WORTMANN FX 73-170 (fx73170-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 73-170 (fx73170-il) Reynolds number: 500,000 Max Cl/Cd: 112.73 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx73170-il-500000-n5.txt Download as CSV file: xf-fx73170-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.250 -0.3238 0.04827 0.04406 -0.1477 0.7464 0.0082
-12.000 -0.3529 0.04184 0.03734 -0.1511 0.7448 0.0081
-11.750 -0.3731 0.03714 0.03235 -0.1525 0.7432 0.0081
-11.500 -0.3906 0.03281 0.02764 -0.1526 0.7416 0.0079
-11.250 -0.3819 0.03161 0.02637 -0.1528 0.7401 0.0083
-11.000 -0.3832 0.02910 0.02360 -0.1521 0.7386 0.0081
-10.750 -0.3766 0.02771 0.02210 -0.1514 0.7371 0.0084
-10.500 -0.3725 0.02597 0.02017 -0.1501 0.7355 0.0085
-10.250 -0.3648 0.02483 0.01892 -0.1488 0.7337 0.0086
-10.000 -0.3588 0.02358 0.01750 -0.1468 0.7318 0.0088
-9.750 -0.3469 0.02256 0.01634 -0.1454 0.7301 0.0088
-9.500 -0.3325 0.02152 0.01513 -0.1442 0.7287 0.0093
-9.250 -0.3156 0.02072 0.01421 -0.1433 0.7274 0.0094
-9.000 -0.2976 0.01996 0.01330 -0.1424 0.7261 0.0097
-8.750 -0.2793 0.01917 0.01239 -0.1416 0.7248 0.0098
-8.500 -0.2598 0.01853 0.01163 -0.1409 0.7235 0.0099
-8.250 -0.2408 0.01785 0.01089 -0.1400 0.7222 0.0101
-8.000 -0.2228 0.01711 0.01013 -0.1391 0.7206 0.0105
-7.750 -0.2019 0.01663 0.00962 -0.1385 0.7191 0.0109
-7.500 -0.1805 0.01617 0.00913 -0.1379 0.7175 0.0113
-7.250 -0.1586 0.01573 0.00864 -0.1374 0.7161 0.0116
-7.000 -0.1363 0.01530 0.00816 -0.1370 0.7148 0.0121
-6.750 -0.1134 0.01491 0.00772 -0.1366 0.7134 0.0127
-6.500 -0.0904 0.01450 0.00725 -0.1362 0.7122 0.0134
-6.250 -0.0671 0.01411 0.00684 -0.1360 0.7110 0.0140
-6.000 -0.0428 0.01378 0.00647 -0.1358 0.7097 0.0149
-5.750 -0.0180 0.01348 0.00611 -0.1357 0.7085 0.0158
-5.500 0.0066 0.01318 0.00576 -0.1355 0.7071 0.0170
-5.250 0.0309 0.01285 0.00544 -0.1353 0.7057 0.0182
-5.000 0.0562 0.01260 0.00518 -0.1352 0.7043 0.0198
-4.750 0.0817 0.01236 0.00493 -0.1351 0.7030 0.0224
-4.500 0.1074 0.01213 0.00469 -0.1351 0.7016 0.0265
-4.250 0.1333 0.01189 0.00447 -0.1351 0.7002 0.0325
-4.000 0.1592 0.01164 0.00427 -0.1351 0.6989 0.0445
-3.750 0.1850 0.01138 0.00407 -0.1351 0.6976 0.0660
-3.500 0.2104 0.01106 0.00387 -0.1352 0.6962 0.1033
-3.250 0.2354 0.01064 0.00365 -0.1352 0.6949 0.1678
-3.000 0.2573 0.00988 0.00335 -0.1351 0.6937 0.3084
-2.750 0.2766 0.00903 0.00308 -0.1343 0.6925 0.4800
-2.500 0.3005 0.00897 0.00333 -0.1337 0.6912 0.5820
-2.250 0.3280 0.00906 0.00341 -0.1337 0.6899 0.6007
-2.000 0.3555 0.00920 0.00352 -0.1337 0.6884 0.6169
-1.750 0.3831 0.00938 0.00368 -0.1336 0.6868 0.6312
-1.500 0.4107 0.00951 0.00382 -0.1336 0.6853 0.6384
-1.250 0.4386 0.00959 0.00386 -0.1338 0.6838 0.6438
-1.000 0.4665 0.00964 0.00384 -0.1339 0.6826 0.6473
-0.750 0.4944 0.00966 0.00385 -0.1341 0.6814 0.6494
-0.500 0.5226 0.00969 0.00386 -0.1344 0.6802 0.6511
-0.250 0.5510 0.00972 0.00385 -0.1347 0.6790 0.6525
0.000 0.5792 0.00976 0.00385 -0.1350 0.6777 0.6538
0.250 0.6057 0.00978 0.00388 -0.1350 0.6762 0.6549
0.500 0.6325 0.00982 0.00392 -0.1350 0.6746 0.6563
0.750 0.6595 0.00985 0.00396 -0.1351 0.6730 0.6576
1.000 0.6866 0.00989 0.00399 -0.1352 0.6715 0.6587
1.250 0.7138 0.00991 0.00401 -0.1353 0.6699 0.6598
1.500 0.7411 0.00994 0.00402 -0.1354 0.6682 0.6608
1.750 0.7685 0.00997 0.00404 -0.1356 0.6668 0.6618
2.000 0.7962 0.01001 0.00407 -0.1358 0.6655 0.6629
2.250 0.8242 0.01003 0.00410 -0.1361 0.6641 0.6639
2.500 0.8514 0.01008 0.00416 -0.1362 0.6626 0.6648
2.750 0.8767 0.01014 0.00428 -0.1359 0.6609 0.6657
3.000 0.9022 0.01020 0.00439 -0.1357 0.6589 0.6666
3.250 0.9278 0.01026 0.00449 -0.1356 0.6568 0.6675
3.500 0.9539 0.01030 0.00457 -0.1355 0.6549 0.6685
3.750 0.9802 0.01034 0.00464 -0.1354 0.6529 0.6695
4.000 1.0069 0.01038 0.00471 -0.1354 0.6510 0.6705
4.250 1.0348 0.01041 0.00473 -0.1357 0.6488 0.6717
4.500 1.0570 0.01047 0.00487 -0.1348 0.6452 0.6731
4.750 1.0797 0.01051 0.00497 -0.1340 0.6409 0.6743
5.000 1.1041 0.01052 0.00500 -0.1335 0.6369 0.6754
5.250 1.1288 0.01053 0.00502 -0.1331 0.6326 0.6765
5.500 1.1483 0.01059 0.00516 -0.1317 0.6265 0.6776
5.750 1.1707 0.01061 0.00519 -0.1308 0.6206 0.6786
6.000 1.1883 0.01066 0.00530 -0.1289 0.6117 0.6796
6.250 1.2056 0.01071 0.00536 -0.1269 0.6020 0.6806
6.500 1.2164 0.01079 0.00545 -0.1237 0.5894 0.6818
6.750 1.2242 0.01098 0.00563 -0.1198 0.5733 0.6829
7.000 1.2277 0.01134 0.00594 -0.1153 0.5504 0.6842
7.250 1.2308 0.01182 0.00637 -0.1110 0.5304 0.6856
7.500 1.2237 0.01270 0.00713 -0.1052 0.5004 0.6871
7.750 1.2142 0.01397 0.00827 -0.0997 0.4702 0.6888
8.000 1.1991 0.01585 0.00997 -0.0941 0.4329 0.6905
8.250 1.1896 0.01777 0.01174 -0.0899 0.3997 0.6918
8.500 1.1861 0.01952 0.01338 -0.0866 0.3719 0.6931
8.750 1.1778 0.02163 0.01532 -0.0830 0.3364 0.6944
9.000 1.1736 0.02361 0.01715 -0.0801 0.3035 0.6955
9.250 1.1691 0.02568 0.01904 -0.0773 0.2677 0.6968
9.500 1.1701 0.02748 0.02072 -0.0752 0.2381 0.6980
9.750 1.1734 0.02920 0.02232 -0.0734 0.2107 0.6993
10.000 1.1744 0.03111 0.02406 -0.0715 0.1784 0.7007
10.250 1.1821 0.03263 0.02552 -0.0702 0.1573 0.7021
10.500 1.1872 0.03434 0.02711 -0.0688 0.1327 0.7036
10.750 1.1961 0.03583 0.02854 -0.0677 0.1154 0.7052
11.000 1.2034 0.03745 0.03008 -0.0666 0.0977 0.7067
11.500 1.2204 0.04057 0.03308 -0.0646 0.0699 0.7101
11.750 1.2310 0.04206 0.03457 -0.0639 0.0599 0.7116
12.000 1.2423 0.04353 0.03604 -0.0634 0.0517 0.7134
12.250 1.2532 0.04506 0.03759 -0.0628 0.0463 0.7153
12.500 1.2645 0.04655 0.03910 -0.0623 0.0416 0.7172
12.750 1.2753 0.04808 0.04066 -0.0618 0.0376 0.7192
13.000 1.2877 0.04955 0.04218 -0.0614 0.0350 0.7214
13.250 1.2974 0.05123 0.04390 -0.0609 0.0321 0.7233
13.500 1.3083 0.05281 0.04553 -0.0604 0.0300 0.7256
13.750 1.3200 0.05441 0.04720 -0.0602 0.0279 0.7276
14.000 1.3303 0.05618 0.04903 -0.0600 0.0260 0.7300
14.250 1.3397 0.05802 0.05091 -0.0596 0.0243 0.7326
14.500 1.3505 0.05974 0.05271 -0.0594 0.0226 0.7355
14.750 1.3604 0.06156 0.05461 -0.0592 0.0215 0.7383
15.000 1.3686 0.06352 0.05662 -0.0589 0.0199 0.7414
15.250 1.3770 0.06560 0.05877 -0.0588 0.0186 0.7444
15.500 1.3866 0.06759 0.06087 -0.0588 0.0177 0.7482
15.750 1.3953 0.06964 0.06299 -0.0588 0.0162 0.7523
16.000 1.4017 0.07193 0.06534 -0.0587 0.0153 0.7567
16.250 1.4079 0.07439 0.06790 -0.0588 0.0148 0.7618
16.500 1.4156 0.07673 0.07036 -0.0590 0.0139 0.7677
17.000 1.4297 0.08180 0.07564 -0.0598 0.0122 0.7838
17.250 1.4350 0.08465 0.07860 -0.0603 0.0115 0.7946
17.500 1.4417 0.08767 0.08176 -0.0614 0.0110 0.8108
17.750 1.4547 0.09109 0.08540 -0.0640 0.0103 0.8446
18.000 1.4812 0.09576 0.09034 -0.0708 0.0093 0.9442
18.250 1.4810 0.09891 0.09355 -0.0703 0.0090 1.0000
18.500 1.4805 0.10218 0.09689 -0.0706 0.0085 1.0000
18.750 1.4811 0.10536 0.10018 -0.0709 0.0081 1.0000
19.000 1.4804 0.10872 0.10365 -0.0714 0.0079 1.0000
19.250 1.4790 0.11219 0.10722 -0.0720 0.0077 1.0000
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