XFOIL Version 6.94 Calculated polar for: GOE 630 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 0.7580 0.01364 0.00564 -0.1433 0.6000 0.0671 0.500 0.8057 0.01322 0.00512 -0.1414 0.5804 0.0729 1.000 0.8518 0.01299 0.00484 -0.1394 0.5597 0.0819 1.500 0.8969 0.01294 0.00471 -0.1372 0.5387 0.0961 2.000 0.9406 0.01281 0.00476 -0.1348 0.5190 0.1660 3.000 1.0643 0.01223 0.00548 -0.1384 0.4829 1.0000 3.500 1.1082 0.01277 0.00581 -0.1363 0.4681 1.0000 4.000 1.1509 0.01328 0.00619 -0.1339 0.4541 1.0000 4.500 1.1944 0.01383 0.00666 -0.1318 0.4423 1.0000 5.000 1.2368 0.01441 0.00713 -0.1295 0.4313 1.0000 5.500 1.2672 0.01489 0.00756 -0.1249 0.4147 1.0000 6.000 1.2895 0.01545 0.00801 -0.1189 0.3945 1.0000 6.500 1.3093 0.01619 0.00861 -0.1128 0.3697 1.0000 7.000 1.3403 0.01700 0.00938 -0.1092 0.3573 1.0000 7.500 1.3644 0.01805 0.01035 -0.1047 0.3369 1.0000 8.000 1.3922 0.01916 0.01142 -0.1011 0.3219 1.0000 8.500 1.4154 0.02060 0.01281 -0.0972 0.3015 1.0000 9.000 1.4399 0.02215 0.01435 -0.0939 0.2831 1.0000 10.000 1.4607 0.02758 0.01949 -0.0858 0.2121 1.0000 10.500 1.4049 0.03604 0.02731 -0.0781 0.1045 1.0000 11.000 1.3655 0.04439 0.03540 -0.0736 0.0355 1.0000 11.500 1.3487 0.05138 0.04240 -0.0713 0.0044 1.0000 12.000 1.3542 0.05635 0.04754 -0.0701 0.0038 1.0000 12.500 1.3577 0.06176 0.05314 -0.0692 0.0037 1.0000 13.000 1.3581 0.06771 0.05930 -0.0686 0.0035 1.0000 13.500 1.3554 0.07428 0.06608 -0.0683 0.0035 1.0000 14.000 1.3500 0.08136 0.07339 -0.0684 0.0035 1.0000 14.500 1.3437 0.08872 0.08096 -0.0687 0.0035 1.0000 15.000 1.3361 0.09640 0.08886 -0.0694 0.0035 1.0000 15.500 1.3290 0.10414 0.09681 -0.0703 0.0035 1.0000 16.000 1.3221 0.11197 0.10485 -0.0715 0.0035 1.0000 16.500 1.3166 0.11967 0.11274 -0.0731 0.0036 1.0000 17.000 1.3124 0.12731 0.12057 -0.0749 0.0036 1.0000 17.500 1.3096 0.13477 0.12821 -0.0769 0.0036 1.0000 18.000 1.3080 0.14206 0.13568 -0.0792 0.0037 1.0000 18.500 1.3056 0.14960 0.14339 -0.0819 0.0038 1.0000 19.000 1.3044 0.15695 0.15090 -0.0847 0.0039 1.0000 19.500 1.3046 0.16406 0.15815 -0.0877 0.0040 1.0000 20.000 1.3056 0.17095 0.16516 -0.0908 0.0041 1.0000 20.500 1.3106 0.17694 0.17125 -0.0936 0.0042 1.0000 21.000 1.3188 0.18213 0.17650 -0.0961 0.0043 1.0000 21.500 1.3319 0.18606 0.18046 -0.0980 0.0044 1.0000 22.000 1.3548 0.18725 0.18160 -0.0981 0.0046 1.0000 22.500 1.3709 0.19061 0.18506 -0.0998 0.0048 1.0000 23.000 1.3826 0.19522 0.18991 -0.1024 0.0051 1.0000 23.500 1.4000 0.19789 0.19279 -0.1036 0.0056 1.0000 24.000 1.4387 0.19427 0.18917 -0.1004 0.0062 1.0000 24.500 1.4297 0.20402 0.19931 -0.1070 0.0064 1.0000 25.000 1.4162 0.21436 0.21021 -0.1136 0.0072 1.0000 25.500 1.4314 0.21634 0.21231 -0.1146 0.0079 1.0000 26.000 1.3844 0.23754 0.23421 -0.1293 0.0085 1.0000 26.500 1.3432 0.25902 0.25614 -0.1441 0.0087 1.0000 27.000 0.9860 0.36806 0.36620 -0.1743 0.0190 1.0000 27.500 0.9912 0.37623 0.37440 -0.1769 0.0181 1.0000 28.000 0.9915 0.38922 0.38740 -0.1808 0.0171 1.0000 28.500 0.9941 0.39971 0.39792 -0.1840 0.0155 1.0000 29.500 0.9981 0.42156 0.41983 -0.1904 0.0136 1.0000 30.000 1.0006 0.43093 0.42922 -0.1933 0.0127 1.0000 30.500 1.0055 0.43769 0.43603 -0.1953 0.0122 1.0000 31.000 1.0033 0.45289 0.45123 -0.1994 0.0114 1.0000 31.500 1.0047 0.46290 0.46128 -0.2023 0.0106 1.0000 32.000 1.0063 0.47145 0.46987 -0.2049 0.0101 1.0000 32.500 1.0081 0.48013 0.47858 -0.2073 0.0098 1.0000 33.000 1.0067 0.49362 0.49210 -0.2108 0.0095 1.0000 33.500 1.0068 0.50407 0.50258 -0.2136 0.0088 1.0000 34.000 1.0068 0.51370 0.51224 -0.2162 0.0084 1.0000 34.500 1.0064 0.52270 0.52128 -0.2188 0.0082 1.0000 35.000 1.0060 0.53083 0.52945 -0.2213 0.0080 1.0000 35.500 1.0051 0.54055 0.53920 -0.2237 0.0078 1.0000 36.000 1.0030 0.55171 0.55039 -0.2265 0.0078 1.0000 36.500 1.0013 0.56156 0.56027 -0.2291 0.0077 1.0000 37.000 0.9994 0.57122 0.56997 -0.2316 0.0075 1.0000 37.500 0.9972 0.58056 0.57935 -0.2341 0.0073 1.0000 38.000 0.9946 0.58933 0.58816 -0.2365 0.0071 1.0000 38.500 0.9918 0.59805 0.59692 -0.2388 0.0069 1.0000 39.000 0.9886 0.60642 0.60532 -0.2411 0.0067 1.0000 39.500 0.9852 0.61453 0.61348 -0.2434 0.0066 1.0000 40.000 0.9813 0.62209 0.62107 -0.2456 0.0064 1.0000 40.500 0.9772 0.62887 0.62789 -0.2477 0.0062 1.0000 41.500 0.9683 0.64631 0.64540 -0.2519 0.0061 1.0000 42.000 0.9640 0.65559 0.65470 -0.2540 0.0056 1.0000 42.500 0.9589 0.66303 0.66218 -0.2559 0.0052 1.0000 43.000 0.9536 0.66980 0.66899 -0.2579 0.0049 1.0000 43.500 0.9475 0.67490 0.67413 -0.2597 0.0047 1.0000 44.000 0.9418 0.68361 0.68286 -0.2616 0.0046 1.0000 44.500 0.9366 0.69300 0.69228 -0.2633 0.0043 1.0000 45.000 0.9304 0.69958 0.69888 -0.2650 0.0039 1.0000 45.500 0.9237 0.70505 0.70438 -0.2667 0.0036 1.0000 46.000 0.9164 0.70929 0.70867 -0.2684 0.0034 1.0000 46.500 0.9093 0.71574 0.71513 -0.2699 0.0034 1.0000 47.000 0.9031 0.72399 0.72341 -0.2713 0.0032 1.0000 47.500 0.8959 0.72954 0.72898 -0.2728 0.0029 1.0000 48.000 0.8883 0.73420 0.73368 -0.2742 0.0026 1.0000 48.500 0.8802 0.73766 0.73717 -0.2757 0.0025 1.0000 49.000 0.8712 0.73956 0.73910 -0.2771 0.0023 1.0000 49.500 0.8634 0.74568 0.74523 -0.2783 0.0023 1.0000 50.000 0.8557 0.75086 0.75044 -0.2794 0.0022 1.0000 50.500 0.8475 0.75462 0.75422 -0.2805 0.0020 1.0000 51.000 0.8387 0.75733 0.75695 -0.2816 0.0018 1.0000 51.500 0.8295 0.75912 0.75877 -0.2827 0.0016 1.0000 52.000 0.8200 0.76011 0.75979 -0.2838 0.0015 1.0000 52.500 0.8098 0.75978 0.75949 -0.2849 0.0014 1.0000 53.500 0.7906 0.76288 0.76262 -0.2867 0.0014 1.0000 54.000 0.7813 0.76452 0.76427 -0.2874 0.0013 1.0000 54.500 0.7716 0.76495 0.76473 -0.2881 0.0013 1.0000 55.000 0.7617 0.76467 0.76447 -0.2887 0.0012 1.0000 55.500 0.7516 0.76400 0.76382 -0.2894 0.0011 1.0000 56.000 0.7410 0.76217 0.76202 -0.2900 0.0010 1.0000 56.500 0.7304 0.76026 0.76012 -0.2906 0.0009 1.0000 57.000 0.7195 0.75749 0.75737 -0.2911 0.0008 1.0000 57.500 0.7083 0.75390 0.75380 -0.2916 0.0007 1.0000 58.000 0.6968 0.74945 0.74937 -0.2921 0.0007 1.0000 58.500 0.6847 0.74417 0.74411 -0.2927 0.0006 1.0000 59.500 0.6634 0.73864 0.73861 -0.2930 0.0006 1.0000 60.000 0.6524 0.73430 0.73429 -0.2931 0.0005 1.0000