XFOIL Version 6.96 Calculated polar for: FX 66-H-80 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -8.000 -0.5443 0.09023 0.08780 0.0184 0.7732 0.0082 -7.750 -0.5483 0.08660 0.08406 0.0163 0.7361 0.0082 -7.500 -0.5515 0.08300 0.08037 0.0143 0.7076 0.0082 -7.250 -0.5487 0.07882 0.07608 0.0117 0.6834 0.0082 -6.750 -0.5353 0.07006 0.06708 0.0068 0.6445 0.0083 -5.250 -0.4585 0.04312 0.03907 0.0011 0.5673 0.0079 -5.000 -0.4417 0.03873 0.03440 0.0014 0.5573 0.0074 -4.750 -0.4224 0.03460 0.02996 0.0021 0.5473 0.0071 -4.500 -0.4021 0.03046 0.02546 0.0033 0.5382 0.0069 -4.250 -0.3809 0.02624 0.02080 0.0048 0.5300 0.0067 -4.000 -0.3589 0.02200 0.01603 0.0066 0.5223 0.0066 -3.750 -0.3353 0.01867 0.01218 0.0082 0.5149 0.0068 -3.500 -0.3098 0.01668 0.00976 0.0092 0.5065 0.0074 -3.250 -0.2837 0.01544 0.00824 0.0098 0.4988 0.0078 -3.000 -0.2572 0.01454 0.00713 0.0103 0.4913 0.0081 -2.750 -0.2311 0.01355 0.00595 0.0109 0.4846 0.0086 -2.500 -0.2054 0.01271 0.00498 0.0114 0.4780 0.0096 -2.250 -0.1794 0.01206 0.00422 0.0119 0.4722 0.0098 -2.000 -0.1535 0.01148 0.00352 0.0125 0.4662 0.0100 -1.750 -0.1273 0.01105 0.00299 0.0130 0.4609 0.0102 -1.500 -0.1008 0.01069 0.00255 0.0134 0.4558 0.0108 -1.250 -0.0741 0.01042 0.00220 0.0138 0.4506 0.0120 -1.000 -0.0471 0.01023 0.00192 0.0141 0.4460 0.0141 -0.750 -0.0203 0.00999 0.00167 0.0145 0.4412 0.0268 -0.500 0.0063 0.00977 0.00154 0.0147 0.4368 0.0607 -0.250 0.0308 0.00922 0.00144 0.0152 0.4328 0.2020 0.000 0.0357 0.00692 0.00129 0.0195 0.4293 0.8123 0.250 0.0963 0.00689 0.00146 0.0131 0.4235 0.9586 0.500 0.1522 0.00712 0.00158 0.0073 0.4188 0.9835 0.750 0.2154 0.00724 0.00159 -0.0002 0.4129 0.9959 1.000 0.2503 0.00727 0.00152 -0.0018 0.4084 0.9984 1.250 0.2823 0.00729 0.00149 -0.0028 0.4046 0.9999 1.500 0.3080 0.00730 0.00148 -0.0024 0.4008 1.0000 1.750 0.3335 0.00734 0.00147 -0.0019 0.3967 1.0000 2.000 0.3590 0.00739 0.00148 -0.0014 0.3929 1.0000 2.250 0.3846 0.00741 0.00150 -0.0010 0.3889 1.0000 2.500 0.4101 0.00746 0.00153 -0.0005 0.3849 1.0000 2.750 0.4357 0.00752 0.00157 -0.0001 0.3811 1.0000 3.000 0.4613 0.00758 0.00163 0.0004 0.3772 1.0000 3.250 0.4869 0.00764 0.00171 0.0008 0.3728 1.0000 3.500 0.5125 0.00771 0.00179 0.0012 0.3688 1.0000 3.750 0.5381 0.00780 0.00188 0.0017 0.3651 1.0000 4.000 0.5638 0.00786 0.00198 0.0021 0.3606 1.0000 4.250 0.5894 0.00795 0.00209 0.0025 0.3560 1.0000 4.500 0.6150 0.00806 0.00224 0.0029 0.3521 1.0000 4.750 0.6408 0.00815 0.00238 0.0033 0.3474 1.0000 5.000 0.6663 0.00825 0.00250 0.0037 0.3365 1.0000 5.250 0.6918 0.00837 0.00262 0.0041 0.3204 1.0000 5.500 0.7169 0.00859 0.00276 0.0045 0.2933 1.0000 5.750 0.7405 0.00916 0.00307 0.0048 0.2299 1.0000 6.000 0.7613 0.01046 0.00385 0.0051 0.1189 1.0000 6.250 0.7819 0.01174 0.00475 0.0056 0.0383 1.0000 6.500 0.8052 0.01236 0.00532 0.0060 0.0210 1.0000 6.750 0.8292 0.01280 0.00583 0.0065 0.0165 1.0000 7.000 0.8527 0.01331 0.00643 0.0071 0.0136 1.0000 7.250 0.8753 0.01402 0.00723 0.0076 0.0108 1.0000 7.500 0.8987 0.01446 0.00775 0.0081 0.0095 1.0000 7.750 0.9213 0.01507 0.00844 0.0087 0.0082 1.0000 8.000 0.9428 0.01584 0.00929 0.0093 0.0070 1.0000 8.250 0.9609 0.01715 0.01075 0.0102 0.0061 1.0000 8.500 0.9817 0.01788 0.01159 0.0109 0.0056 1.0000 8.750 1.0025 0.01857 0.01235 0.0115 0.0049 1.0000 9.000 1.0228 0.01926 0.01315 0.0121 0.0044 1.0000 9.250 1.0409 0.02023 0.01420 0.0129 0.0040 1.0000 9.500 1.0574 0.02132 0.01540 0.0138 0.0038 1.0000 9.750 1.0693 0.02287 0.01706 0.0149 0.0035 1.0000 10.000 1.0767 0.02481 0.01916 0.0164 0.0033 1.0000 10.250 1.0872 0.02627 0.02075 0.0175 0.0032 1.0000 10.500 1.0954 0.02785 0.02248 0.0188 0.0032 1.0000 10.750 1.0975 0.02961 0.02438 0.0203 0.0030 1.0000 11.000 1.0962 0.03196 0.02689 0.0209 0.0030 1.0000 11.250 1.0968 0.03456 0.02965 0.0208 0.0029 1.0000 11.500 1.0978 0.03733 0.03258 0.0205 0.0027 1.0000 11.750 1.0965 0.04049 0.03592 0.0200 0.0026 1.0000 12.000 1.0948 0.04374 0.03933 0.0193 0.0026 1.0000 12.250 1.0894 0.04757 0.04335 0.0184 0.0026 1.0000 12.500 1.0831 0.05162 0.04758 0.0171 0.0025 1.0000 12.750 1.0750 0.05597 0.05211 0.0155 0.0026 1.0000 13.000 1.0641 0.06090 0.05722 0.0136 0.0025 1.0000 13.250 1.0499 0.06644 0.06295 0.0112 0.0025 1.0000 13.500 1.0381 0.07173 0.06839 0.0087 0.0025 1.0000 13.750 1.0227 0.07783 0.07465 0.0057 0.0024 1.0000 14.000 1.0096 0.08392 0.08088 0.0026 0.0025 1.0000 14.250 0.9908 0.09159 0.08871 -0.0015 0.0025 1.0000 14.500 0.9717 0.09978 0.09704 -0.0059 0.0025 1.0000 14.750 0.9559 0.10767 0.10506 -0.0102 0.0026 1.0000 15.000 0.9377 0.11659 0.11409 -0.0150 0.0026 1.0000 15.250 0.9204 0.12591 0.12352 -0.0199 0.0026 1.0000 15.500 0.8946 0.13852 0.13623 -0.0261 0.0027 1.0000