XFOIL Version 6.96 Calculated polar for: WORTMANN FX 80-080 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -10.500 -0.4637 0.12202 0.11673 -0.0272 1.0000 0.0412 -10.250 -0.4651 0.11908 0.11386 -0.0303 1.0000 0.0416 -10.000 -0.4647 0.11585 0.11068 -0.0328 1.0000 0.0418 -9.750 -0.4645 0.11228 0.10718 -0.0350 1.0000 0.0419 -9.500 -0.4585 0.10651 0.10145 -0.0333 1.0000 0.0429 -9.250 -0.4517 0.10274 0.09769 -0.0325 1.0000 0.0438 -9.000 -0.4485 0.09929 0.09428 -0.0330 1.0000 0.0443 -8.750 -0.4471 0.09572 0.09076 -0.0337 1.0000 0.0448 -8.500 -0.3513 0.07429 0.06978 -0.0392 1.0000 0.0402 -8.000 -0.3700 0.06453 0.06014 -0.0416 1.0000 0.0286 -7.750 -0.3778 0.06111 0.05680 -0.0406 1.0000 0.0279 -7.500 -0.3928 0.05831 0.05411 -0.0394 1.0000 0.0276 -7.250 -0.4719 0.07138 0.06676 -0.0436 1.0000 0.0281 -7.000 -0.4769 0.06819 0.06359 -0.0428 1.0000 0.0273 -6.750 -0.4821 0.06509 0.06049 -0.0418 1.0000 0.0267 -6.500 -0.4868 0.06168 0.05702 -0.0409 1.0000 0.0261 -6.250 -0.4881 0.05828 0.05353 -0.0400 1.0000 0.0254 -6.000 -0.4639 0.05214 0.04708 -0.0452 0.9946 0.0244 -5.750 -0.4378 0.04625 0.04079 -0.0493 0.9894 0.0235 -5.500 -0.4123 0.04107 0.03514 -0.0520 0.9839 0.0229 -5.250 -0.3831 0.03629 0.02980 -0.0544 0.9796 0.0226 -5.000 -0.3553 0.03248 0.02543 -0.0557 0.9751 0.0231 -4.750 -0.3263 0.02987 0.02231 -0.0568 0.9709 0.0257 -4.500 -0.2946 0.02735 0.01919 -0.0578 0.9678 0.0278 -4.250 -0.2623 0.02495 0.01619 -0.0587 0.9652 0.0285 -4.000 -0.2347 0.02321 0.01407 -0.0586 0.9608 0.0292 -3.750 -0.2054 0.02123 0.01190 -0.0591 0.9575 0.0310 -3.500 -0.1745 0.01998 0.01057 -0.0599 0.9547 0.0337 -3.250 -0.1415 0.01927 0.00968 -0.0611 0.9523 0.0416 -3.000 -0.1166 0.01823 0.00865 -0.0608 0.9474 0.0474 -2.750 -0.0871 0.01744 0.00781 -0.0613 0.9436 0.0611 -2.500 -0.0554 0.01672 0.00710 -0.0624 0.9407 0.0938 -2.250 -0.0247 0.01556 0.00663 -0.0638 0.9383 0.2345 -2.000 -0.0114 0.01407 0.00684 -0.0610 0.9328 0.6540 -1.750 0.0100 0.01405 0.00698 -0.0586 0.9285 0.7882 -1.500 0.0349 0.01403 0.00695 -0.0570 0.9255 0.8497 -1.250 0.0531 0.01398 0.00688 -0.0539 0.9202 0.9103 -1.000 0.1345 0.01386 0.00661 -0.0639 0.9256 0.9854 -0.750 0.1696 0.01390 0.00650 -0.0661 0.9216 1.0000 -0.500 0.1947 0.01394 0.00641 -0.0661 0.9157 1.0000 -0.250 0.2276 0.01395 0.00632 -0.0676 0.9122 1.0000 0.000 0.2495 0.01406 0.00635 -0.0670 0.9055 1.0000 0.250 0.2795 0.01413 0.00635 -0.0679 0.9009 1.0000 0.500 0.3143 0.01416 0.00634 -0.0696 0.8977 1.0000 0.750 0.3359 0.01434 0.00648 -0.0688 0.8903 1.0000 1.000 0.3683 0.01442 0.00654 -0.0700 0.8862 1.0000 1.250 0.3976 0.01453 0.00665 -0.0706 0.8807 1.0000 1.500 0.4259 0.01464 0.00680 -0.0709 0.8742 1.0000 1.750 0.4624 0.01464 0.00683 -0.0726 0.8701 1.0000 2.000 0.4856 0.01480 0.00704 -0.0719 0.8610 1.0000 2.250 0.5202 0.01478 0.00708 -0.0731 0.8551 1.0000 2.500 0.5478 0.01482 0.00720 -0.0729 0.8453 1.0000 2.750 0.5767 0.01478 0.00730 -0.0728 0.8339 1.0000 3.000 0.6071 0.01461 0.00722 -0.0727 0.8200 1.0000 3.250 0.6397 0.01426 0.00697 -0.0726 0.8018 1.0000 3.500 0.6633 0.01409 0.00688 -0.0710 0.7784 1.0000 3.750 0.6876 0.01392 0.00681 -0.0695 0.7518 1.0000 4.000 0.7129 0.01375 0.00677 -0.0682 0.7188 1.0000 4.250 0.7345 0.01370 0.00677 -0.0662 0.6706 1.0000 4.500 0.7590 0.01376 0.00645 -0.0644 0.5572 1.0000 4.750 0.7693 0.01497 0.00669 -0.0607 0.3868 1.0000 5.000 0.7785 0.01648 0.00740 -0.0577 0.2465 1.0000 5.250 0.7936 0.01773 0.00819 -0.0559 0.1617 1.0000 5.500 0.8106 0.01888 0.00911 -0.0543 0.1122 1.0000 5.750 0.8287 0.01994 0.01004 -0.0529 0.0825 1.0000 6.000 0.8466 0.02104 0.01100 -0.0514 0.0634 1.0000 6.250 0.8653 0.02209 0.01215 -0.0500 0.0524 1.0000 6.500 0.8830 0.02337 0.01356 -0.0482 0.0458 1.0000 6.750 0.9014 0.02471 0.01496 -0.0468 0.0406 1.0000 7.000 0.9214 0.02611 0.01650 -0.0456 0.0348 1.0000 7.250 0.9428 0.02772 0.01826 -0.0446 0.0310 1.0000 7.500 0.9642 0.02983 0.02053 -0.0437 0.0280 1.0000 7.750 0.9863 0.03185 0.02289 -0.0428 0.0237 1.0000 8.000 1.0075 0.03428 0.02568 -0.0417 0.0212 1.0000 8.250 1.0251 0.03682 0.02853 -0.0403 0.0195 1.0000 8.500 1.0373 0.03956 0.03148 -0.0388 0.0177 1.0000 8.750 1.0472 0.04262 0.03508 -0.0364 0.0162 1.0000 9.000 1.0533 0.04601 0.03901 -0.0338 0.0149 1.0000 9.250 1.0532 0.04992 0.04341 -0.0308 0.0146 1.0000 9.500 1.0479 0.05387 0.04777 -0.0276 0.0144 1.0000 9.750 1.0372 0.05759 0.05183 -0.0241 0.0143 1.0000 10.000 1.0225 0.06119 0.05571 -0.0208 0.0143 1.0000 10.250 1.0044 0.06512 0.05988 -0.0183 0.0143 1.0000 10.500 0.9856 0.06934 0.06431 -0.0171 0.0144 1.0000 10.750 0.9653 0.07418 0.06933 -0.0173 0.0145 1.0000 11.000 0.9454 0.07962 0.07493 -0.0189 0.0146 1.0000 11.250 0.9240 0.08637 0.08180 -0.0224 0.0148 1.0000