XFOIL Version 6.94 Calculated polar for: DORNIER A-5 AIRFOIL 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 0.3760 0.01253 0.00725 -0.0936 0.8321 0.7038 0.500 0.4404 0.01259 0.00729 -0.0949 0.8207 0.7113 1.000 0.5005 0.01265 0.00732 -0.0954 0.8068 0.7201 1.500 0.5591 0.01269 0.00736 -0.0956 0.7923 0.7252 2.000 0.6032 0.01262 0.00730 -0.0930 0.7739 0.7323 2.500 0.6436 0.01247 0.00717 -0.0894 0.7493 0.7392 3.000 0.6848 0.01233 0.00703 -0.0860 0.7215 0.7451 3.500 0.7232 0.01227 0.00690 -0.0822 0.6863 0.7532 4.000 0.7589 0.01241 0.00688 -0.0777 0.6376 0.7593 4.500 0.7792 0.01288 0.00700 -0.0703 0.5594 0.7667 5.000 0.7888 0.01385 0.00749 -0.0614 0.4593 0.7751 5.500 0.8022 0.01498 0.00824 -0.0537 0.3937 0.7821 6.000 0.8316 0.01575 0.00888 -0.0492 0.3560 0.7892 6.500 0.8596 0.01664 0.00957 -0.0448 0.3117 0.7969 7.000 0.8863 0.01750 0.01028 -0.0401 0.2520 0.8033 8.000 0.9346 0.02000 0.01231 -0.0312 0.1732 0.8163 8.500 0.9629 0.02111 0.01341 -0.0275 0.1569 0.8228 9.000 0.9935 0.02224 0.01450 -0.0244 0.1379 0.8299 9.500 1.0258 0.02317 0.01549 -0.0215 0.1241 0.8358 10.000 1.0594 0.02419 0.01653 -0.0191 0.1111 0.8416 10.500 1.0874 0.02549 0.01782 -0.0161 0.0990 0.8474 11.000 1.1120 0.02720 0.01953 -0.0132 0.0898 0.8529 11.500 1.1402 0.02863 0.02107 -0.0106 0.0789 0.8590 12.000 1.1706 0.03007 0.02263 -0.0086 0.0716 0.8649 12.500 1.1966 0.03183 0.02450 -0.0063 0.0642 0.8707 13.000 1.2207 0.03393 0.02665 -0.0044 0.0569 0.8761 13.500 1.2420 0.03634 0.02912 -0.0025 0.0496 0.8824 14.000 1.2666 0.03879 0.03176 -0.0013 0.0450 0.8882 14.500 1.2873 0.04183 0.03494 -0.0005 0.0404 0.8946 15.000 1.3068 0.04534 0.03856 -0.0004 0.0340 0.9016 15.500 1.3251 0.04939 0.04279 -0.0009 0.0294 0.9115 16.000 1.3475 0.05406 0.04778 -0.0037 0.0274 0.9688 16.500 1.3475 0.05923 0.05311 -0.0028 0.0248 1.0000 17.000 1.3513 0.06506 0.05914 -0.0038 0.0222 1.0000 17.500 1.3503 0.07178 0.06608 -0.0055 0.0193 1.0000 18.000 1.3440 0.07955 0.07408 -0.0079 0.0178 1.0000 18.500 1.3281 0.08917 0.08393 -0.0117 0.0117 1.0000 19.000 1.2917 0.10262 0.09758 -0.0180 0.0077 1.0000 19.500 1.2630 0.11539 0.11063 -0.0247 0.0072 1.0000 20.000 1.2314 0.12904 0.12458 -0.0325 0.0071 1.0000 20.500 1.2012 0.14290 0.13875 -0.0410 0.0073 1.0000 21.000 1.1613 0.15941 0.15558 -0.0516 0.0074 1.0000 21.500 1.1326 0.17388 0.17033 -0.0613 0.0078 1.0000 22.000 1.0963 0.19066 0.18734 -0.0726 0.0078 1.0000 22.500 1.0758 0.20438 0.20123 -0.0821 0.0077 1.0000 23.000 1.0596 0.21757 0.21455 -0.0912 0.0074 1.0000 23.500 1.0538 0.22842 0.22553 -0.0988 0.0075 1.0000 24.000 1.0503 0.23897 0.23611 -0.1063 0.0069 1.0000 24.500 1.0561 0.24671 0.24389 -0.1122 0.0068 1.0000 25.000 1.0637 0.25394 0.25112 -0.1180 0.0063 1.0000 25.500 1.0737 0.26018 0.25741 -0.1233 0.0062 1.0000 26.000 1.0818 0.26721 0.26451 -0.1291 0.0061 1.0000 26.500 1.0599 0.29186 0.28916 -0.1407 0.0076 1.0000 27.000 1.0694 0.30327 0.30054 -0.1464 0.0124 1.0000 27.500 0.8017 0.33192 0.33029 -0.1361 0.0171 1.0000 28.000 0.8063 0.34090 0.33929 -0.1404 0.0170 1.0000 28.500 0.8098 0.35000 0.34840 -0.1449 0.0168 1.0000 29.000 0.8145 0.35948 0.35790 -0.1492 0.0158 1.0000 29.500 0.8204 0.36823 0.36666 -0.1529 0.0144 1.0000 30.000 0.8263 0.37608 0.37454 -0.1565 0.0135 1.0000 30.500 0.8321 0.38372 0.38220 -0.1600 0.0128 1.0000 31.000 0.8379 0.39073 0.38924 -0.1632 0.0123 1.0000 31.500 0.8435 0.39811 0.39663 -0.1662 0.0121 1.0000 32.000 0.8488 0.40785 0.40639 -0.1689 0.0119 1.0000 32.500 0.8510 0.41622 0.41478 -0.1726 0.0118 1.0000 33.000 0.8531 0.42452 0.42309 -0.1761 0.0118 1.0000 33.500 0.8551 0.43274 0.43133 -0.1797 0.0116 1.0000 34.000 0.8574 0.44175 0.44036 -0.1831 0.0110 1.0000 34.500 0.8598 0.44956 0.44820 -0.1862 0.0106 1.0000 35.000 0.8618 0.45729 0.45595 -0.1893 0.0102 1.0000 35.500 0.8636 0.46488 0.46356 -0.1923 0.0096 1.0000 36.000 0.8649 0.47204 0.47075 -0.1952 0.0093 1.0000 36.500 0.8660 0.47920 0.47794 -0.1981 0.0089 1.0000 37.000 0.8667 0.48590 0.48466 -0.2009 0.0086 1.0000 37.500 0.8671 0.49237 0.49116 -0.2037 0.0084 1.0000 38.000 0.8672 0.49876 0.49757 -0.2064 0.0082 1.0000 39.500 0.8652 0.52069 0.51957 -0.2141 0.0080 1.0000 40.000 0.8633 0.52805 0.52695 -0.2171 0.0079 1.0000 40.500 0.8621 0.53591 0.53484 -0.2197 0.0075 1.0000 41.000 0.8605 0.54281 0.54176 -0.2222 0.0070 1.0000 41.500 0.8585 0.54901 0.54799 -0.2246 0.0064 1.0000 42.000 0.8562 0.55473 0.55373 -0.2270 0.0058 1.0000 42.500 0.8533 0.55965 0.55868 -0.2294 0.0056 1.0000 43.000 0.8503 0.56452 0.56358 -0.2316 0.0054 1.0000 43.500 0.8469 0.57342 0.57248 -0.2339 0.0053 1.0000 44.000 0.8440 0.58053 0.57962 -0.2361 0.0050 1.0000 44.500 0.8405 0.58650 0.58562 -0.2382 0.0044 1.0000 45.000 0.8365 0.59138 0.59051 -0.2403 0.0042 1.0000 45.500 0.8320 0.59509 0.59425 -0.2425 0.0038 1.0000 46.000 0.8271 0.59854 0.59772 -0.2445 0.0036 1.0000 46.500 0.8228 0.60626 0.60545 -0.2464 0.0035 1.0000 47.000 0.8183 0.61186 0.61107 -0.2482 0.0033 1.0000 47.500 0.8133 0.61648 0.61572 -0.2501 0.0029 1.0000 48.000 0.8078 0.61995 0.61921 -0.2520 0.0027 1.0000 48.500 0.8018 0.62234 0.62161 -0.2539 0.0025 1.0000 49.500 0.7902 0.63132 0.63063 -0.2571 0.0023 1.0000 50.000 0.7840 0.63451 0.63385 -0.2588 0.0021 1.0000 50.500 0.7776 0.63741 0.63677 -0.2604 0.0019 1.0000 51.000 0.7708 0.63905 0.63842 -0.2620 0.0018 1.0000 51.500 0.7635 0.63999 0.63938 -0.2636 0.0017 1.0000 52.500 0.7494 0.64495 0.64436 -0.2663 0.0016 1.0000 53.000 0.7421 0.64646 0.64589 -0.2677 0.0015 1.0000 53.500 0.7345 0.64770 0.64715 -0.2690 0.0013 1.0000 54.000 0.7266 0.64771 0.64718 -0.2702 0.0012 1.0000 54.500 0.7184 0.64714 0.64663 -0.2715 0.0011 1.0000 55.000 0.7100 0.64639 0.64589 -0.2728 0.0011 1.0000 56.000 0.6934 0.64654 0.64607 -0.2749 0.0010 1.0000 56.500 0.6850 0.64612 0.64567 -0.2759 0.0009 1.0000 57.000 0.6763 0.64513 0.64470 -0.2768 0.0008 1.0000 57.500 0.6673 0.64308 0.64266 -0.2778 0.0007 1.0000 58.000 0.6581 0.64036 0.63995 -0.2788 0.0007 1.0000 59.000 0.6398 0.63639 0.63601 -0.2803 0.0006 1.0000 59.500 0.6304 0.63333 0.63296 -0.2811 0.0006 1.0000 60.000 0.6209 0.63038 0.63003 -0.2817 0.0006 1.0000