XFOIL Version 6.96 Calculated polar for: FX 74-130 WP1 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 ------ -------- --------- --------- -------- -------- -------- -10.500 -0.1369 0.08418 0.08135 -0.1178 0.7941 0.0057 -10.250 -0.1353 0.08042 0.07760 -0.1196 0.7931 0.0056 -10.000 -0.1337 0.07680 0.07398 -0.1214 0.7919 0.0054 -9.750 -0.1357 0.07247 0.06966 -0.1237 0.7905 0.0052 -9.500 -0.1431 0.06705 0.06426 -0.1267 0.7888 0.0051 -9.250 -0.1562 0.06062 0.05788 -0.1316 0.7874 0.0049 -9.000 -0.1777 0.05437 0.05162 -0.1358 0.7857 0.0048 -8.500 -0.3383 0.02323 0.01914 -0.1238 0.7804 0.0045 -8.250 -0.3241 0.02114 0.01678 -0.1226 0.7793 0.0046 -8.000 -0.3045 0.01993 0.01539 -0.1219 0.7782 0.0047 -7.750 -0.2850 0.01852 0.01374 -0.1212 0.7771 0.0049 -7.500 -0.2638 0.01729 0.01230 -0.1207 0.7760 0.0052 -7.250 -0.2417 0.01609 0.01090 -0.1201 0.7750 0.0053 -7.000 -0.2180 0.01523 0.00988 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2.750 0.8477 0.00616 0.00214 -0.1281 0.6984 0.8171 3.000 0.8748 0.00620 0.00215 -0.1282 0.6892 0.8177 3.250 0.9011 0.00626 0.00220 -0.1281 0.6775 0.8183 3.500 0.9267 0.00637 0.00226 -0.1279 0.6629 0.8188 3.750 0.9509 0.00653 0.00236 -0.1274 0.6420 0.8195 4.000 0.9727 0.00679 0.00250 -0.1264 0.6122 0.8202 4.250 0.9827 0.00750 0.00287 -0.1231 0.5367 0.8210 4.500 0.9849 0.00852 0.00346 -0.1184 0.4487 0.8219 4.750 0.9880 0.00944 0.00401 -0.1140 0.3724 0.8228 5.000 0.9908 0.01020 0.00450 -0.1095 0.3134 0.8238 5.250 0.9947 0.01087 0.00496 -0.1053 0.2678 0.8247 5.500 0.9987 0.01164 0.00552 -0.1012 0.2224 0.8257 5.750 1.0056 0.01237 0.00608 -0.0979 0.1844 0.8269 6.000 1.0141 0.01309 0.00667 -0.0949 0.1523 0.8279 6.250 1.0246 0.01380 0.00726 -0.0925 0.1242 0.8288 6.500 1.0356 0.01453 0.00787 -0.0902 0.0985 0.8296 6.750 1.0477 0.01526 0.00850 -0.0881 0.0759 0.8304 7.000 1.0610 0.01596 0.00912 -0.0863 0.0576 0.8311 7.250 1.0758 0.01661 0.00972 -0.0847 0.0453 0.8318 7.500 1.0913 0.01723 0.01031 -0.0833 0.0363 0.8325 7.750 1.1068 0.01788 0.01093 -0.0819 0.0288 0.8331 8.000 1.1232 0.01848 0.01153 -0.0807 0.0246 0.8337 8.250 1.1394 0.01911 0.01216 -0.0795 0.0208 0.8343 8.500 1.1565 0.01969 0.01277 -0.0784 0.0193 0.8349 8.750 1.1729 0.02031 0.01341 -0.0772 0.0175 0.8357 9.000 1.1884 0.02100 0.01412 -0.0760 0.0154 0.8365 9.250 1.2049 0.02164 0.01479 -0.0749 0.0143 0.8373 9.500 1.2216 0.02227 0.01547 -0.0738 0.0135 0.8382 9.750 1.2375 0.02296 0.01620 -0.0728 0.0125 0.8390 10.000 1.2530 0.02370 0.01696 -0.0716 0.0114 0.8398 10.250 1.2673 0.02453 0.01782 -0.0704 0.0101 0.8405 10.500 1.2834 0.02523 0.01856 -0.0694 0.0095 0.8413 10.750 1.2988 0.02599 0.01937 -0.0684 0.0088 0.8421 11.000 1.3136 0.02682 0.02023 -0.0673 0.0080 0.8428 11.250 1.3272 0.02773 0.02117 -0.0662 0.0072 0.8436 11.500 1.3411 0.02865 0.02213 -0.0651 0.0067 0.8444 11.750 1.3555 0.02954 0.02308 -0.0640 0.0062 0.8452 12.000 1.3690 0.03051 0.02412 -0.0630 0.0057 0.8461 12.250 1.3818 0.03156 0.02520 -0.0619 0.0051 0.8469 12.500 1.3935 0.03273 0.02641 -0.0607 0.0045 0.8476 12.750 1.4059 0.03384 0.02758 -0.0597 0.0043 0.8484 13.000 1.4180 0.03501 0.02882 -0.0587 0.0041 0.8493 13.250 1.4296 0.03623 0.03013 -0.0577 0.0038 0.8502 13.500 1.4404 0.03754 0.03150 -0.0566 0.0036 0.8512 13.750 1.4509 0.03890 0.03293 -0.0557 0.0033 0.8522 14.000 1.4605 0.04039 0.03449 -0.0547 0.0032 0.8533 14.250 1.4687 0.04205 0.03625 -0.0536 0.0029 0.8544 14.500 1.4752 0.04391 0.03821 -0.0525 0.0027 0.8556 14.750 1.4835 0.04562 0.04001 -0.0517 0.0027 0.8568 15.000 1.4914 0.04739 0.04187 -0.0509 0.0026 0.8581 15.250 1.4991 0.04923 0.04381 -0.0502 0.0026 0.8595 15.500 1.5054 0.05127 0.04596 -0.0495 0.0025 0.8609 15.750 1.5113 0.05341 0.04819 -0.0488 0.0024 0.8623 16.000 1.5166 0.05563 0.05052 -0.0483 0.0023 0.8639 16.250 1.5204 0.05807 0.05308 -0.0478 0.0022 0.8656 16.500 1.5245 0.06055 0.05566 -0.0474 0.0022 0.8673 16.750 1.5268 0.06332 0.05855 -0.0472 0.0021 0.8692 17.000 1.5282 0.06626 0.06163 -0.0470 0.0021 0.8712 17.250 1.5285 0.06944 0.06493 -0.0470 0.0020 0.8732 17.500 1.5279 0.07280 0.06841 -0.0472 0.0020 0.8753 18.000 1.5231 0.08033 0.07621 -0.0481 0.0019 0.8801 18.250 1.5190 0.08452 0.08054 -0.0489 0.0019 0.8830 18.500 1.5137 0.08902 0.08517 -0.0500 0.0018 0.8862 18.750 1.5065 0.09393 0.09024 -0.0514 0.0018 0.8894 19.000 1.4980 0.09919 0.09565 -0.0532 0.0018 0.8932