500 1.4097 0.02027 0.01428 -0.0161 0.0210 1.0000 12.750 1.4258 0.02088 0.01492 -0.0145 0.0206 1.0000 13.000 1.4411 0.02158 0.01566 -0.0130 0.0202 1.0000 13.250 1.4572 0.02222 0.01635 -0.0116 0.0199 1.0000 13.500 1.4728 0.02291 0.01710 -0.0103 0.0196 1.0000 13.750 1.4880 0.02365 0.01790 -0.0090 0.0193 1.0000 14.000 1.5027 0.02443 0.01874 -0.0077 0.0190 1.0000 14.250 1.5168 0.02527 0.01963 -0.0064 0.0186 1.0000 14.500 1.5303 0.02618 0.02058 -0.0052 0.0183 1.0000 14.750 1.5430 0.02716 0.02161 -0.0039 0.0180 1.0000 15.000 1.5546 0.02824 0.02275 -0.0027 0.0177 1.0000 15.250 1.5648 0.02946 0.02402 -0.0014 0.0174 1.0000 15.500 1.5736 0.03080 0.02543 -0.0002 0.0172 1.0000 15.750 1.5836 0.03207 0.02679 0.0009 0.0170 1.0000 16.000 1.5926 0.03346 0.02825 0.0019 0.0169 1.0000 16.250 1.6005 0.03496 0.02984 0.0029 0.0167 1.0000 16.500 1.6075 0.03658 0.03154 0.0038 0.0165 1.0000 16.750 1.6133 0.03835 0.03340 0.0047 0.0164 1.0000 17.000 1.6179 0.04025 0.03539 0.0054 0.0162 1.0000 17.250 1.6214 0.04233 0.03757 0.0060 0.0160 1.0000 17.500 1.6237 0.04460 0.03993 0.0065 0.0159 1.0000 17.750 1.6243 0.04709 0.04251 0.0068 0.0157 1.0000 18.000 1.6234 0.04983 0.04534 0.0070 0.0156 1.0000 18.250 1.6210 0.05288 0.04849 0.0068 0.0155 1.0000 18.500 1.6166 0.05631 0.05203 0.0064 0.0154 1.0000 18.750 1.6100 0.06017 0.05600 0.0056 0.0153 1.0000 19.000 1.6009 0.06459 0.06055 0.0043 0.0152 1.0000 19.250 1.5885 0.06972 0.06581 0.0025 0.0151 1.0000