WORTMANN FX 73-170 (fx73170-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 73-170 (fx73170-il) Reynolds number: 100,000 Max Cl/Cd: 24.51 at α=11.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx73170-il-100000-n5.txt Download as CSV file: xf-fx73170-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 73-170
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.500 0.0015 0.11150 0.10582 -0.1174 0.8300 0.0546
-13.250 0.0007 0.10689 0.10117 -0.1191 0.8285 0.0390
-13.000 -0.0968 0.11543 0.10929 -0.1250 0.8425 0.0330
-12.750 -0.0823 0.11312 0.10694 -0.1255 0.8403 0.0318
-12.500 -0.0785 0.10893 0.10276 -0.1278 0.8383 0.0317
-12.250 -0.0725 0.10523 0.09905 -0.1298 0.8363 0.0309
-12.000 -0.0690 0.10113 0.09495 -0.1323 0.8345 0.0310
-11.750 -0.0665 0.09700 0.09082 -0.1345 0.8327 0.0306
-11.500 -0.0887 0.08667 0.08055 -0.1398 0.8304 0.0265
-11.250 -0.0701 0.08834 0.08225 -0.1385 0.8277 0.0305
-11.000 -0.1047 0.07453 0.06846 -0.1465 0.8252 0.0263
-10.750 -0.1317 0.06711 0.06095 -0.1515 0.8224 0.0265
-10.500 -0.1472 0.06268 0.05644 -0.1535 0.8199 0.0263
-10.250 -0.1661 0.05884 0.05245 -0.1549 0.8175 0.0264
-10.000 -0.1850 0.05574 0.04927 -0.1544 0.8144 0.0263
-9.750 -0.1967 0.05350 0.04697 -0.1533 0.8110 0.0261
-9.500 -0.2241 0.05119 0.04444 -0.1504 0.8072 0.0263
-9.250 -0.2356 0.04925 0.04228 -0.1482 0.8042 0.0264
-9.000 -0.2425 0.04698 0.03970 -0.1462 0.8020 0.0265
-8.750 -0.2470 0.04513 0.03763 -0.1437 0.7989 0.0265
-8.500 -0.2469 0.04338 0.03564 -0.1415 0.7959 0.0265
-8.250 -0.2436 0.04145 0.03337 -0.1394 0.7930 0.0266
-8.000 -0.2346 0.03945 0.03111 -0.1379 0.7905 0.0269
-7.750 -0.2207 0.03767 0.02910 -0.1369 0.7885 0.0273
-7.500 -0.2034 0.03612 0.02733 -0.1361 0.7868 0.0278
-7.250 -0.1897 0.03500 0.02604 -0.1346 0.7843 0.0283
-7.000 -0.1780 0.03411 0.02501 -0.1326 0.7812 0.0289
-6.750 -0.1627 0.03328 0.02405 -0.1311 0.7786 0.0300
-6.500 -0.1445 0.03247 0.02302 -0.1299 0.7762 0.0322
-6.250 -0.1236 0.03155 0.02191 -0.1289 0.7742 0.0336
-6.000 -0.1024 0.03058 0.02096 -0.1282 0.7725 0.0353
-5.750 -0.0799 0.02977 0.02009 -0.1275 0.7710 0.0370
-5.500 -0.0706 0.02958 0.01986 -0.1248 0.7678 0.0392
-5.250 -0.0637 0.02965 0.01986 -0.1219 0.7640 0.0412
-5.000 -0.0512 0.02927 0.01955 -0.1200 0.7612 0.0442
-4.750 -0.0327 0.02883 0.01906 -0.1188 0.7589 0.0484
-4.500 -0.0125 0.02826 0.01844 -0.1179 0.7571 0.0541
-4.250 0.0101 0.02780 0.01794 -0.1174 0.7556 0.0644
-4.000 0.0137 0.02805 0.01823 -0.1142 0.7517 0.0761
-3.750 0.0139 0.02835 0.01866 -0.1106 0.7467 0.0931
-3.500 0.0289 0.02767 0.01843 -0.1095 0.7440 0.1729
-3.250 0.0393 0.02628 0.01858 -0.1078 0.7419 0.4638
-3.000 0.0606 0.02729 0.01982 -0.1051 0.7405 0.6028
-2.750 0.0859 0.02807 0.02041 -0.1039 0.7394 0.6397
-2.500 0.0594 0.02959 0.02195 -0.0965 0.7303 0.6475
-2.250 0.0729 0.03063 0.02297 -0.0926 0.7276 0.6759
-2.000 0.0883 0.03146 0.02378 -0.0888 0.7259 0.7000
-1.750 0.1091 0.03188 0.02410 -0.0867 0.7246 0.7156
-1.500 0.0899 0.03327 0.02551 -0.0806 0.7166 0.7225
-1.250 0.1086 0.03358 0.02568 -0.0797 0.7136 0.7286
-1.000 0.1309 0.03379 0.02577 -0.0790 0.7117 0.7326
-0.750 0.1571 0.03391 0.02574 -0.0792 0.7102 0.7369
-0.500 0.1876 0.03392 0.02559 -0.0802 0.7090 0.7411
-0.250 0.1776 0.03524 0.02691 -0.0757 0.7015 0.7444
0.000 0.1961 0.03564 0.02723 -0.0749 0.6986 0.7471
0.250 0.2209 0.03584 0.02732 -0.0750 0.6966 0.7496
0.500 0.2491 0.03592 0.02730 -0.0755 0.6950 0.7522
0.750 0.2796 0.03596 0.02723 -0.0764 0.6937 0.7545
1.250 0.2940 0.03771 0.02889 -0.0726 0.6830 0.7591
1.500 0.3204 0.03788 0.02900 -0.0728 0.6810 0.7608
1.750 0.3481 0.03803 0.02911 -0.0732 0.6795 0.7626
2.000 0.3781 0.03813 0.02914 -0.0739 0.6783 0.7643
2.250 0.3689 0.03967 0.03069 -0.0702 0.6693 0.7664
2.500 0.3944 0.03993 0.03092 -0.0704 0.6669 0.7682
2.750 0.4233 0.04008 0.03102 -0.0710 0.6651 0.7702
3.000 0.4541 0.04016 0.03106 -0.0719 0.6637 0.7721
3.250 0.4487 0.04165 0.03257 -0.0687 0.6546 0.7740
3.500 0.4744 0.04190 0.03282 -0.0689 0.6520 0.7754
3.750 0.5029 0.04202 0.03295 -0.0694 0.6502 0.7769
4.000 0.5342 0.04204 0.03296 -0.0701 0.6488 0.7784
4.500 0.5575 0.04377 0.03475 -0.0677 0.6365 0.7827
4.750 0.5888 0.04380 0.03479 -0.0685 0.6348 0.7847
5.250 0.6174 0.04549 0.03654 -0.0670 0.6226 0.7886
5.500 0.6488 0.04546 0.03656 -0.0678 0.6205 0.7902
5.750 0.6820 0.04533 0.03650 -0.0687 0.6190 0.7920
6.000 0.6808 0.04697 0.03819 -0.0666 0.6081 0.7939
6.250 0.7123 0.04692 0.03820 -0.0674 0.6059 0.7960
6.500 0.7464 0.04666 0.03803 -0.0683 0.6042 0.7986
6.750 0.7471 0.04831 0.03974 -0.0665 0.5930 0.8012
7.000 0.7800 0.04805 0.03956 -0.0674 0.5906 0.8039
7.500 0.8161 0.04931 0.04103 -0.0666 0.5771 0.8086
7.750 0.8507 0.04881 0.04065 -0.0675 0.5750 0.8112
8.000 0.8558 0.05026 0.04220 -0.0662 0.5634 0.8140
8.250 0.8909 0.04960 0.04168 -0.0670 0.5607 0.8171
8.500 0.8987 0.05089 0.04308 -0.0659 0.5491 0.8201
8.750 0.9340 0.05005 0.04239 -0.0666 0.5460 0.8235
9.250 0.9792 0.05018 0.04284 -0.0662 0.5309 0.8321
9.750 1.0093 0.05133 0.04430 -0.0648 0.5072 0.8417
10.000 1.0450 0.04985 0.04301 -0.0651 0.5001 0.8483
10.250 1.0628 0.05025 0.04358 -0.0646 0.4858 0.8550
10.500 1.0846 0.05020 0.04367 -0.0643 0.4679 0.8639
10.750 1.1068 0.05023 0.04385 -0.0641 0.4451 0.8766
11.000 1.1412 0.04895 0.04265 -0.0645 0.4150 0.9069
11.250 1.1599 0.04783 0.04136 -0.0620 0.3816 1.0000
11.500 1.1783 0.04807 0.04136 -0.0611 0.3407 1.0000
11.750 1.1859 0.04947 0.04249 -0.0598 0.2993 1.0000
12.000 1.1889 0.05149 0.04431 -0.0585 0.2619 1.0000
12.250 1.1890 0.05388 0.04647 -0.0572 0.2256 1.0000
12.500 1.1881 0.05648 0.04886 -0.0560 0.1920 1.0000
12.750 1.1880 0.05909 0.05130 -0.0550 0.1627 1.0000
13.000 1.1888 0.06169 0.05376 -0.0542 0.1381 1.0000
13.250 1.1902 0.06430 0.05625 -0.0534 0.1174 1.0000
13.500 1.1923 0.06688 0.05876 -0.0527 0.1016 1.0000
13.750 1.1951 0.06943 0.06127 -0.0521 0.0899 1.0000
14.000 1.1970 0.07211 0.06392 -0.0516 0.0810 1.0000
14.250 1.2019 0.07451 0.06640 -0.0511 0.0741 1.0000
14.500 1.2038 0.07725 0.06912 -0.0507 0.0683 1.0000
14.750 1.2097 0.07958 0.07156 -0.0503 0.0634 1.0000
15.000 1.2123 0.08226 0.07425 -0.0501 0.0592 1.0000
15.250 1.2173 0.08468 0.07675 -0.0497 0.0556 1.0000
15.500 1.2232 0.08704 0.07922 -0.0495 0.0520 1.0000
15.750 1.2269 0.08968 0.08191 -0.0495 0.0491 1.0000
16.000 1.2319 0.09211 0.08437 -0.0493 0.0464 1.0000
16.250 1.2387 0.09436 0.08680 -0.0491 0.0436 1.0000
16.500 1.2432 0.09696 0.08950 -0.0492 0.0412 1.0000
16.750 1.2471 0.09957 0.09213 -0.0493 0.0392 1.0000
17.000 1.2530 0.10194 0.09461 -0.0492 0.0372 1.0000
17.250 1.2582 0.10455 0.09742 -0.0494 0.0352 1.0000
17.500 1.2624 0.10729 0.10029 -0.0497 0.0336 1.0000
17.750 1.2651 0.11019 0.10327 -0.0502 0.0321 1.0000
18.000 1.2692 0.11279 0.10587 -0.0507 0.0307 1.0000
18.250 1.2692 0.11635 0.10967 -0.0515 0.0294 1.0000
18.500 1.2688 0.11998 0.11358 -0.0524 0.0283 1.0000
18.750 1.2673 0.12382 0.11763 -0.0536 0.0272 1.0000
19.000 1.2657 0.12770 0.12167 -0.0549 0.0264 1.0000
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