XFOIL Version 6.96 Calculated polar for: AH 93-K-131/15 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -9.250 -0.4066 0.09044 0.08676 -0.0338 0.7943 0.0178 -9.000 -0.4086 0.08518 0.08152 -0.0381 0.7924 0.0176 -8.750 -0.4139 0.07915 0.07551 -0.0442 0.7903 0.0174 -8.500 -0.4226 0.07319 0.06950 -0.0489 0.7883 0.0172 -8.250 -0.4328 0.06798 0.06419 -0.0508 0.7866 0.0171 -8.000 -0.4390 0.06228 0.05834 -0.0522 0.7853 0.0170 -7.750 -0.4434 0.05646 0.05228 -0.0525 0.7842 0.0170 -7.500 -0.4439 0.05022 0.04573 -0.0525 0.7816 0.0171 -7.250 -0.4433 0.04393 0.03899 -0.0512 0.7788 0.0175 -7.000 -0.4461 0.03655 0.03071 -0.0478 0.7765 0.0188 -6.750 -0.4339 0.03361 0.02736 -0.0461 0.7747 0.0193 -6.500 -0.4161 0.03185 0.02535 -0.0450 0.7733 0.0198 -6.250 -0.3971 0.03020 0.02342 -0.0438 0.7720 0.0204 -6.000 -0.3771 0.02856 0.02148 -0.0426 0.7708 0.0212 -5.750 -0.3560 0.02694 0.01952 -0.0414 0.7698 0.0221 -5.500 -0.3299 0.02566 0.01792 -0.0416 0.7664 0.0236 -5.250 -0.3044 0.02454 0.01650 -0.0413 0.7638 0.0252 -5.000 -0.2797 0.02355 0.01544 -0.0411 0.7618 0.0264 -4.750 -0.2544 0.02275 0.01453 -0.0407 0.7600 0.0277 -4.500 -0.2290 0.02197 0.01360 -0.0403 0.7586 0.0293 -4.250 -0.2033 0.02137 0.01285 -0.0398 0.7574 0.0315 -4.000 -0.1783 0.02054 0.01193 -0.0392 0.7563 0.0335 -3.750 -0.1528 0.01993 0.01131 -0.0391 0.7541 0.0354 -3.500 -0.1260 0.01963 0.01099 -0.0395 0.7503 0.0378 -3.250 -0.1002 0.01930 0.01060 -0.0393 0.7479 0.0411 -3.000 -0.0757 0.01878 0.01003 -0.0387 0.7459 0.0440 -2.750 -0.0514 0.01831 0.00955 -0.0381 0.7444 0.0475 -2.500 -0.0263 0.01795 0.00913 -0.0375 0.7431 0.0525 -2.250 -0.0017 0.01753 0.00869 -0.0368 0.7420 0.0593 -2.000 0.0246 0.01751 0.00866 -0.0371 0.7378 0.0679 -1.750 0.0496 0.01729 0.00854 -0.0369 0.7344 0.0877 -1.500 0.0733 0.01685 0.00831 -0.0363 0.7322 0.1425 -1.250 0.0939 0.01612 0.00807 -0.0352 0.7304 0.2778 -1.000 0.1937 0.01435 0.00849 -0.0495 0.7310 0.8946 -0.750 0.2243 0.01465 0.00870 -0.0493 0.7296 0.9421 -0.500 0.3118 0.01504 0.00895 -0.0609 0.7294 0.9874 -0.250 0.3681 0.01477 0.00857 -0.0669 0.7285 0.9982 0.000 0.3980 0.01458 0.00828 -0.0675 0.7273 1.0000 0.250 0.4271 0.01488 0.00858 -0.0688 0.7215 1.0000 0.500 0.4523 0.01484 0.00849 -0.0686 0.7185 1.0000 0.750 0.4769 0.01471 0.00830 -0.0681 0.7163 1.0000 1.000 0.5012 0.01455 0.00808 -0.0674 0.7145 1.0000 1.250 0.5263 0.01448 0.00798 -0.0671 0.7120 1.0000 1.500 0.5536 0.01473 0.00825 -0.0678 0.7063 1.0000 1.750 0.5787 0.01464 0.00815 -0.0674 0.7033 1.0000 2.000 0.6034 0.01448 0.00796 -0.0668 0.7011 1.0000 2.250 0.6281 0.01429 0.00773 -0.0661 0.6993 1.0000 2.500 0.6549 0.01461 0.00812 -0.0668 0.6926 1.0000 2.750 0.6801 0.01451 0.00803 -0.0664 0.6890 1.0000 3.000 0.7049 0.01428 0.00779 -0.0656 0.6863 1.0000 3.250 0.7306 0.01441 0.00796 -0.0657 0.6803 1.0000 3.500 0.7558 0.01437 0.00796 -0.0654 0.6752 1.0000 3.750 0.7809 0.01412 0.00771 -0.0646 0.6718 1.0000 4.000 0.8061 0.01430 0.00796 -0.0647 0.6644 1.0000 4.250 0.8312 0.01416 0.00784 -0.0642 0.6593 1.0000 4.500 0.8561 0.01416 0.00790 -0.0638 0.6530 1.0000 4.750 0.8810 0.01414 0.00794 -0.0634 0.6458 1.0000 5.000 0.9057 0.01412 0.00796 -0.0630 0.6382 1.0000 5.250 0.9305 0.01402 0.00791 -0.0624 0.6300 1.0000 5.500 0.9547 0.01407 0.00802 -0.0619 0.6189 1.0000 5.750 0.9788 0.01405 0.00803 -0.0613 0.6072 1.0000 6.000 1.0025 0.01402 0.00801 -0.0605 0.5919 1.0000 6.250 1.0257 0.01397 0.00792 -0.0596 0.5714 1.0000 6.500 1.0475 0.01413 0.00804 -0.0586 0.5478 1.0000 6.750 1.0682 0.01437 0.00821 -0.0575 0.5229 1.0000 7.000 1.0864 0.01478 0.00851 -0.0561 0.4928 1.0000 7.250 1.1010 0.01537 0.00896 -0.0543 0.4588 1.0000 7.500 1.1110 0.01617 0.00961 -0.0519 0.4236 1.0000 7.750 1.1164 0.01711 0.01041 -0.0490 0.3887 1.0000 8.000 1.1155 0.01821 0.01136 -0.0451 0.3562 1.0000 8.250 1.1058 0.01922 0.01223 -0.0395 0.3305 1.0000 8.500 1.0984 0.02027 0.01315 -0.0345 0.3038 1.0000 8.750 1.0938 0.02141 0.01414 -0.0301 0.2756 1.0000 9.000 1.0906 0.02263 0.01521 -0.0262 0.2454 1.0000 9.250 1.0883 0.02393 0.01635 -0.0226 0.2146 1.0000 9.500 1.0870 0.02529 0.01757 -0.0194 0.1840 1.0000 9.750 1.0865 0.02670 0.01881 -0.0164 0.1548 1.0000 10.000 1.0876 0.02811 0.02008 -0.0137 0.1291 1.0000 10.500 1.0943 0.03086 0.02264 -0.0092 0.0904 1.0000 10.750 1.0995 0.03220 0.02394 -0.0073 0.0764 1.0000 11.000 1.1050 0.03357 0.02528 -0.0055 0.0645 1.0000 11.250 1.1105 0.03499 0.02668 -0.0038 0.0545 1.0000 11.500 1.1155 0.03651 0.02820 -0.0022 0.0461 1.0000 11.750 1.1222 0.03797 0.02969 -0.0008 0.0391 1.0000 12.000 1.1280 0.03956 0.03132 0.0006 0.0336 1.0000 12.250 1.1330 0.04127 0.03305 0.0019 0.0291 1.0000 12.500 1.1384 0.04299 0.03484 0.0032 0.0256 1.0000 12.750 1.1435 0.04478 0.03669 0.0043 0.0227 1.0000 13.000 1.1455 0.04694 0.03889 0.0054 0.0208 1.0000 13.250 1.1502 0.04889 0.04097 0.0064 0.0192 1.0000 13.500 1.1537 0.05099 0.04321 0.0073 0.0179 1.0000 13.750 1.1565 0.05324 0.04554 0.0081 0.0168 1.0000 14.000 1.1562 0.05586 0.04823 0.0089 0.0158 1.0000 14.250 1.1576 0.05836 0.05084 0.0096 0.0150 1.0000 14.500 1.1603 0.06077 0.05339 0.0101 0.0142 1.0000 14.750 1.1626 0.06330 0.05602 0.0104 0.0134 1.0000 15.000 1.1642 0.06596 0.05879 0.0107 0.0127 1.0000 15.250 1.1644 0.06884 0.06177 0.0108 0.0122 1.0000 15.500 1.1626 0.07199 0.06502 0.0109 0.0119 1.0000 15.750 1.1589 0.07545 0.06856 0.0109 0.0115 1.0000 16.000 1.1586 0.07856 0.07181 0.0109 0.0112 1.0000 16.250 1.1580 0.08175 0.07516 0.0108 0.0110 1.0000 16.500 1.1566 0.08510 0.07869 0.0105 0.0107 1.0000 16.750 1.1547 0.08860 0.08234 0.0101 0.0105 1.0000 17.000 1.1521 0.09228 0.08617 0.0096 0.0102 1.0000 17.250 1.1488 0.09614 0.09018 0.0088 0.0100 1.0000 17.500 1.1447 0.10019 0.09439 0.0079 0.0099 1.0000 17.750 1.1397 0.10448 0.09883 0.0067 0.0097 1.0000 18.000 1.1338 0.10904 0.10355 0.0053 0.0096 1.0000 18.250 1.1271 0.11386 0.10853 0.0036 0.0094 1.0000 18.500 1.1196 0.11895 0.11378 0.0015 0.0093 1.0000 18.750 1.1114 0.12430 0.11928 -0.0008 0.0092 1.0000 19.000 1.1025 0.12995 0.12509 -0.0035 0.0091 1.0000 19.250 1.0927 0.13598 0.13128 -0.0065 0.0090 1.0000