XFOIL Version 6.96 Calculated polar for: PSU 94-097 (AIAA 2001-2478) 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 ------ -------- --------- --------- -------- -------- -------- -10.000 -0.3529 0.11451 0.11224 -0.0274 1.0000 0.0072 -9.750 -0.3469 0.11092 0.10866 -0.0291 1.0000 0.0072 -9.500 -0.3409 0.10731 0.10507 -0.0308 0.9999 0.0073 -9.250 -0.3306 0.10321 0.10096 -0.0341 0.9723 0.0073 -9.000 -0.3218 0.09924 0.09698 -0.0368 0.9533 0.0073 -8.750 -0.3163 0.09562 0.09334 -0.0384 0.9351 0.0073 -8.000 -0.2174 0.07102 0.06859 -0.0475 0.8563 0.0062 -7.750 -0.2184 0.06658 0.06414 -0.0490 0.8479 0.0056 -7.500 -0.2253 0.06005 0.05760 -0.0514 0.8404 0.0044 -7.250 -0.2952 0.07185 0.06937 -0.0512 0.8585 0.0044 -7.000 -0.2839 0.06686 0.06435 -0.0577 0.8485 0.0043 -6.750 -0.2680 0.06096 0.05839 -0.0662 0.8395 0.0042 -6.500 -0.2480 0.05412 0.05143 -0.0757 0.8311 0.0040 -6.250 -0.2249 0.04643 0.04356 -0.0847 0.8237 0.0039 -6.000 -0.2001 0.03797 0.03477 -0.0919 0.8169 0.0038 -5.750 -0.1735 0.02749 0.02363 -0.0975 0.8110 0.0036 -5.500 -0.1444 0.01877 0.01381 -0.1003 0.8053 0.0038 -5.250 -0.1154 0.01627 0.01077 -0.1010 0.7999 0.0041 -5.000 -0.0863 0.01491 0.00906 -0.1014 0.7940 0.0044 -4.750 -0.0576 0.01403 0.00793 -0.1017 0.7884 0.0046 -4.500 -0.0286 0.01279 0.00648 -0.1021 0.7832 0.0049 -4.250 0.0001 0.01232 0.00593 -0.1025 0.7775 0.0054 -4.000 0.0288 0.01198 0.00550 -0.1028 0.7726 0.0062 -3.750 0.0581 0.01148 0.00489 -0.1031 0.7673 0.0068 -3.500 0.0875 0.01092 0.00422 -0.1035 0.7622 0.0070 -3.250 0.1170 0.01047 0.00367 -0.1039 0.7575 0.0072 -3.000 0.1468 0.01001 0.00311 -0.1043 0.7524 0.0078 -2.750 0.1764 0.00972 0.00274 -0.1046 0.7475 0.0093 -2.500 0.2059 0.00944 0.00241 -0.1050 0.7430 0.0150 -2.250 0.2356 0.00914 0.00220 -0.1055 0.7380 0.0396 -2.000 0.2651 0.00881 0.00205 -0.1060 0.7332 0.0972 -1.750 0.2946 0.00855 0.00194 -0.1066 0.7287 0.1540 -1.500 0.3242 0.00828 0.00185 -0.1072 0.7235 0.2249 -1.250 0.3536 0.00802 0.00179 -0.1077 0.7186 0.3060 -1.000 0.3832 0.00775 0.00175 -0.1083 0.7135 0.3952 -0.750 0.4127 0.00748 0.00173 -0.1089 0.7076 0.4995 -0.500 0.4418 0.00728 0.00174 -0.1093 0.7021 0.5913 -0.250 0.4707 0.00714 0.00177 -0.1095 0.6957 0.6567 0.000 0.4990 0.00707 0.00178 -0.1096 0.6891 0.7069 0.250 0.5268 0.00697 0.00181 -0.1095 0.6810 0.7619 0.500 0.5531 0.00688 0.00183 -0.1090 0.6734 0.8184 0.750 0.5786 0.00681 0.00185 -0.1083 0.6655 0.8616 1.000 0.6014 0.00673 0.00183 -0.1070 0.6581 0.9103 1.250 0.6271 0.00663 0.00175 -0.1063 0.6493 1.0000 1.500 0.6561 0.00671 0.00178 -0.1066 0.6401 1.0000 1.750 0.6850 0.00680 0.00181 -0.1069 0.6304 1.0000 2.000 0.7137 0.00690 0.00186 -0.1071 0.6194 1.0000 2.250 0.7424 0.00700 0.00191 -0.1074 0.6074 1.0000 2.500 0.7708 0.00711 0.00198 -0.1076 0.5942 1.0000 2.750 0.7990 0.00725 0.00205 -0.1077 0.5790 1.0000 3.000 0.8270 0.00740 0.00216 -0.1078 0.5620 1.0000 3.250 0.8547 0.00758 0.00226 -0.1079 0.5421 1.0000 3.500 0.8819 0.00781 0.00240 -0.1080 0.5197 1.0000 3.750 0.9089 0.00808 0.00256 -0.1079 0.4942 1.0000 4.000 0.9352 0.00840 0.00277 -0.1079 0.4640 1.0000 4.250 0.9612 0.00876 0.00299 -0.1077 0.4314 1.0000 4.500 0.9867 0.00918 0.00326 -0.1075 0.3972 1.0000 4.750 1.0119 0.00962 0.00355 -0.1073 0.3640 1.0000 5.000 1.0371 0.01006 0.00387 -0.1071 0.3334 1.0000 5.250 1.0622 0.01049 0.00419 -0.1069 0.3061 1.0000 5.500 1.0871 0.01092 0.00452 -0.1067 0.2806 1.0000 5.750 1.1120 0.01135 0.00486 -0.1064 0.2573 1.0000 6.000 1.1365 0.01179 0.00523 -0.1061 0.2342 1.0000 6.500 1.1850 0.01269 0.00599 -0.1054 0.1943 1.0000 6.750 1.2085 0.01318 0.00641 -0.1049 0.1741 1.0000 7.000 1.2318 0.01368 0.00686 -0.1044 0.1557 1.0000 7.250 1.2544 0.01423 0.00733 -0.1038 0.1353 1.0000 7.500 1.2762 0.01483 0.00784 -0.1031 0.1152 1.0000 7.750 1.2981 0.01538 0.00835 -0.1025 0.0998 1.0000 8.000 1.3193 0.01599 0.00891 -0.1016 0.0846 1.0000 8.250 1.3393 0.01667 0.00953 -0.1007 0.0697 1.0000 8.500 1.3589 0.01736 0.01019 -0.0997 0.0565 1.0000 8.750 1.3773 0.01812 0.01090 -0.0985 0.0431 1.0000 9.000 1.3938 0.01899 0.01170 -0.0970 0.0300 1.0000 9.250 1.4093 0.01989 0.01254 -0.0955 0.0204 1.0000 9.500 1.4244 0.02075 0.01338 -0.0938 0.0140 1.0000 9.750 1.4381 0.02156 0.01421 -0.0919 0.0103 1.0000 10.000 1.4503 0.02240 0.01508 -0.0898 0.0080 1.0000 10.250 1.4628 0.02327 0.01601 -0.0878 0.0060 1.0000 10.500 1.4743 0.02424 0.01706 -0.0858 0.0043 1.0000 10.750 1.4843 0.02537 0.01824 -0.0838 0.0028 1.0000 11.000 1.4933 0.02662 0.01957 -0.0819 0.0019 1.0000 11.250 1.5025 0.02789 0.02095 -0.0800 0.0014 1.0000 11.500 1.5108 0.02928 0.02244 -0.0782 0.0011 1.0000 11.750 1.5165 0.03095 0.02422 -0.0763 0.0009 1.0000 12.000 1.5229 0.03261 0.02600 -0.0746 0.0008 1.0000 12.250 1.5292 0.03431 0.02784 -0.0731 0.0007 1.0000 12.500 1.5343 0.03617 0.02983 -0.0716 0.0007 1.0000 12.750 1.5384 0.03818 0.03198 -0.0702 0.0006 1.0000 13.000 1.5414 0.04034 0.03427 -0.0689 0.0006 1.0000 13.250 1.5430 0.04272 0.03682 -0.0677 0.0005 1.0000 13.500 1.5433 0.04529 0.03953 -0.0667 0.0005 1.0000 13.750 1.5425 0.04805 0.04243 -0.0657 0.0005 1.0000 14.000 1.5402 0.05108 0.04561 -0.0650 0.0005 1.0000 14.250 1.5369 0.05428 0.04896 -0.0644 0.0005 1.0000 14.500 1.5321 0.05778 0.05261 -0.0640 0.0004 1.0000 14.750 1.5261 0.06162 0.05661 -0.0639 0.0004 1.0000 15.000 1.5188 0.06578 0.06092 -0.0642 0.0004 1.0000 15.250 1.5100 0.07035 0.06565 -0.0647 0.0004 1.0000 15.500 1.5000 0.07532 0.07078 -0.0656 0.0004 1.0000 15.750 1.4889 0.08067 0.07629 -0.0670 0.0004 1.0000 16.000 1.4761 0.08649 0.08227 -0.0686 0.0004 1.0000 16.250 1.4618 0.09281 0.08876 -0.0708 0.0004 1.0000 16.500 1.4476 0.09934 0.09545 -0.0732 0.0004 1.0000 16.750 1.4312 0.10647 0.10274 -0.0761 0.0004 1.0000 17.000 1.4147 0.11382 0.11025 -0.0793 0.0004 1.0000 17.250 1.3974 0.12157 0.11816 -0.0828 0.0004 1.0000 17.500 1.3799 0.12958 0.12631 -0.0867 0.0004 1.0000