XFOIL Version 6.94 Calculated polar for: SPICA 11.73% smoothed 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.300 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.4758 0.01276 0.00459 -0.0846 0.6247 0.0572 0.500 0.5269 0.01230 0.00413 -0.0834 0.6135 0.0710 1.000 0.6477 0.00980 0.00394 -0.0972 0.5997 1.0000 1.500 0.6945 0.00994 0.00391 -0.0952 0.5865 1.0000 2.000 0.7417 0.01013 0.00400 -0.0933 0.5740 1.0000 2.500 0.7899 0.01037 0.00410 -0.0916 0.5622 1.0000 3.000 0.8377 0.01055 0.00421 -0.0899 0.5491 1.0000 3.500 0.8851 0.01076 0.00439 -0.0881 0.5355 1.0000 4.000 0.9324 0.01098 0.00457 -0.0863 0.5209 1.0000 4.500 0.9796 0.01121 0.00476 -0.0844 0.5059 1.0000 5.000 1.0258 0.01144 0.00497 -0.0824 0.4886 1.0000 5.500 1.0714 0.01171 0.00523 -0.0804 0.4697 1.0000 6.000 1.1156 0.01204 0.00555 -0.0781 0.4478 1.0000 6.500 1.1584 0.01248 0.00593 -0.0757 0.4246 1.0000 7.000 1.1994 0.01302 0.00645 -0.0730 0.3993 1.0000 7.500 1.2381 0.01367 0.00705 -0.0700 0.3726 1.0000 8.000 1.2749 0.01443 0.00777 -0.0668 0.3478 1.0000 8.500 1.3092 0.01526 0.00858 -0.0632 0.3238 1.0000 9.000 1.3384 0.01622 0.00949 -0.0589 0.3011 1.0000 9.500 1.3609 0.01721 0.01047 -0.0535 0.2794 1.0000 10.000 1.3840 0.01829 0.01158 -0.0485 0.2604 1.0000 10.500 1.4055 0.01956 0.01290 -0.0438 0.2428 1.0000 11.000 1.4251 0.02106 0.01446 -0.0394 0.2263 1.0000 11.500 1.4423 0.02286 0.01635 -0.0354 0.2092 1.0000 12.000 1.4570 0.02507 0.01864 -0.0318 0.1896 1.0000 12.500 1.4681 0.02786 0.02149 -0.0288 0.1689 1.0000 13.000 1.4715 0.03160 0.02524 -0.0261 0.1423 1.0000 13.500 1.4570 0.03733 0.03081 -0.0236 0.1040 1.0000 14.000 1.4222 0.04559 0.03879 -0.0217 0.0572 1.0000 14.500 1.3921 0.05416 0.04727 -0.0210 0.0354 1.0000 15.000 1.3724 0.06231 0.05556 -0.0213 0.0301 1.0000 15.500 1.3583 0.07030 0.06378 -0.0223 0.0273 1.0000 16.000 1.3400 0.07933 0.07303 -0.0240 0.0257 1.0000 16.500 1.3167 0.08954 0.08345 -0.0267 0.0245 1.0000 17.000 1.2980 0.09940 0.09352 -0.0295 0.0235 1.0000 17.500 1.2872 0.10831 0.10264 -0.0324 0.0223 1.0000 18.000 1.2779 0.11707 0.11156 -0.0354 0.0213 1.0000 18.500 1.2721 0.12519 0.11980 -0.0384 0.0204 1.0000 19.000 1.2745 0.13130 0.12594 -0.0403 0.0193 1.0000 19.500 1.2821 0.13677 0.13156 -0.0420 0.0187 1.0000 20.000 1.2871 0.14306 0.13804 -0.0445 0.0181 1.0000 20.500 1.2912 0.14949 0.14468 -0.0474 0.0176 1.0000 21.000 1.2918 0.15681 0.15219 -0.0512 0.0168 1.0000 21.500 1.2914 0.16440 0.15996 -0.0555 0.0162 1.0000 22.000 1.2912 0.17190 0.16764 -0.0599 0.0158 1.0000 22.500 1.2840 0.18124 0.17723 -0.0656 0.0156 1.0000 23.000 1.2697 0.19257 0.18884 -0.0730 0.0155 1.0000 23.500 1.2429 0.20801 0.20461 -0.0834 0.0156 1.0000 25.500 0.8617 0.30427 0.30215 -0.1268 0.0244 1.0000 26.000 0.8635 0.31578 0.31367 -0.1311 0.0234 1.0000 26.500 0.8675 0.32569 0.32361 -0.1351 0.0209 1.0000 27.000 0.8754 0.33282 0.33078 -0.1379 0.0197 1.0000 27.500 0.8880 0.33974 0.33776 -0.1395 0.0191 1.0000 28.000 0.8829 0.35376 0.35177 -0.1454 0.0175 1.0000 28.500 0.8885 0.36203 0.36007 -0.1486 0.0158 1.0000 29.000 0.8947 0.36962 0.36771 -0.1515 0.0153 1.0000 29.500 0.9000 0.37919 0.37730 -0.1544 0.0149 1.0000 30.000 0.9008 0.39106 0.38920 -0.1588 0.0141 1.0000 30.500 0.9046 0.40063 0.39880 -0.1621 0.0130 1.0000 31.000 0.9086 0.40928 0.40749 -0.1652 0.0122 1.0000 31.500 0.9126 0.41731 0.41556 -0.1682 0.0118 1.0000 32.000 0.9183 0.42583 0.42412 -0.1704 0.0115 1.0000 32.500 0.9171 0.43845 0.43676 -0.1748 0.0111 1.0000 33.000 0.9195 0.44837 0.44671 -0.1780 0.0102 1.0000 33.500 0.9217 0.45748 0.45586 -0.1811 0.0096 1.0000 34.000 0.9236 0.46616 0.46458 -0.1841 0.0091 1.0000 34.500 0.9256 0.47414 0.47261 -0.1869 0.0087 1.0000 35.000 0.9272 0.48372 0.48221 -0.1896 0.0086 1.0000 35.500 0.9269 0.49515 0.49367 -0.1931 0.0084 1.0000 36.000 0.9276 0.50516 0.50371 -0.1961 0.0078 1.0000 36.500 0.9280 0.51442 0.51300 -0.1989 0.0071 1.0000 37.000 0.9279 0.52309 0.52172 -0.2018 0.0067 1.0000 37.500 0.9274 0.53124 0.52990 -0.2046 0.0064 1.0000 38.500 0.9257 0.55084 0.54956 -0.2101 0.0060 1.0000 39.000 0.9247 0.56057 0.55932 -0.2128 0.0055 1.0000 39.500 0.9232 0.56935 0.56814 -0.2155 0.0050 1.0000 40.000 0.9212 0.57757 0.57640 -0.2181 0.0048 1.0000 40.500 0.9188 0.58511 0.58397 -0.2208 0.0044 1.0000 41.500 0.9133 0.60267 0.60159 -0.2258 0.0042 1.0000 42.000 0.9109 0.61208 0.61104 -0.2282 0.0039 1.0000 42.500 0.9077 0.62027 0.61925 -0.2306 0.0035 1.0000 43.000 0.9039 0.62759 0.62660 -0.2329 0.0031 1.0000 43.500 0.8997 0.63437 0.63342 -0.2354 0.0029 1.0000 44.500 0.8912 0.65053 0.64963 -0.2398 0.0027 1.0000 45.000 0.8870 0.65853 0.65766 -0.2419 0.0023 1.0000 45.500 0.8820 0.66521 0.66437 -0.2441 0.0020 1.0000 46.000 0.8765 0.67121 0.67040 -0.2462 0.0018 1.0000 46.500 0.8702 0.67602 0.67525 -0.2484 0.0016 1.0000 47.000 0.8653 0.68462 0.68387 -0.2502 0.0015 1.0000 47.500 0.8597 0.69096 0.69023 -0.2521 0.0014 1.0000 48.000 0.8535 0.69662 0.69592 -0.2540 0.0011 1.0000 48.500 0.8468 0.70147 0.70080 -0.2559 0.0010 1.0000 49.000 0.8397 0.70537 0.70473 -0.2578 0.0008 1.0000 50.000 0.8256 0.71514 0.71454 -0.2612 0.0007 1.0000 50.500 0.8187 0.72000 0.71943 -0.2627 0.0006 1.0000 51.000 0.8109 0.72344 0.72289 -0.2643 0.0005 1.0000 51.500 0.8029 0.72628 0.72575 -0.2659 0.0004 1.0000 52.000 0.7945 0.72818 0.72768 -0.2674 0.0003 1.0000 53.500 0.7692 0.73527 0.73484 -0.2716 0.0002 1.0000 54.000 0.7606 0.73700 0.73659 -0.2728 0.0002 1.0000 54.500 0.7512 0.73712 0.73673 -0.2741 0.0001 1.0000 55.000 0.7420 0.73754 0.73717 -0.2753 0.0001 1.0000 55.500 0.7323 0.73686 0.73652 -0.2765 0.0000 1.0000 56.000 0.7222 0.73523 0.73492 -0.2777 0.0000 1.0000 56.500 0.7119 0.73329 0.73300 -0.2789 0.0000 1.0000 57.500 0.6925 0.73174 0.73148 -0.2806 0.0000 1.0000 58.000 0.6824 0.72968 0.72944 -0.2814 0.0000 1.0000 58.500 0.6721 0.72735 0.72713 -0.2822 0.0000 1.0000 59.000 0.6614 0.72363 0.72343 -0.2830 0.0000 1.0000 59.500 0.6506 0.71988 0.71970 -0.2837 0.0000 1.0000 60.000 0.6398 0.71563 0.71547 -0.2844 0.0000 1.0000