XFOIL Version 6.96 Calculated polar for: CAST 10-2/DOA 2 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 ------ -------- --------- --------- -------- -------- -------- -11.000 -0.5478 0.07736 0.07561 -0.0619 0.9758 0.0067 -10.750 -0.5855 0.06593 0.06404 -0.0709 0.9612 0.0067 -10.500 -0.6129 0.05989 0.05784 -0.0732 0.9486 0.0067 -10.250 -0.6338 0.05567 0.05346 -0.0726 0.9381 0.0067 -10.000 -0.6443 0.05178 0.04939 -0.0714 0.9306 0.0067 -9.750 -0.6473 0.04792 0.04534 -0.0705 0.9253 0.0068 -9.500 -0.6471 0.04391 0.04111 -0.0694 0.9202 0.0069 -9.250 -0.6432 0.04008 0.03704 -0.0681 0.9159 0.0070 -8.750 -0.6623 0.02054 0.01581 -0.0609 0.9062 0.0083 -8.500 -0.6417 0.01866 0.01365 -0.0602 0.9034 0.0086 -8.250 -0.6186 0.01758 0.01240 -0.0599 0.9009 0.0087 -8.000 -0.5959 0.01638 0.01102 -0.0594 0.8985 0.0089 -7.750 -0.5716 0.01557 0.01012 -0.0592 0.8962 0.0091 -7.500 -0.5462 0.01502 0.00952 -0.0592 0.8936 0.0092 -7.250 -0.5205 0.01457 0.00902 -0.0591 0.8911 0.0094 -7.000 -0.4947 0.01411 0.00851 -0.0591 0.8887 0.0096 -6.750 -0.4688 0.01365 0.00799 -0.0590 0.8865 0.0098 -6.500 -0.4431 0.01315 0.00743 -0.0589 0.8843 0.0100 -6.250 -0.4173 0.01267 0.00689 -0.0588 0.8822 0.0103 -6.000 -0.3911 0.01219 0.00637 -0.0588 0.8799 0.0106 -5.750 -0.3649 0.01175 0.00588 -0.0588 0.8776 0.0109 -5.500 -0.3384 0.01136 0.00545 -0.0588 0.8754 0.0112 -5.250 -0.3113 0.01107 0.00512 -0.0589 0.8733 0.0114 -5.000 -0.2852 0.01061 0.00462 -0.0589 0.8712 0.0119 -4.750 -0.2583 0.01029 0.00428 -0.0590 0.8691 0.0123 -4.500 -0.2308 0.01003 0.00400 -0.0591 0.8671 0.0127 -4.250 -0.2031 0.00976 0.00373 -0.0594 0.8651 0.0131 -4.000 -0.1753 0.00952 0.00347 -0.0596 0.8631 0.0135 -3.750 -0.1474 0.00928 0.00322 -0.0598 0.8611 0.0140 -3.500 -0.1193 0.00907 0.00299 -0.0601 0.8590 0.0145 -3.250 -0.0910 0.00889 0.00279 -0.0603 0.8569 0.0148 -3.000 -0.0630 0.00865 0.00255 -0.0606 0.8549 0.0159 -2.750 -0.0345 0.00851 0.00240 -0.0609 0.8531 0.0169 -2.500 -0.0059 0.00836 0.00226 -0.0612 0.8513 0.0177 -2.250 0.0229 0.00823 0.00213 -0.0616 0.8494 0.0186 -2.000 0.0516 0.00808 0.00200 -0.0620 0.8473 0.0200 -1.750 0.0803 0.00796 0.00189 -0.0623 0.8438 0.0223 -1.500 0.1087 0.00785 0.00177 -0.0625 0.8388 0.0264 -1.250 0.1372 0.00772 0.00167 -0.0627 0.8322 0.0342 -1.000 0.1600 0.00570 0.00124 -0.0633 0.8257 0.5518 -0.750 0.1884 0.00556 0.00123 -0.0636 0.8188 0.6003 -0.500 0.2169 0.00553 0.00119 -0.0637 0.8087 0.6195 -0.250 0.2452 0.00550 0.00117 -0.0639 0.7955 0.6370 0.000 0.2736 0.00549 0.00116 -0.0640 0.7814 0.6523 0.250 0.3017 0.00552 0.00115 -0.0641 0.7644 0.6598 0.500 0.3297 0.00559 0.00114 -0.0642 0.7428 0.6657 0.750 0.3564 0.00571 0.00115 -0.0640 0.7077 0.6713 1.000 0.3809 0.00603 0.00122 -0.0634 0.6452 0.6747 1.250 0.4026 0.00660 0.00140 -0.0624 0.5508 0.6780 1.500 0.4257 0.00710 0.00158 -0.0617 0.4741 0.6809 1.750 0.4487 0.00759 0.00176 -0.0610 0.3976 0.6840 2.000 0.4724 0.00802 0.00194 -0.0605 0.3331 0.6876 2.250 0.4979 0.00831 0.00207 -0.0602 0.2933 0.6913 2.500 0.5243 0.00852 0.00219 -0.0601 0.2680 0.6950 2.750 0.5505 0.00874 0.00231 -0.0600 0.2449 0.6985 3.000 0.5765 0.00896 0.00245 -0.0599 0.2195 0.7022 3.250 0.6024 0.00920 0.00260 -0.0597 0.1966 0.7060 3.500 0.6286 0.00941 0.00274 -0.0596 0.1793 0.7100 3.750 0.6546 0.00963 0.00290 -0.0594 0.1621 0.7140 4.000 0.6807 0.00983 0.00307 -0.0592 0.1477 0.7184 4.250 0.7069 0.01002 0.00323 -0.0591 0.1378 0.7231 4.500 0.7330 0.01022 0.00339 -0.0590 0.1283 0.7274 4.750 0.7592 0.01041 0.00358 -0.0588 0.1192 0.7317 5.000 0.7849 0.01062 0.00377 -0.0586 0.1095 0.7366 5.250 0.8103 0.01086 0.00397 -0.0584 0.0984 0.7419 5.500 0.8354 0.01112 0.00419 -0.0581 0.0867 0.7471 5.750 0.8601 0.01141 0.00444 -0.0577 0.0742 0.7529 6.000 0.8847 0.01171 0.00470 -0.0573 0.0638 0.7586 6.250 0.9090 0.01202 0.00498 -0.0569 0.0520 0.7642 6.500 0.9312 0.01253 0.00538 -0.0561 0.0317 0.7707 6.750 0.9548 0.01291 0.00574 -0.0556 0.0250 0.7772 7.000 0.9789 0.01321 0.00608 -0.0551 0.0221 0.7849 7.250 1.0031 0.01350 0.00640 -0.0546 0.0207 0.7925 7.500 1.0269 0.01382 0.00677 -0.0541 0.0194 0.8011 7.750 1.0501 0.01418 0.00717 -0.0535 0.0181 0.8095 8.000 1.0738 0.01448 0.00753 -0.0529 0.0175 0.8195 8.250 1.0971 0.01477 0.00790 -0.0523 0.0169 0.8311 8.500 1.1199 0.01508 0.00829 -0.0516 0.0162 0.8450 8.750 1.1419 0.01541 0.00870 -0.0508 0.0154 0.8622 9.000 1.1628 0.01577 0.00915 -0.0497 0.0147 0.8845 9.250 1.1806 0.01617 0.00968 -0.0480 0.0139 0.9179 9.500 1.1991 0.01640 0.01003 -0.0463 0.0136 1.0000 9.750 1.2204 0.01681 0.01049 -0.0454 0.0133 1.0000 10.000 1.2403 0.01724 0.01096 -0.0443 0.0129 1.0000 10.250 1.2597 0.01770 0.01146 -0.0431 0.0125 1.0000 10.500 1.2789 0.01818 0.01199 -0.0419 0.0121 1.0000 10.750 1.2976 0.01870 0.01254 -0.0406 0.0118 1.0000 11.000 1.3158 0.01925 0.01313 -0.0393 0.0114 1.0000 11.250 1.3330 0.01989 0.01380 -0.0379 0.0111 1.0000 11.500 1.3482 0.02066 0.01465 -0.0362 0.0107 1.0000 11.750 1.3648 0.02130 0.01535 -0.0348 0.0105 1.0000 12.000 1.3815 0.02193 0.01604 -0.0335 0.0103 1.0000 12.250 1.3974 0.02260 0.01678 -0.0320 0.0101 1.0000 12.500 1.4125 0.02333 0.01758 -0.0305 0.0099 1.0000 12.750 1.4265 0.02413 0.01845 -0.0289 0.0097 1.0000 13.000 1.4402 0.02495 0.01935 -0.0273 0.0095 1.0000 13.250 1.4531 0.02584 0.02031 -0.0257 0.0094 1.0000 13.500 1.4653 0.02677 0.02131 -0.0241 0.0092 1.0000 13.750 1.4769 0.02775 0.02237 -0.0224 0.0090 1.0000 14.000 1.4873 0.02882 0.02352 -0.0208 0.0089 1.0000 14.250 1.4967 0.02998 0.02475 -0.0190 0.0087 1.0000 14.500 1.5048 0.03126 0.02611 -0.0173 0.0086 1.0000 14.750 1.5112 0.03270 0.02763 -0.0155 0.0084 1.0000 15.000 1.5150 0.03436 0.02939 -0.0136 0.0083 1.0000 15.250 1.5152 0.03638 0.03152 -0.0116 0.0081 1.0000 15.500 1.5157 0.03844 0.03370 -0.0099 0.0080 1.0000 15.750 1.5195 0.04027 0.03563 -0.0086 0.0079 1.0000 16.000 1.5216 0.04232 0.03779 -0.0074 0.0078 1.0000 16.250 1.5220 0.04463 0.04022 -0.0063 0.0078 1.0000 16.500 1.5201 0.04726 0.04296 -0.0054 0.0077 1.0000 16.750 1.5162 0.05028 0.04611 -0.0048 0.0076 1.0000 17.000 1.5106 0.05374 0.04970 -0.0046 0.0076 1.0000 17.250 1.5031 0.05768 0.05378 -0.0050 0.0075 1.0000 17.500 1.4928 0.06230 0.05854 -0.0059 0.0075 1.0000 17.750 1.4793 0.06781 0.06420 -0.0078 0.0074 1.0000 18.000 1.4622 0.07443 0.07098 -0.0106 0.0074 1.0000 18.250 1.4393 0.08256 0.07929 -0.0147 0.0074 1.0000 18.500 1.4097 0.09232 0.08923 -0.0198 0.0074 1.0000 18.750 1.3746 0.10328 0.10038 -0.0255 0.0074 1.0000 19.000 1.3350 0.11494 0.11220 -0.0314 0.0075 1.0000