XFOIL Version 6.96 Calculated polar for: RAE 102 AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -16.500 -0.9447 0.11912 0.11722 0.0069 1.0000 0.0043 -16.250 -0.9911 0.10440 0.10237 -0.0005 1.0000 0.0041 -16.000 -1.0566 0.08557 0.08333 -0.0106 1.0000 0.0041 -15.750 -1.0905 0.07392 0.07151 -0.0177 1.0000 0.0040 -15.500 -1.1141 0.06530 0.06274 -0.0232 1.0000 0.0040 -15.250 -1.1354 0.05791 0.05519 -0.0278 1.0000 0.0040 -15.000 -1.1564 0.05122 0.04832 -0.0316 1.0000 0.0040 -14.750 -1.1732 0.04574 0.04266 -0.0342 1.0000 0.0040 -14.500 -1.1795 0.04204 0.03883 -0.0355 1.0000 0.0040 -14.250 -1.1836 0.03891 0.03556 -0.0362 1.0000 0.0041 -14.000 -1.1907 0.03579 0.03228 -0.0363 1.0000 0.0041 -13.750 -1.1917 0.03352 0.02988 -0.0357 1.0000 0.0041 -13.500 -1.2014 0.03078 0.02695 -0.0341 1.0000 0.0042 -13.250 -1.2051 0.02879 0.02480 -0.0319 1.0000 0.0042 -13.000 -1.2075 0.02707 0.02293 -0.0291 1.0000 0.0043 -12.750 -1.2071 0.02568 0.02141 -0.0260 1.0000 0.0044 -12.500 -1.2013 0.02467 0.02030 -0.0233 1.0000 0.0045 -12.250 -1.1913 0.02363 0.01916 -0.0211 1.0000 0.0046 -12.000 -1.1776 0.02276 0.01819 -0.0195 1.0000 0.0047 -11.750 -1.1637 0.02182 0.01714 -0.0179 1.0000 0.0048 -11.500 -1.1476 0.02104 0.01627 -0.0165 1.0000 0.0049 -11.250 -1.1302 0.02032 0.01548 -0.0152 1.0000 0.0050 -11.000 -1.1128 0.01956 0.01463 -0.0139 1.0000 0.0052 -10.750 -1.0941 0.01889 0.01389 -0.0127 1.0000 0.0053 -10.500 -1.0754 0.01821 0.01312 -0.0115 1.0000 0.0055 -10.250 -1.0556 0.01762 0.01246 -0.0104 1.0000 0.0058 -10.000 -1.0357 0.01703 0.01178 -0.0093 1.0000 0.0059 -9.750 -1.0151 0.01650 0.01119 -0.0083 1.0000 0.0061 -9.500 -0.9940 0.01603 0.01065 -0.0073 1.0000 0.0063 -9.250 -0.9753 0.01528 0.00982 -0.0059 1.0000 0.0065 -9.000 -0.9558 0.01462 0.00909 -0.0046 1.0000 0.0068 -8.750 -0.9350 0.01413 0.00855 -0.0035 1.0000 0.0071 -8.500 -0.9137 0.01368 0.00808 -0.0024 1.0000 0.0075 -8.250 -0.8921 0.01328 0.00763 -0.0014 1.0000 0.0079 -8.000 -0.8704 0.01289 0.00719 -0.0004 1.0000 0.0082 -7.750 -0.8487 0.01251 0.00677 0.0007 1.0000 0.0086 -7.500 -0.8267 0.01217 0.00639 0.0017 1.0000 0.0090 -7.250 -0.8051 0.01180 0.00599 0.0028 1.0000 0.0094 -7.000 -0.7740 0.01134 0.00549 0.0018 0.9972 0.0104 -6.750 -0.7435 0.01099 0.00514 0.0009 0.9930 0.0113 -6.500 -0.7132 0.01070 0.00482 0.0002 0.9879 0.0124 -6.000 -0.6496 0.01003 0.00413 -0.0020 0.9773 0.0153 -5.750 -0.6154 0.00974 0.00383 -0.0035 0.9708 0.0171 -5.500 -0.5816 0.00947 0.00354 -0.0050 0.9609 0.0195 -5.250 -0.5473 0.00918 0.00326 -0.0066 0.9477 0.0233 -5.000 -0.5155 0.00897 0.00301 -0.0075 0.9293 0.0272 -4.750 -0.4881 0.00877 0.00278 -0.0075 0.9057 0.0324 -4.500 -0.4627 0.00861 0.00257 -0.0070 0.8815 0.0404 -4.250 -0.4377 0.00846 0.00238 -0.0064 0.8580 0.0498 -4.000 -0.4126 0.00831 0.00219 -0.0058 0.8377 0.0622 -3.750 -0.3875 0.00811 0.00201 -0.0053 0.8189 0.0823 -3.500 -0.3625 0.00790 0.00184 -0.0048 0.8008 0.1081 -3.250 -0.3378 0.00764 0.00166 -0.0043 0.7838 0.1459 -3.000 -0.3131 0.00737 0.00149 -0.0038 0.7679 0.1911 -2.750 -0.2888 0.00702 0.00132 -0.0032 0.7533 0.2518 -2.500 -0.2646 0.00664 0.00115 -0.0027 0.7399 0.3222 -2.250 -0.2406 0.00624 0.00101 -0.0021 0.7272 0.4013 -2.000 -0.2151 0.00603 0.00094 -0.0017 0.7152 0.4555 -1.750 -0.1887 0.00592 0.00088 -0.0014 0.7034 0.4878 -1.500 -0.1621 0.00584 0.00084 -0.0012 0.6915 0.5127 -1.000 -0.1082 0.00573 0.00078 -0.0008 0.6694 0.5535 -0.750 -0.0811 0.00569 0.00076 -0.0006 0.6589 0.5716 -0.500 -0.0541 0.00566 0.00075 -0.0004 0.6473 0.5887 -0.250 -0.0270 0.00565 0.00074 -0.0002 0.6345 0.6051 0.000 0.0000 0.00564 0.00073 0.0000 0.6202 0.6203 0.250 0.0270 0.00565 0.00074 0.0002 0.6049 0.6344 0.500 0.0541 0.00566 0.00075 0.0004 0.5887 0.6473 0.750 0.0811 0.00569 0.00076 0.0006 0.5715 0.6590 1.000 0.1082 0.00573 0.00078 0.0008 0.5535 0.6695 1.500 0.1621 0.00584 0.00084 0.0012 0.5123 0.6914 1.750 0.1888 0.00592 0.00088 0.0014 0.4874 0.7033 2.000 0.2152 0.00602 0.00094 0.0017 0.4572 0.7152 2.250 0.2407 0.00623 0.00101 0.0021 0.4049 0.7272 2.500 0.2645 0.00665 0.00116 0.0027 0.3207 0.7399 2.750 0.2888 0.00702 0.00132 0.0032 0.2514 0.7533 3.000 0.3131 0.00737 0.00149 0.0038 0.1900 0.7678 3.250 0.3380 0.00764 0.00166 0.0043 0.1470 0.7836 3.500 0.3626 0.00790 0.00184 0.0048 0.1089 0.8008 3.750 0.3876 0.00811 0.00201 0.0053 0.0822 0.8189 4.000 0.4127 0.00830 0.00219 0.0058 0.0627 0.8377 4.250 0.4377 0.00846 0.00238 0.0064 0.0498 0.8582 4.500 0.4627 0.00862 0.00257 0.0070 0.0398 0.8815 4.750 0.4882 0.00877 0.00278 0.0075 0.0325 0.9061 5.000 0.5157 0.00897 0.00301 0.0075 0.0272 0.9293 5.250 0.5474 0.00918 0.00326 0.0066 0.0234 0.9476 5.500 0.5817 0.00947 0.00354 0.0050 0.0196 0.9610 5.750 0.6157 0.00974 0.00383 0.0035 0.0171 0.9710 6.000 0.6498 0.01003 0.00414 0.0019 0.0153 0.9777 6.250 0.6811 0.01038 0.00448 0.0009 0.0134 0.9837 6.500 0.7138 0.01069 0.00482 -0.0003 0.0124 0.9881 6.750 0.7441 0.01099 0.00514 -0.0011 0.0113 0.9931 7.000 0.7744 0.01134 0.00550 -0.0019 0.0103 0.9975 7.250 0.8047 0.01180 0.00598 -0.0027 0.0094 1.0000 7.500 0.8263 0.01216 0.00638 -0.0016 0.0090 1.0000 7.750 0.8483 0.01251 0.00677 -0.0006 0.0086 1.0000 8.000 0.8701 0.01288 0.00719 0.0004 0.0083 1.0000 8.250 0.8919 0.01328 0.00762 0.0015 0.0079 1.0000 8.500 0.9135 0.01369 0.00809 0.0025 0.0075 1.0000 8.750 0.9350 0.01412 0.00855 0.0035 0.0072 1.0000 9.000 0.9559 0.01462 0.00909 0.0046 0.0069 1.0000 9.250 0.9756 0.01527 0.00980 0.0059 0.0065 1.0000 9.500 0.9952 0.01593 0.01054 0.0071 0.0062 1.0000 9.750 1.0151 0.01656 0.01125 0.0083 0.0061 1.0000 10.000 1.0360 0.01706 0.01181 0.0092 0.0060 1.0000 10.250 1.0563 0.01761 0.01245 0.0103 0.0058 1.0000 10.500 1.0759 0.01823 0.01315 0.0114 0.0056 1.0000 10.750 1.0951 0.01888 0.01387 0.0125 0.0054 1.0000 11.000 1.1134 0.01959 0.01466 0.0137 0.0052 1.0000 11.250 1.1314 0.02029 0.01545 0.0149 0.0051 1.0000 11.500 1.1477 0.02113 0.01638 0.0164 0.0050 1.0000 11.750 1.1646 0.02185 0.01718 0.0177 0.0048 1.0000 12.000 1.1792 0.02273 0.01815 0.0192 0.0047 1.0000 12.250 1.1929 0.02362 0.01915 0.0209 0.0046 1.0000 12.500 1.2035 0.02464 0.02027 0.0229 0.0045 1.0000 12.750 1.2091 0.02569 0.02142 0.0257 0.0044 1.0000 13.000 1.2085 0.02714 0.02301 0.0289 0.0043 1.0000 13.250 1.2116 0.02847 0.02445 0.0312 0.0043 1.0000 13.500 1.2017 0.03093 0.02710 0.0338 0.0041 1.0000 13.750 1.1968 0.03326 0.02960 0.0352 0.0041 1.0000 14.000 1.1908 0.03600 0.03250 0.0359 0.0041 1.0000 14.250 1.1865 0.03886 0.03550 0.0358 0.0041 1.0000 14.500 1.1882 0.04132 0.03807 0.0354 0.0040 1.0000 14.750 1.1768 0.04563 0.04255 0.0338 0.0040 1.0000 15.000 1.1603 0.05109 0.04819 0.0312 0.0040 1.0000 15.250 1.1435 0.05711 0.05437 0.0278 0.0040 1.0000 15.500 1.1427 0.06096 0.05831 0.0255 0.0040 1.0000 15.750 1.0952 0.07366 0.07125 0.0174 0.0040 1.0000 16.000 1.0347 0.09114 0.08898 0.0068 0.0041 1.0000 16.250 1.0050 0.10209 0.10004 0.0012 0.0042 1.0000