XFOIL Version 6.96 Calculated polar for: HAWKER TEMPEST 37.5% SEMISPAN AIRFOIL 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.250 -0.8352 0.13075 0.12841 -0.0333 1.0000 0.0090 -19.000 -0.8560 0.12235 0.11991 -0.0377 1.0000 0.0091 -18.750 -0.8894 0.11203 0.10944 -0.0429 1.0000 0.0090 -18.500 -0.9139 0.10358 0.10087 -0.0473 1.0000 0.0090 -18.250 -0.9343 0.09604 0.09321 -0.0512 1.0000 0.0089 -18.000 -0.9494 0.08942 0.08649 -0.0547 1.0000 0.0091 -17.750 -0.9749 0.08151 0.07843 -0.0587 1.0000 0.0089 -17.500 -0.9908 0.07521 0.07201 -0.0620 1.0000 0.0090 -17.250 -1.0067 0.06915 0.06582 -0.0650 1.0000 0.0090 -17.000 -1.0199 0.06374 0.06029 -0.0676 1.0000 0.0091 -16.750 -1.0298 0.05907 0.05551 -0.0697 1.0000 0.0091 -16.500 -1.0398 0.05465 0.05097 -0.0714 1.0000 0.0092 -16.250 -1.0456 0.05097 0.04717 -0.0726 1.0000 0.0093 -16.000 -1.0563 0.04697 0.04304 -0.0734 1.0000 0.0093 -15.750 -1.0639 0.04360 0.03955 -0.0738 1.0000 0.0093 -15.500 -1.0660 0.04099 0.03684 -0.0737 1.0000 0.0094 -15.250 -1.0638 0.03896 0.03472 -0.0733 1.0000 0.0095 -15.000 -1.0609 0.03715 0.03282 -0.0727 1.0000 0.0097 -14.750 -1.0667 0.03471 0.03027 -0.0713 1.0000 0.0096 -14.500 -1.0600 0.03348 0.02898 -0.0703 1.0000 0.0097 -14.250 -1.0772 0.03052 0.02587 -0.0674 1.0000 0.0100 -14.000 -1.0781 0.02900 0.02426 -0.0651 1.0000 0.0100 -13.750 -1.0866 0.02717 0.02234 -0.0617 1.0000 0.0104 -13.500 -1.0868 0.02601 0.02112 -0.0587 1.0000 0.0105 -13.250 -1.0872 0.02499 0.02005 -0.0553 1.0000 0.0107 -13.000 -1.0863 0.02418 0.01918 -0.0518 1.0000 0.0108 -12.750 -1.0868 0.02344 0.01838 -0.0479 1.0000 0.0109 -12.500 -1.0882 0.02281 0.01769 -0.0436 1.0000 0.0111 -12.250 -1.0914 0.02224 0.01707 -0.0388 1.0000 0.0112 -12.000 -1.0695 0.02139 0.01616 -0.0390 0.9987 0.0115 -11.750 -1.0450 0.02064 0.01533 -0.0396 0.9970 0.0120 -11.500 -1.0190 0.01998 0.01460 -0.0403 0.9953 0.0123 -11.250 -0.9933 0.01923 0.01378 -0.0410 0.9937 0.0124 -11.000 -0.9763 0.01818 0.01264 -0.0401 0.9904 0.0131 -10.750 -0.9521 0.01745 0.01187 -0.0403 0.9878 0.0135 -10.500 -0.9244 0.01688 0.01126 -0.0411 0.9859 0.0140 -10.250 -0.8955 0.01630 0.01065 -0.0420 0.9844 0.0148 -10.000 -0.8646 0.01582 0.01012 -0.0433 0.9833 0.0154 -9.750 -0.8417 0.01531 0.00955 -0.0428 0.9797 0.0161 -9.500 -0.8182 0.01462 0.00883 -0.0426 0.9761 0.0173 -9.250 -0.7888 0.01412 0.00832 -0.0434 0.9740 0.0186 -9.000 -0.7573 0.01366 0.00782 -0.0447 0.9725 0.0197 -8.750 -0.7261 0.01303 0.00719 -0.0459 0.9711 0.0223 -8.500 -0.6920 0.01259 0.00673 -0.0477 0.9699 0.0245 -8.250 -0.6700 0.01208 0.00623 -0.0469 0.9644 0.0288 -8.000 -0.6399 0.01158 0.00576 -0.0478 0.9612 0.0350 -7.750 -0.6088 0.01109 0.00531 -0.0489 0.9582 0.0452 -7.500 -0.5757 0.01058 0.00490 -0.0506 0.9558 0.0596 -7.250 -0.5545 0.01028 0.00464 -0.0494 0.9486 0.0707 -7.000 -0.5259 0.00997 0.00436 -0.0499 0.9437 0.0818 -6.750 -0.4956 0.00968 0.00409 -0.0507 0.9392 0.0934 -6.500 -0.4749 0.00947 0.00390 -0.0494 0.9312 0.1020 -6.250 -0.4462 0.00921 0.00366 -0.0498 0.9257 0.1128 -6.000 -0.4255 0.00903 0.00349 -0.0484 0.9175 0.1224 -5.750 -0.3994 0.00882 0.00328 -0.0482 0.9111 0.1335 -5.500 -0.3785 0.00862 0.00311 -0.0468 0.9029 0.1475 -5.250 -0.3549 0.00839 0.00292 -0.0461 0.8957 0.1651 -5.000 -0.3348 0.00815 0.00276 -0.0446 0.8876 0.1878 -4.750 -0.3135 0.00786 0.00257 -0.0434 0.8800 0.2216 -4.500 -0.2953 0.00755 0.00241 -0.0415 0.8716 0.2626 -4.250 -0.2751 0.00724 0.00223 -0.0401 0.8639 0.3071 -4.000 -0.2572 0.00694 0.00209 -0.0381 0.8554 0.3535 -3.750 -0.2375 0.00666 0.00195 -0.0365 0.8477 0.4021 -3.500 -0.2192 0.00640 0.00185 -0.0346 0.8394 0.4491 -3.250 -0.1991 0.00620 0.00174 -0.0330 0.8319 0.4922 -3.000 -0.1786 0.00604 0.00168 -0.0314 0.8238 0.5245 -2.750 -0.1569 0.00592 0.00160 -0.0301 0.8161 0.5540 -2.500 -0.1355 0.00580 0.00155 -0.0287 0.8078 0.5813 -2.250 -0.1135 0.00571 0.00149 -0.0275 0.8000 0.6043 -2.000 -0.0912 0.00563 0.00145 -0.0263 0.7914 0.6259 -1.750 -0.0696 0.00554 0.00141 -0.0249 0.7832 0.6499 -1.500 -0.0474 0.00548 0.00137 -0.0236 0.7744 0.6711 -1.250 -0.0247 0.00542 0.00135 -0.0225 0.7657 0.6911 -1.000 -0.0031 0.00537 0.00133 -0.0211 0.7564 0.7130 -0.750 0.0195 0.00532 0.00132 -0.0199 0.7470 0.7323 -0.500 0.0420 0.00530 0.00131 -0.0187 0.7372 0.7517 -0.250 0.0638 0.00527 0.00132 -0.0173 0.7266 0.7730 0.000 0.0857 0.00525 0.00134 -0.0159 0.7156 0.7951 0.250 0.1082 0.00526 0.00136 -0.0146 0.7044 0.8122 0.500 0.1313 0.00529 0.00138 -0.0135 0.6924 0.8255 0.750 0.1551 0.00531 0.00141 -0.0126 0.6808 0.8383 1.000 0.1790 0.00534 0.00145 -0.0117 0.6700 0.8505 1.250 0.2020 0.00540 0.00148 -0.0106 0.6588 0.8616 1.500 0.2275 0.00545 0.00153 -0.0100 0.6480 0.8705 1.750 0.2515 0.00550 0.00157 -0.0092 0.6375 0.8796 2.000 0.2772 0.00557 0.00164 -0.0087 0.6265 0.8875 2.250 0.3005 0.00565 0.00169 -0.0077 0.6147 0.8956 2.500 0.3261 0.00574 0.00177 -0.0072 0.6014 0.9027 2.750 0.3487 0.00583 0.00183 -0.0061 0.5872 0.9105 3.000 0.3764 0.00594 0.00193 -0.0061 0.5741 0.9163 3.250 0.3968 0.00603 0.00199 -0.0044 0.5621 0.9242 3.500 0.4274 0.00616 0.00211 -0.0051 0.5493 0.9285 3.750 0.4533 0.00630 0.00223 -0.0047 0.5365 0.9342 4.000 0.4754 0.00642 0.00232 -0.0035 0.5221 0.9408 4.250 0.5069 0.00660 0.00247 -0.0045 0.5049 0.9441 4.500 0.5356 0.00679 0.00262 -0.0048 0.4861 0.9481 4.750 0.5547 0.00695 0.00273 -0.0029 0.4679 0.9550 5.000 0.5868 0.00724 0.00293 -0.0041 0.4388 0.9570 5.250 0.6183 0.00759 0.00316 -0.0052 0.4057 0.9591 5.500 0.6486 0.00804 0.00343 -0.0062 0.3630 0.9612 5.750 0.6747 0.00855 0.00375 -0.0063 0.3184 0.9644 6.000 0.6931 0.00899 0.00402 -0.0046 0.2814 0.9699 6.250 0.7245 0.00949 0.00436 -0.0059 0.2459 0.9710 6.500 0.7554 0.00999 0.00471 -0.0071 0.2121 0.9724 6.750 0.7854 0.01048 0.00506 -0.0081 0.1818 0.9742 7.000 0.8130 0.01097 0.00542 -0.0086 0.1542 0.9769 7.250 0.8312 0.01138 0.00575 -0.0069 0.1358 0.9826 7.500 0.8624 0.01184 0.00611 -0.0083 0.1154 0.9837 7.750 0.8930 0.01226 0.00644 -0.0095 0.0987 0.9850 8.000 0.9220 0.01269 0.00680 -0.0103 0.0831 0.9868 8.250 0.9484 0.01319 0.00720 -0.0107 0.0670 0.9892 8.500 0.9729 0.01368 0.00763 -0.0107 0.0535 0.9920 8.750 0.9971 0.01420 0.00808 -0.0107 0.0420 0.9943 9.000 1.0245 0.01472 0.00855 -0.0114 0.0336 0.9960 9.250 1.0512 0.01522 0.00904 -0.0120 0.0281 0.9978 9.500 1.0766 0.01582 0.00961 -0.0124 0.0241 0.9995 9.750 1.0897 0.01616 0.00999 -0.0101 0.0225 1.0000 10.000 1.0911 0.01653 0.01037 -0.0054 0.0211 1.0000 10.250 1.0901 0.01707 0.01094 -0.0005 0.0195 1.0000 10.500 1.0963 0.01744 0.01134 0.0031 0.0189 1.0000 10.750 1.1031 0.01785 0.01179 0.0065 0.0180 1.0000 11.000 1.1093 0.01838 0.01234 0.0099 0.0170 1.0000 11.250 1.1141 0.01905 0.01304 0.0133 0.0163 1.0000 11.500 1.1170 0.01990 0.01394 0.0169 0.0154 1.0000 11.750 1.1265 0.02050 0.01459 0.0194 0.0151 1.0000 12.000 1.1365 0.02113 0.01527 0.0216 0.0146 1.0000 12.250 1.1445 0.02192 0.01611 0.0241 0.0141 1.0000 12.500 1.1537 0.02269 0.01692 0.0262 0.0137 1.0000 12.750 1.1616 0.02359 0.01786 0.0283 0.0132 1.0000 13.000 1.1670 0.02471 0.01902 0.0305 0.0126 1.0000 13.250 1.1670 0.02626 0.02065 0.0331 0.0123 1.0000 13.500 1.1739 0.02742 0.02188 0.0348 0.0120 1.0000 13.750 1.1833 0.02847 0.02300 0.0362 0.0117 1.0000 14.000 1.1896 0.02979 0.02438 0.0377 0.0115 1.0000 14.250 1.1982 0.03099 0.02564 0.0389 0.0111 1.0000 14.500 1.2022 0.03260 0.02733 0.0402 0.0110 1.0000 14.750 1.2099 0.03397 0.02875 0.0412 0.0105 1.0000 15.000 1.2132 0.03578 0.03063 0.0422 0.0104 1.0000 15.250 1.2161 0.03770 0.03261 0.0430 0.0102 1.0000 15.500 1.2175 0.03985 0.03483 0.0437 0.0100 1.0000 15.750 1.2166 0.04230 0.03736 0.0443 0.0099 1.0000 16.000 1.1991 0.04656 0.04175 0.0449 0.0095 1.0000 16.250 1.1993 0.04917 0.04445 0.0449 0.0094 1.0000 16.500 1.1987 0.05195 0.04732 0.0448 0.0093 1.0000 16.750 1.2001 0.05459 0.05006 0.0446 0.0092 1.0000 17.000 1.1971 0.05784 0.05340 0.0441 0.0092 1.0000 17.250 1.1905 0.06163 0.05730 0.0434 0.0091 1.0000 17.500 1.1898 0.06477 0.06053 0.0426 0.0090 1.0000 17.750 1.1834 0.06876 0.06463 0.0416 0.0089 1.0000 18.000 1.1781 0.07271 0.06867 0.0404 0.0088 1.0000 18.250 1.1710 0.07703 0.07309 0.0389 0.0086 1.0000 18.500 1.1664 0.08108 0.07723 0.0374 0.0085 1.0000 18.750 1.1527 0.08650 0.08278 0.0354 0.0085 1.0000 19.000 1.1417 0.09168 0.08806 0.0334 0.0085 1.0000