XFOIL Version 6.96 Calculated polar for: EH 0.0/9.0 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 ------ -------- --------- --------- -------- -------- -------- -14.750 -0.9105 0.10675 0.10498 0.0108 1.0000 0.0016 -14.500 -0.9505 0.09327 0.09141 0.0037 1.0000 0.0016 -14.250 -0.9806 0.08214 0.08020 -0.0024 1.0000 0.0015 -14.000 -1.0317 0.06627 0.06412 -0.0124 1.0000 0.0015 -13.750 -1.0475 0.05847 0.05620 -0.0179 1.0000 0.0015 -13.500 -1.0717 0.04997 0.04751 -0.0242 1.0000 0.0015 -13.250 -1.0894 0.04398 0.04134 -0.0279 1.0000 0.0015 -13.000 -1.1030 0.03963 0.03682 -0.0296 1.0000 0.0015 -12.750 -1.1204 0.03574 0.03273 -0.0294 1.0000 0.0015 -12.500 -1.1296 0.03320 0.03003 -0.0278 1.0000 0.0015 -12.250 -1.1385 0.03104 0.02769 -0.0248 1.0000 0.0015 -12.000 -1.1443 0.02914 0.02561 -0.0213 1.0000 0.0015 -11.750 -1.1402 0.02733 0.02361 -0.0192 1.0000 0.0015 -11.500 -1.1319 0.02570 0.02179 -0.0173 1.0000 0.0015 -11.250 -1.1212 0.02412 0.02002 -0.0156 1.0000 0.0016 -11.000 -1.1076 0.02274 0.01847 -0.0141 1.0000 0.0016 -10.750 -1.0923 0.02147 0.01701 -0.0128 1.0000 0.0017 -10.500 -1.0754 0.02032 0.01570 -0.0116 1.0000 0.0017 -10.250 -1.0568 0.01933 0.01458 -0.0106 1.0000 0.0017 -10.000 -1.0358 0.01861 0.01377 -0.0098 1.0000 0.0018 -9.750 -1.0158 0.01773 0.01276 -0.0089 1.0000 0.0018 -9.500 -0.9982 0.01642 0.01127 -0.0075 1.0000 0.0021 -9.250 -0.9770 0.01562 0.01038 -0.0067 1.0000 0.0022 -9.000 -0.9541 0.01509 0.00981 -0.0061 1.0000 0.0026 -8.750 -0.9312 0.01454 0.00920 -0.0054 1.0000 0.0028 -8.500 -0.9081 0.01400 0.00856 -0.0048 1.0000 0.0030 -8.250 -0.8847 0.01353 0.00804 -0.0041 1.0000 0.0033 -8.000 -0.8611 0.01308 0.00752 -0.0035 1.0000 0.0036 -7.750 -0.8372 0.01269 0.00709 -0.0029 1.0000 0.0038 -7.500 -0.8141 0.01218 0.00651 -0.0021 1.0000 0.0042 -7.250 -0.7910 0.01172 0.00601 -0.0013 1.0000 0.0048 -7.000 -0.7676 0.01135 0.00562 -0.0006 1.0000 0.0053 -6.750 -0.7442 0.01101 0.00526 0.0002 1.0000 0.0060 -6.500 -0.7206 0.01073 0.00495 0.0010 1.0000 0.0066 -6.250 -0.6976 0.01038 0.00455 0.0019 1.0000 0.0078 -6.000 -0.6661 0.01001 0.00419 0.0009 0.9970 0.0099 -5.750 -0.6334 0.00974 0.00390 -0.0004 0.9936 0.0115 -5.500 -0.6030 0.00939 0.00356 -0.0011 0.9893 0.0158 -5.250 -0.5710 0.00913 0.00329 -0.0021 0.9849 0.0188 -5.000 -0.5388 0.00885 0.00302 -0.0032 0.9798 0.0249 -4.750 -0.5076 0.00855 0.00275 -0.0040 0.9715 0.0359 -4.500 -0.4768 0.00825 0.00251 -0.0048 0.9611 0.0518 -4.250 -0.4479 0.00789 0.00227 -0.0051 0.9479 0.0805 -4.000 -0.4208 0.00762 0.00206 -0.0050 0.9323 0.1051 -3.750 -0.3951 0.00738 0.00188 -0.0045 0.9149 0.1308 -3.500 -0.3700 0.00712 0.00169 -0.0040 0.8971 0.1645 -3.250 -0.3442 0.00694 0.00154 -0.0036 0.8793 0.1893 -3.000 -0.3188 0.00670 0.00139 -0.0031 0.8610 0.2291 -2.750 -0.2929 0.00653 0.00127 -0.0027 0.8421 0.2609 -2.500 -0.2668 0.00638 0.00114 -0.0024 0.8220 0.2937 -2.250 -0.2407 0.00621 0.00104 -0.0020 0.8019 0.3314 -2.000 -0.2142 0.00610 0.00096 -0.0017 0.7811 0.3620 -1.500 -0.1610 0.00590 0.00082 -0.0012 0.7392 0.4221 -1.250 -0.1343 0.00583 0.00076 -0.0010 0.7162 0.4514 -1.000 -0.1075 0.00578 0.00071 -0.0008 0.6920 0.4800 -0.750 -0.0807 0.00574 0.00068 -0.0006 0.6671 0.5079 -0.500 -0.0538 0.00571 0.00066 -0.0004 0.6423 0.5356 -0.250 -0.0269 0.00568 0.00064 -0.0002 0.6175 0.5643 0.000 0.0000 0.00567 0.00063 0.0000 0.5921 0.5922 0.250 0.0268 0.00568 0.00064 0.0002 0.5643 0.6176 0.500 0.0537 0.00571 0.00066 0.0004 0.5356 0.6422 0.750 0.0806 0.00574 0.00068 0.0006 0.5074 0.6672 1.000 0.1075 0.00578 0.00071 0.0008 0.4801 0.6919 1.250 0.1342 0.00583 0.00076 0.0010 0.4516 0.7160 1.500 0.1609 0.00590 0.00082 0.0013 0.4219 0.7390 2.000 0.2141 0.00610 0.00096 0.0018 0.3619 0.7811 2.250 0.2406 0.00622 0.00104 0.0020 0.3310 0.8020 2.500 0.2667 0.00638 0.00114 0.0024 0.2936 0.8221 2.750 0.2928 0.00653 0.00127 0.0027 0.2610 0.8422 3.000 0.3187 0.00670 0.00139 0.0031 0.2301 0.8611 3.250 0.3441 0.00694 0.00154 0.0036 0.1898 0.8794 3.500 0.3699 0.00712 0.00168 0.0040 0.1652 0.8973 3.750 0.3951 0.00738 0.00188 0.0046 0.1307 0.9150 4.000 0.4208 0.00762 0.00206 0.0050 0.1050 0.9323 4.250 0.4479 0.00788 0.00226 0.0051 0.0815 0.9480 4.500 0.4769 0.00825 0.00251 0.0048 0.0522 0.9612 4.750 0.5078 0.00855 0.00275 0.0040 0.0359 0.9716 5.000 0.5390 0.00885 0.00302 0.0031 0.0249 0.9799 5.250 0.5712 0.00913 0.00329 0.0020 0.0188 0.9850 5.500 0.6033 0.00939 0.00356 0.0010 0.0157 0.9894 6.000 0.6665 0.01001 0.00419 -0.0010 0.0099 0.9972 6.250 0.6972 0.01039 0.00455 -0.0018 0.0077 1.0000 6.500 0.7202 0.01074 0.00496 -0.0009 0.0066 1.0000 6.750 0.7439 0.01102 0.00527 -0.0001 0.0060 1.0000 7.000 0.7674 0.01135 0.00562 0.0006 0.0054 1.0000 7.250 0.7909 0.01172 0.00602 0.0013 0.0048 1.0000 7.500 0.8141 0.01218 0.00651 0.0021 0.0042 1.0000 7.750 0.8373 0.01268 0.00707 0.0029 0.0038 1.0000 8.000 0.8610 0.01310 0.00755 0.0035 0.0036 1.0000 8.250 0.8846 0.01355 0.00806 0.0041 0.0033 1.0000 8.500 0.9082 0.01402 0.00859 0.0047 0.0030 1.0000 8.750 0.9313 0.01456 0.00922 0.0054 0.0028 1.0000 9.000 0.9545 0.01506 0.00977 0.0060 0.0025 1.0000 9.250 0.9771 0.01565 0.01041 0.0067 0.0023 1.0000 9.500 0.9987 0.01639 0.01124 0.0075 0.0021 1.0000 9.750 1.0160 0.01774 0.01278 0.0088 0.0018 1.0000 10.000 1.0368 0.01851 0.01366 0.0096 0.0018 1.0000 10.250 1.0569 0.01935 0.01461 0.0105 0.0018 1.0000 10.500 1.0757 0.02033 0.01571 0.0115 0.0017 1.0000 10.750 1.0926 0.02149 0.01703 0.0127 0.0017 1.0000 11.000 1.1085 0.02269 0.01841 0.0140 0.0016 1.0000 11.250 1.1221 0.02408 0.01998 0.0155 0.0016 1.0000 11.500 1.1330 0.02564 0.02172 0.0171 0.0016 1.0000 11.750 1.1407 0.02736 0.02364 0.0191 0.0015 1.0000 12.000 1.1447 0.02919 0.02566 0.0212 0.0015 1.0000 12.250 1.1396 0.03105 0.02770 0.0247 0.0015 1.0000 12.500 1.1314 0.03315 0.02997 0.0275 0.0015 1.0000 12.750 1.1204 0.03584 0.03284 0.0293 0.0015 1.0000 13.000 1.1058 0.03944 0.03663 0.0294 0.0015 1.0000 13.250 1.0921 0.04378 0.04113 0.0279 0.0015 1.0000 13.500 1.0682 0.05078 0.04835 0.0234 0.0015 1.0000 13.750 1.0508 0.05810 0.05582 0.0180 0.0015 1.0000 14.000 1.0258 0.06791 0.06579 0.0110 0.0015 1.0000 14.250 0.9884 0.08080 0.07884 0.0029 0.0015 1.0000 14.500 0.9508 0.09361 0.09175 -0.0042 0.0016 1.0000 14.750 0.9117 0.10691 0.10514 -0.0111 0.0016 1.0000