XFOIL Version 6.94 Calculated polar for: GOE 528 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 0.6361 0.01054 0.00284 -0.1164 0.5618 0.0598 0.500 0.6866 0.01026 0.00289 -0.1154 0.5481 0.1852 1.000 0.7734 0.00870 0.00330 -0.1226 0.5351 1.0000 1.500 0.8218 0.00898 0.00340 -0.1209 0.5226 1.0000 2.000 0.8711 0.00924 0.00356 -0.1195 0.5115 1.0000 2.500 0.9196 0.00953 0.00371 -0.1179 0.4996 1.0000 3.000 0.9684 0.00982 0.00393 -0.1165 0.4883 1.0000 3.500 1.0163 0.01011 0.00412 -0.1149 0.4760 1.0000 4.000 1.0642 0.01040 0.00440 -0.1133 0.4641 1.0000 4.500 1.1110 0.01072 0.00465 -0.1116 0.4521 1.0000 5.000 1.1486 0.01099 0.00477 -0.1080 0.4160 1.0000 5.500 1.1865 0.01148 0.00508 -0.1047 0.3861 1.0000 6.000 1.2182 0.01216 0.00555 -0.1004 0.3455 1.0000 6.500 1.2466 0.01287 0.00610 -0.0955 0.3163 1.0000 7.000 1.2583 0.01427 0.00710 -0.0880 0.2531 1.0000 7.500 1.2776 0.01558 0.00818 -0.0823 0.2129 1.0000 8.000 1.2934 0.01717 0.00955 -0.0766 0.1748 1.0000 8.500 1.2670 0.02123 0.01300 -0.0665 0.0726 1.0000 9.000 1.2507 0.02554 0.01701 -0.0595 0.0041 1.0000 9.500 1.2718 0.02773 0.01929 -0.0567 0.0022 1.0000 10.000 1.2922 0.03011 0.02178 -0.0543 0.0020 1.0000 10.500 1.3103 0.03283 0.02462 -0.0520 0.0020 1.0000 11.000 1.3253 0.03597 0.02790 -0.0500 0.0020 1.0000 11.500 1.3375 0.03958 0.03167 -0.0482 0.0021 1.0000 12.000 1.3469 0.04365 0.03590 -0.0468 0.0021 1.0000 12.500 1.3540 0.04821 0.04064 -0.0456 0.0022 1.0000 13.000 1.3572 0.05343 0.04605 -0.0449 0.0023 1.0000 13.500 1.3575 0.05923 0.05205 -0.0445 0.0024 1.0000 14.000 1.3559 0.06545 0.05847 -0.0445 0.0024 1.0000 14.500 1.3504 0.07239 0.06563 -0.0448 0.0025 1.0000 15.000 1.3429 0.07982 0.07328 -0.0456 0.0026 1.0000 15.500 1.3332 0.08781 0.08148 -0.0468 0.0026 1.0000 16.000 1.3234 0.09612 0.09000 -0.0485 0.0027 1.0000 16.500 1.3174 0.10408 0.09815 -0.0504 0.0028 1.0000 17.000 1.3116 0.11226 0.10650 -0.0527 0.0029 1.0000 17.500 1.3071 0.12037 0.11481 -0.0554 0.0030 1.0000 18.000 1.2992 0.12924 0.12386 -0.0586 0.0032 1.0000 18.500 1.2908 0.13832 0.13311 -0.0624 0.0034 1.0000 19.000 1.2824 0.14744 0.14238 -0.0664 0.0036 1.0000 19.500 1.2764 0.15608 0.15113 -0.0705 0.0037 1.0000 20.000 1.2781 0.16310 0.15821 -0.0739 0.0038 1.0000 20.500 1.2853 0.16944 0.16471 -0.0773 0.0040 1.0000 21.000 1.2961 0.17469 0.17008 -0.0799 0.0046 1.0000 21.500 1.3164 0.17695 0.17227 -0.0807 0.0051 1.0000 22.000 1.3251 0.18312 0.17869 -0.0843 0.0057 1.0000 22.500 1.3569 0.18274 0.17829 -0.0834 0.0067 1.0000 23.000 1.3884 0.18277 0.17852 -0.0824 0.0084 1.0000 24.000 1.3849 0.19811 0.19492 -0.0903 0.0132 1.0000 24.500 1.3369 0.21744 0.21474 -0.1035 0.0135 1.0000 25.000 1.3055 0.23352 0.23108 -0.1145 0.0133 1.0000 25.500 1.2718 0.25158 0.24933 -0.1265 0.0129 1.0000 26.000 0.9580 0.35078 0.34925 -0.1645 0.0157 1.0000 26.500 0.9590 0.36421 0.36268 -0.1687 0.0137 1.0000 27.000 0.9665 0.37072 0.36921 -0.1712 0.0129 1.0000 27.500 0.9672 0.38439 0.38289 -0.1754 0.0109 1.0000 28.000 0.9706 0.39499 0.39351 -0.1787 0.0100 1.0000 28.500 0.9744 0.40484 0.40339 -0.1819 0.0087 1.0000 29.000 0.9815 0.41039 0.40897 -0.1839 0.0083 1.0000 29.500 0.9803 0.42612 0.42470 -0.1883 0.0069 1.0000 30.000 0.9846 0.43333 0.43195 -0.1909 0.0066 1.0000 30.500 0.9850 0.44845 0.44708 -0.1946 0.0059 1.0000 31.000 0.9876 0.45776 0.45641 -0.1975 0.0053 1.0000 31.500 0.9904 0.46509 0.46377 -0.2001 0.0051 1.0000 32.000 0.9908 0.47849 0.47719 -0.2034 0.0049 1.0000 32.500 0.9921 0.49072 0.48944 -0.2065 0.0045 1.0000 33.000 0.9932 0.50080 0.49955 -0.2093 0.0041 1.0000 33.500 0.9939 0.51044 0.50921 -0.2122 0.0040 1.0000 34.000 0.9944 0.51859 0.51739 -0.2148 0.0038 1.0000 34.500 0.9946 0.52812 0.52694 -0.2174 0.0037 1.0000 35.000 0.9940 0.53928 0.53813 -0.2203 0.0037 1.0000 35.500 0.9934 0.54998 0.54885 -0.2231 0.0037 1.0000 36.000 0.9928 0.56157 0.56047 -0.2258 0.0036 1.0000 36.500 0.9916 0.57135 0.57027 -0.2284 0.0035 1.0000 37.000 0.9902 0.58107 0.58002 -0.2309 0.0035 1.0000 37.500 0.9884 0.59033 0.58931 -0.2335 0.0034 1.0000 38.000 0.9863 0.59964 0.59865 -0.2359 0.0034 1.0000 38.500 0.9840 0.60860 0.60764 -0.2384 0.0033 1.0000 39.000 0.9813 0.61753 0.61660 -0.2408 0.0032 1.0000 39.500 0.9782 0.62603 0.62513 -0.2432 0.0032 1.0000 40.000 0.9749 0.63453 0.63365 -0.2455 0.0031 1.0000 40.500 0.9712 0.64259 0.64175 -0.2478 0.0031 1.0000 41.000 0.9673 0.65055 0.64973 -0.2501 0.0031 1.0000 41.500 0.9631 0.65827 0.65749 -0.2523 0.0030 1.0000 42.000 0.9584 0.66534 0.66459 -0.2545 0.0029 1.0000 42.500 0.9534 0.67183 0.67111 -0.2566 0.0028 1.0000 43.000 0.9480 0.67772 0.67703 -0.2587 0.0027 1.0000 44.000 0.9369 0.69276 0.69212 -0.2627 0.0026 1.0000 44.500 0.9324 0.70311 0.70249 -0.2644 0.0025 1.0000 45.000 0.9266 0.71016 0.70956 -0.2662 0.0022 1.0000 45.500 0.9202 0.71596 0.71538 -0.2681 0.0020 1.0000 46.000 0.9133 0.72084 0.72030 -0.2698 0.0019 1.0000 46.500 0.9059 0.72474 0.72422 -0.2717 0.0018 1.0000 47.500 0.8917 0.73728 0.73680 -0.2749 0.0017 1.0000 48.000 0.8856 0.74516 0.74469 -0.2762 0.0016 1.0000 48.500 0.8782 0.75011 0.74967 -0.2777 0.0015 1.0000 49.000 0.8703 0.75425 0.75383 -0.2791 0.0013 1.0000 49.500 0.8619 0.75725 0.75685 -0.2805 0.0012 1.0000 50.000 0.8533 0.75974 0.75936 -0.2819 0.0011 1.0000 50.500 0.8441 0.76096 0.76061 -0.2834 0.0011 1.0000 51.500 0.8265 0.76806 0.76774 -0.2858 0.0010 1.0000 52.000 0.8181 0.77173 0.77142 -0.2868 0.0010 1.0000 52.500 0.8094 0.77434 0.77405 -0.2878 0.0010 1.0000 53.000 0.8005 0.77655 0.77628 -0.2887 0.0009 1.0000 53.500 0.7909 0.77718 0.77693 -0.2897 0.0008 1.0000 54.000 0.7813 0.77784 0.77760 -0.2906 0.0007 1.0000 54.500 0.7712 0.77735 0.77713 -0.2915 0.0006 1.0000 55.000 0.7610 0.77630 0.77610 -0.2924 0.0006 1.0000 55.500 0.7503 0.77429 0.77411 -0.2933 0.0005 1.0000 56.000 0.7394 0.77162 0.77146 -0.2941 0.0005 1.0000 56.500 0.7280 0.76802 0.76787 -0.2950 0.0005 1.0000 57.500 0.7075 0.76643 0.76631 -0.2959 0.0004 1.0000 58.000 0.6974 0.76470 0.76458 -0.2963 0.0004 1.0000 58.500 0.6865 0.76149 0.76139 -0.2967 0.0004 1.0000 59.000 0.6754 0.75736 0.75728 -0.2971 0.0003 1.0000 59.500 0.6640 0.75246 0.75240 -0.2975 0.0003 1.0000 60.000 0.6524 0.74700 0.74694 -0.2979 0.0003 1.0000