XFOIL Version 6.94 Calculated polar for: GOE 615 AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.080 Re = 0.450 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------- -------- --------- --------- -------- ------- ------- 0.000 0.5797 0.01033 0.00300 -0.1060 0.5725 0.1584 0.500 0.6241 0.00968 0.00320 -0.1040 0.5606 0.4512 1.000 0.7560 0.00877 0.00357 -0.1200 0.5475 1.0000 1.500 0.8014 0.00907 0.00367 -0.1177 0.5354 1.0000 2.000 0.8477 0.00924 0.00380 -0.1156 0.5254 1.0000 2.500 0.8921 0.00955 0.00394 -0.1131 0.5111 1.0000 3.000 0.9365 0.00972 0.00408 -0.1106 0.4964 1.0000 3.500 0.9792 0.00999 0.00427 -0.1078 0.4795 1.0000 4.000 1.0203 0.01029 0.00446 -0.1047 0.4608 1.0000 4.500 1.0382 0.01095 0.00467 -0.0972 0.3766 1.0000 5.000 1.0539 0.01194 0.00528 -0.0896 0.3212 1.0000 5.500 1.0711 0.01304 0.00603 -0.0826 0.2722 1.0000 6.000 1.0992 0.01389 0.00669 -0.0778 0.2403 1.0000 6.500 1.1181 0.01521 0.00767 -0.0719 0.1917 1.0000 7.000 1.1396 0.01655 0.00877 -0.0668 0.1538 1.0000 7.500 1.1217 0.02016 0.01173 -0.0573 0.0505 1.0000 8.000 1.1481 0.02166 0.01321 -0.0540 0.0402 1.0000 8.500 1.1625 0.02407 0.01552 -0.0498 0.0036 1.0000 9.000 1.1900 0.02576 0.01728 -0.0473 0.0033 1.0000 9.500 1.2157 0.02769 0.01929 -0.0449 0.0033 1.0000 10.000 1.2390 0.02989 0.02159 -0.0426 0.0033 1.0000 10.500 1.2596 0.03243 0.02426 -0.0404 0.0033 1.0000 11.000 1.2770 0.03537 0.02734 -0.0384 0.0034 1.0000 11.500 1.2907 0.03883 0.03096 -0.0366 0.0035 1.0000 12.000 1.3009 0.04279 0.03510 -0.0350 0.0035 1.0000 12.500 1.3063 0.04751 0.04002 -0.0338 0.0036 1.0000 13.000 1.3104 0.05259 0.04529 -0.0331 0.0037 1.0000 13.500 1.3147 0.05787 0.05074 -0.0327 0.0038 1.0000 14.000 1.3158 0.06370 0.05676 -0.0326 0.0039 1.0000 14.500 1.3134 0.07012 0.06338 -0.0328 0.0041 1.0000 15.000 1.3063 0.07733 0.07080 -0.0335 0.0043 1.0000 15.500 1.2946 0.08537 0.07908 -0.0345 0.0045 1.0000 16.000 1.2781 0.09441 0.08834 -0.0363 0.0046 1.0000 16.500 1.2586 0.10423 0.09838 -0.0386 0.0047 1.0000 17.000 1.2363 0.11488 0.10924 -0.0418 0.0048 1.0000 17.500 1.2107 0.12633 0.12089 -0.0457 0.0048 1.0000 18.000 1.2090 0.13395 0.12865 -0.0484 0.0050 1.0000 18.500 1.2046 0.14208 0.13694 -0.0516 0.0052 1.0000 19.000 1.1991 0.15049 0.14550 -0.0552 0.0057 1.0000 19.500 1.1933 0.15903 0.15414 -0.0592 0.0058 1.0000 20.000 1.1926 0.16624 0.16136 -0.0627 0.0062 1.0000 20.500 1.2003 0.17246 0.16771 -0.0659 0.0065 1.0000 21.000 1.2103 0.17789 0.17325 -0.0688 0.0071 1.0000 21.500 1.2295 0.18093 0.17625 -0.0702 0.0080 1.0000 22.000 1.2480 0.18442 0.17983 -0.0721 0.0091 1.0000 22.500 1.2682 0.18776 0.18330 -0.0739 0.0106 1.0000 23.000 1.2937 0.18950 0.18507 -0.0748 0.0119 1.0000 23.500 1.3214 0.19107 0.18676 -0.0755 0.0140 1.0000 24.000 1.3626 0.18887 0.18459 -0.0735 0.0159 1.0000 24.500 1.3650 0.19610 0.19211 -0.0783 0.0166 1.0000 25.000 1.3767 0.20052 0.19676 -0.0812 0.0172 1.0000 25.500 1.3858 0.20518 0.20164 -0.0843 0.0177 1.0000 26.000 1.3837 0.21245 0.20915 -0.0895 0.0178 1.0000 26.500 1.3756 0.22113 0.21808 -0.0959 0.0181 1.0000 27.000 1.3622 0.23141 0.22862 -0.1036 0.0184 1.0000 27.500 0.9195 0.35542 0.35383 -0.1577 0.0165 1.0000 28.000 0.9234 0.36499 0.36342 -0.1612 0.0143 1.0000 28.500 0.9270 0.37480 0.37324 -0.1646 0.0123 1.0000 29.500 0.9341 0.39369 0.39218 -0.1712 0.0100 1.0000 30.000 0.9403 0.39896 0.39749 -0.1738 0.0096 1.0000 30.500 0.9397 0.41400 0.41253 -0.1778 0.0085 1.0000 31.000 0.9440 0.42070 0.41926 -0.1806 0.0079 1.0000 31.500 0.9479 0.42773 0.42632 -0.1833 0.0078 1.0000 32.000 0.9466 0.44397 0.44256 -0.1872 0.0071 1.0000 32.500 0.9486 0.45323 0.45186 -0.1902 0.0067 1.0000 33.000 0.9510 0.46042 0.45907 -0.1930 0.0064 1.0000 33.500 0.9534 0.46729 0.46598 -0.1957 0.0063 1.0000 34.000 0.9539 0.47792 0.47662 -0.1987 0.0062 1.0000 34.500 0.9531 0.49084 0.48956 -0.2019 0.0061 1.0000 35.000 0.9533 0.50175 0.50049 -0.2049 0.0058 1.0000 35.500 0.9533 0.51079 0.50956 -0.2077 0.0058 1.0000 36.000 0.9531 0.52012 0.51892 -0.2105 0.0056 1.0000 36.500 0.9526 0.52911 0.52794 -0.2132 0.0055 1.0000 37.000 0.9518 0.53773 0.53659 -0.2158 0.0053 1.0000 37.500 0.9507 0.54626 0.54514 -0.2185 0.0053 1.0000 38.000 0.9492 0.55462 0.55353 -0.2211 0.0052 1.0000 38.500 0.9474 0.56264 0.56158 -0.2237 0.0052 1.0000 39.000 0.9454 0.57046 0.56943 -0.2263 0.0051 1.0000 39.500 0.9429 0.57802 0.57702 -0.2288 0.0051 1.0000 40.000 0.9402 0.58531 0.58434 -0.2312 0.0050 1.0000 40.500 0.9372 0.59156 0.59063 -0.2336 0.0049 1.0000 41.500 0.9303 0.60582 0.60494 -0.2382 0.0049 1.0000 42.000 0.9263 0.61670 0.61584 -0.2406 0.0048 1.0000 42.500 0.9225 0.62524 0.62441 -0.2428 0.0045 1.0000 43.000 0.9183 0.63260 0.63179 -0.2449 0.0041 1.0000 43.500 0.9136 0.63864 0.63786 -0.2471 0.0039 1.0000 44.000 0.9084 0.64331 0.64256 -0.2492 0.0037 1.0000 44.500 0.9030 0.64682 0.64611 -0.2512 0.0036 1.0000 45.000 0.8978 0.65824 0.65753 -0.2531 0.0036 1.0000 45.500 0.8929 0.66672 0.66604 -0.2549 0.0032 1.0000 46.000 0.8870 0.67223 0.67157 -0.2568 0.0029 1.0000 46.500 0.8806 0.67656 0.67593 -0.2587 0.0027 1.0000 47.000 0.8738 0.67966 0.67906 -0.2606 0.0026 1.0000 48.000 0.8605 0.69210 0.69153 -0.2638 0.0025 1.0000 48.500 0.8543 0.69883 0.69829 -0.2653 0.0023 1.0000 49.000 0.8471 0.70308 0.70256 -0.2668 0.0020 1.0000 49.500 0.8395 0.70612 0.70562 -0.2684 0.0018 1.0000 50.000 0.8315 0.70829 0.70781 -0.2699 0.0017 1.0000 50.500 0.8228 0.70889 0.70844 -0.2715 0.0016 1.0000 51.500 0.8065 0.71576 0.71534 -0.2741 0.0016 1.0000 52.000 0.7989 0.72086 0.72046 -0.2751 0.0015 1.0000 52.500 0.7907 0.72363 0.72325 -0.2763 0.0015 1.0000 53.000 0.7821 0.72541 0.72504 -0.2773 0.0013 1.0000 53.500 0.7731 0.72636 0.72601 -0.2784 0.0012 1.0000 54.000 0.7638 0.72657 0.72624 -0.2795 0.0010 1.0000 54.500 0.7542 0.72596 0.72565 -0.2805 0.0009 1.0000 55.000 0.7444 0.72440 0.72411 -0.2816 0.0008 1.0000 55.500 0.7340 0.72187 0.72160 -0.2826 0.0008 1.0000 56.500 0.7146 0.72162 0.72137 -0.2841 0.0007 1.0000 57.000 0.7052 0.72140 0.72117 -0.2847 0.0006 1.0000 57.500 0.6950 0.71910 0.71888 -0.2853 0.0005 1.0000 58.000 0.6846 0.71608 0.71588 -0.2860 0.0005 1.0000 58.500 0.6737 0.71193 0.71175 -0.2866 0.0004 1.0000 60.000 0.6418 0.70148 0.70133 -0.2878 0.0003 1.0000