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 = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.000 -0.9762 0.10183 0.09887 -0.0472 1.0000 0.0065 -18.750 -1.0281 0.08907 0.08591 -0.0537 1.0000 0.0063 -18.500 -1.0613 0.07971 0.07639 -0.0586 1.0000 0.0063 -18.250 -1.0852 0.07219 0.06873 -0.0625 1.0000 0.0063 -18.000 -1.1023 0.06601 0.06241 -0.0656 1.0000 0.0063 -17.750 -1.1211 0.05991 0.05617 -0.0685 1.0000 0.0064 -17.500 -1.1317 0.05529 0.05144 -0.0704 1.0000 0.0065 -17.250 -1.1454 0.05053 0.04654 -0.0722 1.0000 0.0064 -17.000 -1.1528 0.04684 0.04274 -0.0731 1.0000 0.0065 -16.750 -1.1548 0.04399 0.03981 -0.0736 1.0000 0.0066 -16.500 -1.1586 0.04112 0.03683 -0.0737 1.0000 0.0067 -16.250 -1.1602 0.03866 0.03428 -0.0735 1.0000 0.0067 -16.000 -1.1640 0.03617 0.03168 -0.0728 1.0000 0.0068 -15.750 -1.1642 0.03417 0.02959 -0.0719 1.0000 0.0068 -15.500 -1.1636 0.03237 0.02770 -0.0706 1.0000 0.0069 -15.250 -1.1606 0.03088 0.02613 -0.0692 1.0000 0.0070 -15.000 -1.1574 0.02951 0.02468 -0.0675 1.0000 0.0071 -14.750 -1.1546 0.02821 0.02330 -0.0656 1.0000 0.0072 -14.500 -1.1513 0.02704 0.02206 -0.0634 1.0000 0.0072 -14.250 -1.1468 0.02604 0.02099 -0.0610 1.0000 0.0073 -14.000 -1.1443 0.02503 0.01991 -0.0583 1.0000 0.0073 -13.750 -1.1443 0.02398 0.01879 -0.0550 1.0000 0.0076 -13.500 -1.1429 0.02314 0.01788 -0.0515 1.0000 0.0077 -13.250 -1.1309 0.02222 0.01691 -0.0502 0.9994 0.0079 -13.000 -1.1099 0.02140 0.01603 -0.0503 0.9982 0.0081 -12.750 -1.0883 0.02063 0.01520 -0.0505 0.9964 0.0083 -12.500 -1.0661 0.01993 0.01444 -0.0506 0.9942 0.0085 -12.250 -1.0462 0.01926 0.01373 -0.0502 0.9918 0.0087 -12.000 -1.0251 0.01862 0.01304 -0.0499 0.9892 0.0090 -11.750 -1.0019 0.01805 0.01241 -0.0499 0.9869 0.0093 -11.500 -0.9770 0.01749 0.01180 -0.0502 0.9848 0.0095 -11.250 -0.9514 0.01691 0.01117 -0.0506 0.9832 0.0097 -11.000 -0.9312 0.01635 0.01057 -0.0498 0.9795 0.0103 -10.750 -0.9087 0.01584 0.01003 -0.0495 0.9759 0.0106 -10.500 -0.8833 0.01536 0.00953 -0.0496 0.9732 0.0112 -10.250 -0.8554 0.01488 0.00902 -0.0503 0.9712 0.0118 -10.000 -0.8253 0.01445 0.00854 -0.0514 0.9696 0.0123 -9.750 -0.8035 0.01404 0.00809 -0.0506 0.9639 0.0129 -9.500 -0.7742 0.01357 0.00762 -0.0515 0.9608 0.0138 -9.250 -0.7418 0.01313 0.00716 -0.0531 0.9582 0.0150 -9.000 -0.7076 0.01274 0.00673 -0.0550 0.9556 0.0159 -8.750 -0.6816 0.01234 0.00634 -0.0550 0.9490 0.0180 -8.500 -0.6500 0.01198 0.00595 -0.0563 0.9434 0.0197 -8.250 -0.6214 0.01160 0.00557 -0.0569 0.9368 0.0227 -8.000 -0.5949 0.01129 0.00523 -0.0570 0.9287 0.0256 -7.750 -0.5701 0.01098 0.00491 -0.0567 0.9204 0.0296 -7.500 -0.5471 0.01069 0.00461 -0.0559 0.9116 0.0349 -7.250 -0.5268 0.01042 0.00434 -0.0546 0.9024 0.0418 -7.000 -0.5057 0.01017 0.00410 -0.0534 0.8937 0.0501 -6.750 -0.4866 0.00992 0.00388 -0.0518 0.8841 0.0608 -6.500 -0.4651 0.00972 0.00368 -0.0506 0.8758 0.0687 -6.250 -0.4437 0.00955 0.00349 -0.0494 0.8667 0.0771 -6.000 -0.4226 0.00935 0.00331 -0.0481 0.8582 0.0870 -5.750 -0.4008 0.00919 0.00315 -0.0470 0.8498 0.0952 -5.500 -0.3789 0.00904 0.00299 -0.0459 0.8415 0.1048 -5.250 -0.3572 0.00889 0.00284 -0.0447 0.8332 0.1147 -5.000 -0.3352 0.00872 0.00270 -0.0436 0.8253 0.1257 -4.500 -0.2919 0.00839 0.00242 -0.0412 0.8091 0.1562 -4.250 -0.2702 0.00824 0.00229 -0.0400 0.8010 0.1729 -4.000 -0.2480 0.00808 0.00218 -0.0389 0.7927 0.1913 -3.750 -0.2265 0.00791 0.00206 -0.0376 0.7846 0.2124 -3.500 -0.2049 0.00772 0.00194 -0.0364 0.7764 0.2394 -3.250 -0.1840 0.00753 0.00183 -0.0351 0.7684 0.2706 -3.000 -0.1624 0.00735 0.00173 -0.0339 0.7600 0.3002 -2.750 -0.1421 0.00714 0.00163 -0.0324 0.7514 0.3388 -2.500 -0.1218 0.00693 0.00154 -0.0309 0.7423 0.3794 -2.250 -0.1007 0.00676 0.00146 -0.0296 0.7334 0.4145 -2.000 -0.0799 0.00662 0.00139 -0.0281 0.7239 0.4488 -1.750 -0.0588 0.00647 0.00134 -0.0267 0.7140 0.4862 -1.500 -0.0369 0.00637 0.00130 -0.0255 0.7044 0.5120 -1.250 -0.0150 0.00631 0.00126 -0.0243 0.6939 0.5353 -1.000 0.0069 0.00622 0.00123 -0.0230 0.6830 0.5616 -0.750 0.0292 0.00618 0.00121 -0.0219 0.6725 0.5823 -0.500 0.0503 0.00612 0.00119 -0.0204 0.6607 0.6068 -0.250 0.0701 0.00603 0.00118 -0.0187 0.6486 0.6396 0.000 0.0890 0.00594 0.00118 -0.0168 0.6360 0.6766 0.250 0.1090 0.00589 0.00119 -0.0150 0.6234 0.7060 0.500 0.1296 0.00587 0.00120 -0.0135 0.6103 0.7279 0.750 0.1509 0.00587 0.00123 -0.0120 0.5986 0.7498 1.000 0.1731 0.00587 0.00126 -0.0108 0.5882 0.7697 1.250 0.1957 0.00588 0.00129 -0.0097 0.5774 0.7858 1.500 0.2186 0.00591 0.00133 -0.0086 0.5678 0.7997 1.750 0.2423 0.00594 0.00137 -0.0077 0.5580 0.8118 2.000 0.2659 0.00598 0.00142 -0.0068 0.5475 0.8228 2.250 0.2890 0.00604 0.00147 -0.0058 0.5355 0.8330 2.500 0.3117 0.00612 0.00154 -0.0047 0.5207 0.8436 2.750 0.3340 0.00622 0.00161 -0.0036 0.5012 0.8530 3.250 0.3790 0.00644 0.00177 -0.0014 0.4648 0.8715 3.750 0.4235 0.00673 0.00197 0.0009 0.4245 0.8889 4.000 0.4450 0.00693 0.00210 0.0021 0.3998 0.8971 4.250 0.4665 0.00713 0.00223 0.0033 0.3745 0.9058 4.500 0.4888 0.00738 0.00240 0.0043 0.3473 0.9133 4.750 0.5097 0.00763 0.00257 0.0056 0.3222 0.9217 5.000 0.5335 0.00789 0.00275 0.0062 0.2973 0.9281 5.250 0.5573 0.00817 0.00295 0.0068 0.2736 0.9353 5.500 0.5809 0.00847 0.00317 0.0074 0.2491 0.9417 5.750 0.6089 0.00887 0.00344 0.0069 0.2186 0.9465 6.000 0.6298 0.00928 0.00372 0.0079 0.1870 0.9535 6.250 0.6588 0.00973 0.00403 0.0071 0.1583 0.9571 6.500 0.6905 0.01016 0.00436 0.0057 0.1349 0.9599 6.750 0.7196 0.01054 0.00468 0.0050 0.1186 0.9637 7.000 0.7413 0.01089 0.00496 0.0059 0.1045 0.9696 7.250 0.7716 0.01131 0.00531 0.0048 0.0895 0.9713 7.500 0.7994 0.01172 0.00565 0.0043 0.0759 0.9734 7.750 0.8248 0.01215 0.00602 0.0042 0.0624 0.9760 8.000 0.8479 0.01257 0.00639 0.0046 0.0521 0.9794 8.250 0.8690 0.01299 0.00677 0.0054 0.0429 0.9830 8.500 0.8961 0.01344 0.00718 0.0049 0.0357 0.9845 8.750 0.9221 0.01388 0.00760 0.0046 0.0304 0.9863 9.000 0.9476 0.01430 0.00801 0.0044 0.0264 0.9884 9.250 0.9713 0.01476 0.00846 0.0045 0.0227 0.9908 9.500 0.9938 0.01522 0.00892 0.0048 0.0204 0.9931 9.750 1.0179 0.01568 0.00939 0.0048 0.0185 0.9951 10.000 1.0428 0.01616 0.00988 0.0045 0.0168 0.9970 10.250 1.0670 0.01670 0.01043 0.0043 0.0153 0.9985 10.500 1.0918 0.01718 0.01095 0.0040 0.0145 0.9996 10.750 1.1067 0.01768 0.01146 0.0057 0.0134 1.0000 11.000 1.1132 0.01818 0.01198 0.0090 0.0125 1.0000 11.250 1.1206 0.01871 0.01255 0.0121 0.0121 1.0000 11.500 1.1303 0.01921 0.01308 0.0147 0.0117 1.0000 11.750 1.1396 0.01979 0.01370 0.0173 0.0113 1.0000 12.000 1.1493 0.02040 0.01434 0.0197 0.0109 1.0000 12.250 1.1584 0.02110 0.01508 0.0220 0.0105 1.0000 12.500 1.1677 0.02183 0.01585 0.0242 0.0101 1.0000 12.750 1.1759 0.02269 0.01674 0.0264 0.0096 1.0000 13.000 1.1848 0.02355 0.01765 0.0284 0.0094 1.0000 13.250 1.1940 0.02444 0.01859 0.0302 0.0092 1.0000 13.500 1.2039 0.02533 0.01953 0.0318 0.0091 1.0000 13.750 1.2131 0.02632 0.02058 0.0334 0.0088 1.0000 14.000 1.2213 0.02742 0.02174 0.0350 0.0085 1.0000 14.250 1.2301 0.02852 0.02290 0.0363 0.0082 1.0000 14.500 1.2373 0.02979 0.02422 0.0377 0.0080 1.0000 14.750 1.2449 0.03108 0.02555 0.0388 0.0077 1.0000 15.000 1.2504 0.03258 0.02712 0.0400 0.0076 1.0000 15.250 1.2550 0.03422 0.02881 0.0411 0.0074 1.0000 15.500 1.2589 0.03599 0.03066 0.0420 0.0071 1.0000 15.750 1.2617 0.03794 0.03268 0.0429 0.0071 1.0000 16.000 1.2674 0.03968 0.03451 0.0434 0.0069 1.0000 16.250 1.2714 0.04164 0.03654 0.0439 0.0069 1.0000 16.500 1.2730 0.04392 0.03891 0.0442 0.0068 1.0000 16.750 1.2755 0.04618 0.04124 0.0444 0.0067 1.0000 17.000 1.2754 0.04882 0.04397 0.0445 0.0066 1.0000 17.250 1.2742 0.05164 0.04688 0.0443 0.0065 1.0000 17.500 1.2734 0.05449 0.04982 0.0440 0.0064 1.0000 17.750 1.2709 0.05767 0.05309 0.0435 0.0063 1.0000 18.000 1.2671 0.06109 0.05660 0.0429 0.0063 1.0000 18.250 1.2635 0.06454 0.06015 0.0420 0.0061 1.0000 18.500 1.2591 0.06820 0.06390 0.0410 0.0061 1.0000 18.750 1.2493 0.07273 0.06854 0.0396 0.0060 1.0000 19.000 1.2396 0.07736 0.07328 0.0380 0.0060 1.0000 19.250 1.2273 0.08249 0.07853 0.0361 0.0060 1.0000