XFOIL Version 6.96 Calculated polar for: UNIVERSITY OF ALBERTA UA 79-SF-187 AIRFOIL MAIN 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.100 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -10.500 -0.3635 0.10875 0.10499 -0.0448 -0.0009 4.3309 -10.250 -0.3373 0.10620 0.10241 -0.0413 -0.0009 4.3212 -10.000 -0.3558 0.10275 0.09904 -0.0433 -0.0009 4.3092 -9.750 -0.3457 0.09964 0.09594 -0.0419 -0.0009 4.3009 -9.500 -0.3506 0.09682 0.09316 -0.0421 -0.0009 4.2864 -9.250 -0.3582 0.09337 0.08976 -0.0426 -0.0009 4.2764 -9.000 -0.3534 0.09095 0.08736 -0.0416 -0.0009 4.2611 -8.750 -0.3733 0.08744 0.08393 -0.0433 -0.0009 4.2476 -8.500 -0.3615 0.08518 0.08168 -0.0415 -0.0009 4.2306 -8.250 -0.3848 0.08179 0.07836 -0.0433 -0.0009 4.2136 -8.000 -0.3745 0.07958 0.07617 -0.0415 -0.0009 4.1943 -7.750 -0.3910 0.07640 0.07306 -0.0423 -0.0009 4.1739 -7.500 -0.4027 0.07399 0.07069 -0.0424 -0.0009 4.1505 -7.250 -0.4003 0.07124 0.06797 -0.0413 -0.0009 4.1280 -7.000 -0.4432 0.06856 0.06537 -0.0429 -0.0009 4.1080 -5.500 -0.4956 0.03617 0.03064 -0.0428 -0.0009 4.4366 -5.250 -0.4852 0.03358 0.02774 -0.0409 -0.0009 4.4426 -5.000 -0.4742 0.03135 0.02510 -0.0388 -0.0009 4.4466 -4.750 -0.4624 0.02955 0.02314 -0.0371 -0.0009 4.4483 -4.500 -0.4495 0.02795 0.02114 -0.0350 -0.0009 4.4501 -4.250 -0.4366 0.02660 0.01969 -0.0334 -0.0009 4.4507 -4.000 -0.4231 0.02541 0.01834 -0.0317 -0.0009 4.4513 -3.750 -0.4093 0.02440 0.01720 -0.0300 -0.0009 4.4516 -3.500 -0.3956 0.02352 0.01625 -0.0284 -0.0009 4.4516 -3.250 -0.3821 0.02277 0.01546 -0.0269 -0.0009 4.4513 -3.000 -0.3693 0.02212 0.01480 -0.0253 -0.0009 4.4508 -2.750 -0.3572 0.02157 0.01421 -0.0237 -0.0009 4.4499 -2.500 -0.3462 0.02102 0.01370 -0.0222 -0.0009 4.4484 -2.250 -0.1692 0.03310 0.02837 -0.0241 -0.0009 2.0490 -2.000 -0.1415 0.03496 0.02998 -0.0240 -0.0009 2.0009 -1.750 -0.1392 0.03436 0.02927 -0.0228 -0.0009 2.0009 -1.500 -0.1364 0.03382 0.02862 -0.0216 -0.0009 2.0009 -1.250 -0.1332 0.03333 0.02802 -0.0204 -0.0009 2.0009 -1.000 -0.1182 0.03251 0.02707 -0.0205 -0.0005 2.0009 -0.750 -0.0991 0.03265 0.02705 -0.0211 -0.0001 2.0009 -0.500 -0.0898 0.03197 0.02627 -0.0205 0.0001 2.0009 -0.250 -0.0739 0.03183 0.02599 -0.0205 0.0000 2.0009 0.000 -0.0544 0.03337 0.02739 -0.0211 -0.0002 2.0009 0.250 -0.0505 0.03158 0.02556 -0.0196 -0.0011 2.0009 0.500 -0.0316 0.03245 0.02630 -0.0199 -0.0015 2.0009 0.750 -0.0279 0.03157 0.02538 -0.0184 -0.0015 2.0009 1.000 -0.0098 0.03222 0.02592 -0.0185 -0.0010 2.0009 1.250 -0.0062 0.03170 0.02536 -0.0170 -0.0004 2.0009 1.500 0.0112 0.03225 0.02583 -0.0170 0.0000 2.0009 1.750 0.0152 0.03192 0.02548 -0.0156 -0.0001 2.0009 2.000 0.0335 0.03259 0.02607 -0.0156 -0.0004 2.0009 2.250 0.0367 0.03215 0.02561 -0.0141 -0.0001 2.0009 2.500 0.0576 0.03328 0.02667 -0.0143 0.0010 2.0009 2.750 0.0622 0.03270 0.02608 -0.0129 0.0053 2.0009 3.000 0.0686 0.03271 0.02606 -0.0117 0.0105 2.0009 3.250 0.0906 0.03371 0.02701 -0.0120 0.0164 2.0009 3.500 0.1001 0.03352 0.02681 -0.0110 0.0262 2.0009 3.750 0.1119 0.03353 0.02679 -0.0101 0.0374 2.0009 4.000 0.1548 0.03287 0.02603 -0.0109 0.0885 2.0009 4.250 0.1772 0.03288 0.02601 -0.0106 0.1169 2.0009 4.500 0.1926 0.03280 0.02591 -0.0098 0.1452 2.0009 4.750 0.2049 0.03278 0.02589 -0.0088 0.1721 2.0009 5.000 0.2190 0.03285 0.02596 -0.0079 0.1968 2.0009 5.250 0.2453 0.03310 0.02620 -0.0078 0.2135 2.0009 5.500 0.2521 0.03306 0.02619 -0.0064 0.2428 2.0009 5.750 0.2608 0.03309 0.02625 -0.0052 0.2731 2.0009 6.000 0.2725 0.03323 0.02640 -0.0042 0.3020 2.0009 6.250 0.2957 0.03338 0.02658 -0.0038 0.3231 2.0009 6.500 0.2999 0.03348 0.02671 -0.0023 0.3605 2.0009 6.750 0.3091 0.03367 0.02697 -0.0011 0.3935 2.0009 7.000 0.3315 0.03377 0.02710 -0.0006 0.4165 2.0009 7.250 0.3339 0.03397 0.02736 0.0009 0.4568 2.0009 7.500 0.3642 0.03400 0.02744 0.0011 0.4725 2.0009 7.750 0.3634 0.03423 0.02772 0.0028 0.5172 2.0009 8.000 0.3675 0.03449 0.02805 0.0042 0.5571 2.0009 8.250 0.3945 0.03434 0.02797 0.0047 0.5772 2.0009 8.500 0.3939 0.03469 0.02839 0.0063 0.6234 2.0009 8.750 0.4270 0.03434 0.02811 0.0067 0.6375 2.0009 9.000 0.4234 0.03475 0.02860 0.0084 0.6883 2.0009 9.250 0.4219 0.03523 0.02916 0.0099 0.7372 2.0009 9.500 0.4542 0.03468 0.02871 0.0105 0.7535 2.0009 9.750 0.4486 0.03530 0.02941 0.0121 0.8079 2.0009 10.000 0.4467 0.03590 0.03010 0.0135 0.8592 2.0009 10.250 0.4766 0.03526 0.02958 0.0144 0.8790 2.0009 10.750 0.4693 0.03671 0.03120 0.0171 0.9883 2.0009 11.000 0.4983 0.03588 0.03052 0.0183 1.0123 2.0009 11.250 0.4929 0.03670 0.03143 0.0195 1.0720 2.0009 11.500 0.4946 0.03719 0.03203 0.0208 1.1264 2.0009 11.750 0.6889 0.01668 0.01151 0.0285 1.4225 2.0009 12.000 0.6851 0.01674 0.01144 0.0309 1.6202 2.0009 12.250 0.6775 0.01725 0.01188 0.0330 1.8100 2.0009 12.500 0.6691 0.01787 0.01238 0.0350 2.0286 2.0009 12.750 0.6568 0.01878 0.01311 0.0368 2.3119 2.0009 13.000 0.6420 0.01994 0.01407 0.0383 2.6191 2.0009 13.250 0.6272 0.02127 0.01520 0.0396 2.9607 2.0009 13.500 0.6091 0.02293 0.01658 0.0406 3.3995 2.0009 13.750 0.5928 0.02460 0.01804 0.0413 3.7171 2.0009 14.000 0.5834 0.02594 0.01937 0.0421 3.8111 2.0009 14.250 0.5773 0.02706 0.02059 0.0427 3.8448 2.0009 14.500 0.5709 0.02828 0.02191 0.0433 3.8700 2.0009 14.750 0.5642 0.02954 0.02328 0.0436 3.8866 2.0009 15.000 0.5581 0.03081 0.02466 0.0439 3.8957 2.0009 15.250 0.5520 0.03212 0.02611 0.0442 3.9055 2.0009 15.500 0.5460 0.03347 0.02759 0.0443 3.9119 2.0009 15.750 0.5399 0.03486 0.02909 0.0443 3.9188 2.0009 16.000 0.5341 0.03624 0.03056 0.0444 3.9242 2.0009 16.250 0.5300 0.03743 0.03184 0.0445 3.9289 2.0009 16.500 0.5285 0.03833 0.03285 0.0448 3.9326 2.0009 16.750 0.5300 0.03894 0.03354 0.0454 3.9368 2.0009 17.000 0.5373 0.03889 0.03355 0.0466 3.9422 2.0009 17.250 0.5616 0.03720 0.03188 0.0494 3.9484 2.0009 17.500 0.5995 0.03545 0.03014 0.0530 3.9492 2.0009 17.750 0.6248 0.03550 0.03034 0.0552 3.9447 2.0009 18.000 0.6351 0.03656 0.03158 0.0562 3.9394 2.0009 18.250 0.6372 0.03801 0.03322 0.0568 3.9346 2.0009 18.500 0.6385 0.03958 0.03494 0.0572 3.9296 2.0009 18.750 0.6314 0.04138 0.03693 0.0570 3.9254 2.0009 19.000 0.6050 0.04389 0.03972 0.0553 3.9211 2.0009 19.250 0.5808 0.04694 0.04302 0.0533 3.9161 2.0009