1.000000 .000000 .986564 .002523 .966059 .006377 .945268 .010588 .924259 .015117 .903119 .019941 .881883 .025057 .860571 .030449 .839191 .036096 .817746 .041973 .796235 .048047 .774663 .054279 .753049 .060625 .731430 .067044 .709849 .073487 .688359 .079869 .667013 .086099 .645833 .092095 .624817 .097777 .603947 .103065 .583183 .107888 .562470 .112196 .541750 .115972 .520988 .119234 .500174 .122008 .479311 .124306 .458409 .126137 .437483 .127501 .416545 .128394 .395607 .128814 .374682 .128769 .353796 .128274 .332992 .127334 .312308 .125936 .291786 .124084 .271485 .121790 .251482 .119060 .231867 .115905 .212747 .112351 .194251 .108433 .176518 .104196 .159689 .099707 .143893 .095043 .129232 .090283 .115762 .085502 .103492 .080765 .092386 .076127 .082375 .071624 .073370 .067277 .065275 .063097 .057993 .059085 .051431 .055235 .045509 .051540 .040150 .047990 .035293 .044573 .030882 .041276 .026868 .038090 .023213 .035004 .019884 .032006 .016853 .029085 .014095 .026234 .011596 .023444 .009344 .020705 .007326 .018012 .005536 .015357 .003971 .012731 .002627 .010130 .001530 .007553 .000721 .005004 .000219 .002487 .000077 .001251 .000000 .000000 .000198 -.002373 .000934 -.004609 .002241 -.006727 .004073 -.008534 .006343 -.009942 .008928 -.011007 .011725 -.011835 .014714 -.012494 .017883 -.013048 .021242 -.013512 .024806 -.013901 .028590 -.014231 .032618 -.014505 .036917 -.014724 .041519 -.014891 .046460 -.015012 .051785 -.015085 .057544 -.015107 .063799 -.015077 .070618 -.014994 .078085 -.014855 .086291 -.014651 .095338 -.014374 .105341 -.014016 .116415 -.013565 .128665 -.013012 .142176 -.012348 .156988 -.011569 .173082 -.010675 .190376 -.009675 .208729 -.008581 .227962 -.007410 .247890 -.006183 .268338 -.004917 .289155 -.003630 .310224 -.002336 .331455 -.001046 .352786 .000224 .374179 .001464 .395605 .002672 .417040 .003836 .438476 .004945 .459906 .005999 .481321 .006993 .502713 .007917 .524081 .008756 .545431 .009504 .566767 .010158 .588088 .010715 .609397 .011168 .630700 .011514 .652000 .011758 .673295 .011898 .694586 .011935 .715872 .011871 .737148 .011708 .758404 .011445 .779634 .011074 .800834 .010592 .821997 .009995 .843114 .009278 .864172 .008443 .885146 .007487 .906010 .006408 .926724 .005215 .947217 .003919 .967390 .002516 .987138 .001010 1.000000 .000000 XFOIL Version 6.8 Calculated polar for: DAE-11 AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = .000 Re = .500 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top Xtr Bot Xtr ------- -------- --------- --------- -------- ------- ------- -1.000 .5457 .01151 .00452 -.1278 .6523 .0465 -.500 .6040 .01100 .00426 -.1285 .6481 .1290 .000 .6612 .01020 .00429 -.1295 .6428 .4137 .500 .7115 .00916 .00435 -.1285 .6381 .8122 1.000 .7718 .00901 .00421 -.1290 .6336 1.0000 1.500 .8295 .00913 .00429 -.1296 .6280 1.0000 2.000 .8874 .00920 .00427 -.1302 .6223 1.0000 2.500 .9453 .00928 .00421 -.1306 .6172 1.0000 3.000 1.0022 .00941 .00437 -.1311 .6104 1.0000 3.500 1.0594 .00946 .00437 -.1316 .6036 1.0000 4.000 1.1161 .00959 .00447 -.1320 .5970 1.0000 4.500 1.1723 .00968 .00460 -.1324 .5884 1.0000 5.000 1.2284 .00981 .00471 -.1328 .5804 1.0000 5.500 1.2836 .00993 .00491 -.1331 .5703 1.0000 6.000 1.3383 .01012 .00514 -.1333 .5594 1.0000 6.500 1.3921 .01033 .00536 -.1334 .5472 1.0000 7.000 1.4447 .01062 .00566 -.1333 .5329 1.0000 7.500 1.4957 .01099 .00609 -.1331 .5162 1.0000 8.000 1.5450 .01146 .00663 -.1327 .4965 1.0000 8.500 1.5912 .01208 .00729 -.1319 .4729 1.0000 9.000 1.6313 .01297 .00814 -.1302 .4449 1.0000 9.500 1.6610 .01425 .00936 -.1273 .4116 1.0000 10.000 1.6664 .01643 .01149 -.1216 .3797 1.0000