XFOIL Version 6.96 Calculated polar for: PW98-mod 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 2.000 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -7.500 -0.7196 0.01613 0.01271 -0.0101 1.0000 0.0032 -7.250 -0.6993 0.01280 0.00887 -0.0089 1.0000 0.0029 -7.000 -0.6740 0.01150 0.00736 -0.0084 1.0000 0.0027 -6.750 -0.6480 0.01046 0.00614 -0.0080 1.0000 0.0025 -6.500 -0.6188 0.00953 0.00501 -0.0082 0.9824 0.0024 -4.500 -0.4037 0.01106 0.00620 -0.0054 0.8086 0.0015 -4.250 -0.3758 0.01121 0.00630 -0.0055 0.7864 0.0014 -4.000 -0.3480 0.01111 0.00613 -0.0054 0.7650 0.0014 -3.750 -0.3202 0.01095 0.00588 -0.0054 0.7439 0.0014 -3.500 -0.2924 0.01072 0.00556 -0.0053 0.7234 0.0013 -3.250 -0.2646 0.01047 0.00521 -0.0052 0.7038 0.0013 -3.000 -0.2367 0.01019 0.00484 -0.0051 0.6846 0.0013 -2.750 -0.2088 0.00990 0.00447 -0.0051 0.6664 0.0013 -2.000 -0.1245 0.00977 0.00398 -0.0053 0.6149 0.0021 -1.750 -0.0985 0.00705 0.00100 -0.0034 0.6013 0.0052 -1.500 -0.0701 0.00701 0.00093 -0.0034 0.5856 0.0061 -1.250 -0.0417 0.00698 0.00089 -0.0035 0.5697 0.0072 -1.000 -0.0133 0.00696 0.00084 -0.0035 0.5538 0.0077 -0.500 0.0435 0.00694 0.00079 -0.0037 0.5219 0.0093 -0.250 0.0721 0.00692 0.00070 -0.0037 0.5060 0.0093 0.000 0.1007 0.00691 0.00063 -0.0038 0.4906 0.0109 0.250 0.1292 0.00690 0.00065 -0.0038 0.4754 0.0235 0.500 0.1569 0.00663 0.00061 -0.0039 0.4601 0.1222 0.750 0.1840 0.00617 0.00059 -0.0040 0.4453 0.2944 1.000 0.2092 0.00532 0.00058 -0.0039 0.4305 0.5976 1.250 0.2264 0.00436 0.00066 -0.0015 0.4173 0.9319 1.500 0.2567 0.00440 0.00073 -0.0017 0.4019 0.9832 1.750 0.2899 0.00450 0.00077 -0.0028 0.3856 0.9905 2.000 0.3264 0.00462 0.00081 -0.0047 0.3679 0.9949 2.250 0.3644 0.00475 0.00085 -0.0070 0.3505 0.9983 2.500 0.3985 0.00486 0.00090 -0.0084 0.3354 1.0000 2.750 0.4253 0.00499 0.00095 -0.0082 0.3167 1.0000 3.000 0.4519 0.00522 0.00102 -0.0081 0.2824 1.0000 3.250 0.4780 0.00567 0.00116 -0.0080 0.2158 1.0000 3.500 0.5025 0.00676 0.00158 -0.0080 0.0753 1.0000 3.750 0.5278 0.00742 0.00195 -0.0078 0.0077 1.0000 4.250 0.5807 0.00777 0.00227 -0.0072 0.0012 1.0000 4.500 0.6074 0.00791 0.00238 -0.0070 0.0011 1.0000 4.750 0.6342 0.00805 0.00249 -0.0068 0.0011 1.0000 5.000 0.6612 0.00821 0.00262 -0.0067 0.0011 1.0000 5.250 0.6882 0.00837 0.00276 -0.0066 0.0012 1.0000 5.500 0.7153 0.00856 0.00293 -0.0065 0.0012 1.0000 5.750 0.7424 0.00876 0.00314 -0.0064 0.0014 1.0000 6.250 0.7969 0.00909 0.00351 -0.0063 0.0019 1.0000 7.000 0.8785 0.00976 0.00420 -0.0061 0.0026 1.0000 7.250 0.9056 0.01004 0.00460 -0.0060 0.0032 1.0000 7.500 0.9324 0.01036 0.00499 -0.0058 0.0036 1.0000 7.750 0.9591 0.01074 0.00545 -0.0057 0.0040 1.0000 8.000 0.9853 0.01122 0.00602 -0.0055 0.0039 1.0000 8.250 1.0109 0.01181 0.00672 -0.0052 0.0035 1.0000 8.500 1.0356 0.01259 0.00763 -0.0049 0.0031 1.0000 8.750 1.0577 0.01388 0.00912 -0.0043 0.0026 1.0000 9.000 1.0763 0.01575 0.01123 -0.0035 0.0022 1.0000 9.250 1.1018 0.01609 0.01159 -0.0034 0.0020 1.0000 9.500 1.1246 0.01692 0.01249 -0.0030 0.0018 1.0000 9.750 1.1464 0.01789 0.01355 -0.0026 0.0016 1.0000 10.000 1.1673 0.01894 0.01469 -0.0022 0.0014 1.0000 10.250 1.1859 0.02032 0.01624 -0.0015 0.0014 1.0000 10.500 1.2046 0.02155 0.01758 -0.0009 0.0013 1.0000 10.750 1.2222 0.02285 0.01899 -0.0003 0.0012 1.0000 11.000 1.2382 0.02422 0.02048 0.0004 0.0011 1.0000 11.250 1.2524 0.02571 0.02209 0.0011 0.0010 1.0000 11.500 1.2641 0.02735 0.02384 0.0019 0.0010 1.0000 11.750 1.2721 0.02916 0.02578 0.0029 0.0009 1.0000 12.000 1.2722 0.03124 0.02799 0.0041 0.0009 1.0000 12.250 1.2698 0.03392 0.03082 0.0042 0.0008 1.0000 12.500 1.2657 0.03738 0.03442 0.0030 0.0008 1.0000 12.750 1.2599 0.04160 0.03879 0.0008 0.0008 1.0000 13.000 1.2518 0.04660 0.04393 -0.0023 0.0008 1.0000 13.250 1.2410 0.05226 0.04974 -0.0058 0.0008 1.0000 13.500 1.2278 0.05853 0.05615 -0.0096 0.0008 1.0000 13.750 1.2120 0.06536 0.06311 -0.0137 0.0008 1.0000 14.000 1.1942 0.07260 0.07047 -0.0177 0.0008 1.0000 14.250 1.1744 0.08031 0.07830 -0.0218 0.0008 1.0000 14.500 1.1522 0.08862 0.08673 -0.0261 0.0009 1.0000 14.750 1.1290 0.09746 0.09569 -0.0305 0.0009 1.0000 15.000 1.1051 0.10680 0.10514 -0.0352 0.0009 1.0000 15.250 1.0797 0.11676 0.11522 -0.0400 0.0010 1.0000 15.500 1.0507 0.12801 0.12659 -0.0453 0.0011 1.0000 15.750 1.0202 0.14026 0.13896 -0.0511 0.0012 1.0000 16.000 0.9749 0.15776 0.15660 -0.0592 0.0014 1.0000 17.000 0.6492 0.18469 0.18363 -0.0466 0.0081 1.0000 17.250 0.6497 0.18815 0.18709 -0.0479 0.0081 1.0000 17.500 0.6506 0.19153 0.19047 -0.0491 0.0081 1.0000 17.750 0.6520 0.19488 0.19382 -0.0504 0.0081 1.0000 18.000 0.6535 0.19815 0.19709 -0.0516 0.0081 1.0000 18.250 0.6555 0.20138 0.20032 -0.0528 0.0080 1.0000 18.500 0.6579 0.20449 0.20343 -0.0540 0.0080 1.0000 18.750 0.6611 0.20740 0.20634 -0.0552 0.0078 1.0000 19.000 0.6676 0.20956 0.20851 -0.0564 0.0068 1.0000 19.250 0.6703 0.21280 0.21175 -0.0577 0.0058 1.0000 19.500 0.6729 0.21587 0.21482 -0.0589 0.0050 1.0000 19.750 0.6756 0.21877 0.21772 -0.0602 0.0044 1.0000 20.000 0.6786 0.22155 0.22050 -0.0614 0.0040 1.0000