WORTMANN FX 76-120 (fx76120-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: WORTMANN FX 76-120 (fx76120-il) Reynolds number: 200,000 Max Cl/Cd: 49.45 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx76120-il-200000-n5.txt Download as CSV file: xf-fx76120-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 76-120
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.250 -0.8900 0.12691 0.12253 -0.0049 1.0000 0.0251
-17.000 -0.9395 0.11189 0.10727 -0.0136 1.0000 0.0250
-16.750 -0.9672 0.10224 0.09743 -0.0192 1.0000 0.0250
-16.500 -0.9929 0.09341 0.08842 -0.0244 1.0000 0.0252
-16.250 -1.0103 0.08648 0.08132 -0.0283 1.0000 0.0252
-16.000 -1.0285 0.07961 0.07426 -0.0322 1.0000 0.0255
-15.750 -1.0422 0.07376 0.06824 -0.0354 1.0000 0.0257
-15.500 -1.0547 0.06830 0.06258 -0.0383 1.0000 0.0259
-15.250 -1.0653 0.06331 0.05743 -0.0409 1.0000 0.0263
-15.000 -1.0712 0.05931 0.05335 -0.0426 1.0000 0.0267
-14.750 -1.0759 0.05556 0.04952 -0.0443 1.0000 0.0271
-14.500 -1.0798 0.05206 0.04592 -0.0457 1.0000 0.0275
-14.250 -1.0823 0.04889 0.04265 -0.0467 1.0000 0.0280
-14.000 -1.0847 0.04591 0.03953 -0.0473 1.0000 0.0284
-13.750 -1.0855 0.04327 0.03677 -0.0475 1.0000 0.0290
-13.500 -1.0856 0.04086 0.03422 -0.0473 1.0000 0.0297
-13.250 -1.0843 0.03873 0.03192 -0.0467 1.0000 0.0305
-13.000 -1.0816 0.03682 0.02983 -0.0457 1.0000 0.0312
-12.750 -1.0799 0.03497 0.02791 -0.0444 1.0000 0.0318
-12.500 -1.0769 0.03340 0.02628 -0.0429 1.0000 0.0325
-12.250 -1.0720 0.03208 0.02490 -0.0412 1.0000 0.0335
-12.000 -1.0663 0.03084 0.02357 -0.0392 1.0000 0.0344
-11.750 -1.0596 0.02972 0.02235 -0.0371 1.0000 0.0354
-11.500 -1.0520 0.02870 0.02120 -0.0347 1.0000 0.0366
-11.250 -1.0450 0.02771 0.02010 -0.0321 1.0000 0.0376
-11.000 -1.0404 0.02671 0.01909 -0.0290 1.0000 0.0387
-10.750 -1.0323 0.02588 0.01821 -0.0262 1.0000 0.0399
-10.500 -1.0206 0.02512 0.01738 -0.0240 1.0000 0.0416
-10.250 -1.0082 0.02435 0.01652 -0.0217 1.0000 0.0432
-10.000 -0.9958 0.02356 0.01566 -0.0194 1.0000 0.0449
-9.750 -0.9840 0.02276 0.01485 -0.0171 1.0000 0.0468
-9.500 -0.9696 0.02210 0.01413 -0.0150 1.0000 0.0489
-9.250 -0.9541 0.02149 0.01344 -0.0130 1.0000 0.0515
-9.000 -0.9400 0.02079 0.01271 -0.0108 1.0000 0.0540
-8.750 -0.9249 0.02015 0.01205 -0.0087 1.0000 0.0569
-8.500 -0.9084 0.01960 0.01144 -0.0068 1.0000 0.0604
-8.250 -0.8929 0.01900 0.01083 -0.0047 1.0000 0.0643
-8.000 -0.8766 0.01846 0.01028 -0.0027 1.0000 0.0690
-7.750 -0.8601 0.01794 0.00974 -0.0008 1.0000 0.0743
-7.500 -0.8436 0.01743 0.00923 0.0012 1.0000 0.0809
-7.250 -0.8270 0.01694 0.00876 0.0032 1.0000 0.0891
-7.000 -0.8100 0.01649 0.00833 0.0051 1.0000 0.0988
-6.750 -0.7928 0.01607 0.00794 0.0070 1.0000 0.1104
-6.500 -0.7753 0.01569 0.00759 0.0088 1.0000 0.1233
-6.000 -0.7395 0.01502 0.00700 0.0124 1.0000 0.1505
-5.750 -0.7212 0.01473 0.00674 0.0141 1.0000 0.1638
-5.500 -0.6985 0.01445 0.00649 0.0149 0.9991 0.1772
-5.250 -0.6643 0.01418 0.00625 0.0133 0.9951 0.1934
-5.000 -0.6312 0.01390 0.00600 0.0120 0.9907 0.2089
-4.750 -0.5973 0.01364 0.00579 0.0106 0.9867 0.2255
-4.500 -0.5645 0.01338 0.00558 0.0094 0.9820 0.2425
-4.250 -0.5304 0.01313 0.00537 0.0079 0.9778 0.2599
-4.000 -0.4984 0.01287 0.00517 0.0070 0.9721 0.2777
-3.750 -0.4640 0.01258 0.00497 0.0055 0.9667 0.2974
-3.500 -0.4295 0.01228 0.00476 0.0041 0.9599 0.3191
-3.250 -0.3943 0.01200 0.00455 0.0026 0.9535 0.3420
-3.000 -0.3609 0.01170 0.00437 0.0015 0.9466 0.3665
-2.750 -0.3256 0.01143 0.00420 0.0000 0.9409 0.3941
-2.500 -0.2951 0.01115 0.00404 -0.0005 0.9319 0.4227
-2.250 -0.2630 0.01087 0.00388 -0.0012 0.9228 0.4532
-2.000 -0.2294 0.01057 0.00372 -0.0022 0.9125 0.4863
-1.750 -0.2007 0.01031 0.00360 -0.0021 0.8988 0.5219
-1.500 -0.1715 0.01006 0.00349 -0.0021 0.8849 0.5577
-1.250 -0.1423 0.00984 0.00339 -0.0020 0.8700 0.5928
-1.000 -0.1137 0.00964 0.00330 -0.0017 0.8531 0.6281
-0.750 -0.0852 0.00946 0.00324 -0.0013 0.8337 0.6630
-0.500 -0.0563 0.00932 0.00318 -0.0010 0.8119 0.6977
-0.250 -0.0285 0.00924 0.00315 -0.0005 0.7862 0.7297
0.000 0.0000 0.00921 0.00314 0.0000 0.7593 0.7600
0.250 0.0285 0.00924 0.00316 0.0004 0.7298 0.7867
0.500 0.0563 0.00932 0.00318 0.0010 0.6980 0.8117
0.750 0.0853 0.00946 0.00324 0.0013 0.6634 0.8338
1.000 0.1137 0.00964 0.00331 0.0017 0.6282 0.8535
1.250 0.1422 0.00984 0.00339 0.0020 0.5929 0.8699
1.500 0.1714 0.01006 0.00349 0.0021 0.5576 0.8847
1.750 0.2006 0.01031 0.00360 0.0021 0.5209 0.8988
2.000 0.2294 0.01057 0.00372 0.0022 0.4860 0.9125
2.250 0.2630 0.01087 0.00388 0.0012 0.4530 0.9228
2.500 0.2952 0.01116 0.00404 0.0005 0.4219 0.9320
2.750 0.3257 0.01143 0.00420 0.0000 0.3942 0.9409
3.000 0.3608 0.01170 0.00437 -0.0015 0.3665 0.9466
3.250 0.3942 0.01199 0.00455 -0.0026 0.3423 0.9534
3.500 0.4295 0.01228 0.00476 -0.0041 0.3194 0.9599
3.750 0.4640 0.01258 0.00497 -0.0055 0.2974 0.9668
4.000 0.4984 0.01287 0.00517 -0.0070 0.2778 0.9721
4.250 0.5304 0.01313 0.00537 -0.0079 0.2600 0.9779
4.500 0.5646 0.01338 0.00558 -0.0094 0.2425 0.9820
4.750 0.5973 0.01364 0.00579 -0.0106 0.2255 0.9868
5.000 0.6313 0.01390 0.00600 -0.0120 0.2092 0.9908
5.250 0.6644 0.01418 0.00625 -0.0133 0.1932 0.9951
5.500 0.6986 0.01445 0.00649 -0.0149 0.1773 0.9991
5.750 0.7212 0.01473 0.00674 -0.0141 0.1639 1.0000
6.000 0.7394 0.01502 0.00700 -0.0124 0.1505 1.0000
6.250 0.7575 0.01534 0.00728 -0.0106 0.1367 1.0000
6.500 0.7753 0.01568 0.00759 -0.0088 0.1233 1.0000
6.750 0.7928 0.01607 0.00794 -0.0070 0.1103 1.0000
7.000 0.8100 0.01649 0.00833 -0.0051 0.0989 1.0000
7.250 0.8270 0.01693 0.00876 -0.0032 0.0894 1.0000
7.500 0.8435 0.01743 0.00923 -0.0012 0.0813 1.0000
7.750 0.8601 0.01793 0.00973 0.0008 0.0743 1.0000
8.000 0.8767 0.01845 0.01027 0.0027 0.0690 1.0000
8.250 0.8930 0.01900 0.01083 0.0047 0.0642 1.0000
8.500 0.9086 0.01959 0.01143 0.0068 0.0603 1.0000
8.750 0.9249 0.02015 0.01205 0.0087 0.0568 1.0000
9.000 0.9400 0.02078 0.01271 0.0108 0.0539 1.0000
9.250 0.9543 0.02148 0.01343 0.0130 0.0514 1.0000
9.500 0.9697 0.02210 0.01413 0.0150 0.0489 1.0000
9.750 0.9841 0.02276 0.01484 0.0170 0.0467 1.0000
10.250 1.0083 0.02436 0.01653 0.0217 0.0433 1.0000
10.500 1.0211 0.02509 0.01736 0.0239 0.0414 1.0000
10.750 1.0325 0.02588 0.01822 0.0262 0.0399 1.0000
11.000 1.0406 0.02671 0.01909 0.0290 0.0386 1.0000
11.250 1.0456 0.02770 0.02010 0.0320 0.0377 1.0000
11.500 1.0523 0.02871 0.02121 0.0347 0.0366 1.0000
11.750 1.0599 0.02974 0.02237 0.0370 0.0355 1.0000
12.000 1.0667 0.03084 0.02358 0.0392 0.0344 1.0000
12.250 1.0726 0.03206 0.02488 0.0411 0.0334 1.0000
12.500 1.0775 0.03338 0.02626 0.0428 0.0324 1.0000
12.750 1.0807 0.03495 0.02790 0.0443 0.0318 1.0000
13.000 1.0825 0.03681 0.02982 0.0456 0.0312 1.0000
13.250 1.0851 0.03873 0.03193 0.0466 0.0305 1.0000
13.500 1.0865 0.04085 0.03421 0.0471 0.0297 1.0000
13.750 1.0868 0.04322 0.03672 0.0473 0.0289 1.0000
14.000 1.0861 0.04584 0.03947 0.0471 0.0284 1.0000
14.250 1.0843 0.04875 0.04250 0.0465 0.0278 1.0000
14.500 1.0814 0.05197 0.04581 0.0454 0.0273 1.0000
14.750 1.0779 0.05545 0.04938 0.0440 0.0268 1.0000
15.000 1.0727 0.05925 0.05327 0.0424 0.0265 1.0000
15.250 1.0673 0.06322 0.05735 0.0407 0.0263 1.0000
15.500 1.0559 0.06833 0.06263 0.0381 0.0259 1.0000
15.750 1.0452 0.07348 0.06794 0.0354 0.0257 1.0000
16.000 1.0287 0.07989 0.07456 0.0317 0.0254 1.0000
16.250 1.0125 0.08635 0.08119 0.0281 0.0252 1.0000
16.500 0.9924 0.09386 0.08888 0.0238 0.0250 1.0000
16.750 0.9698 0.10208 0.09728 0.0191 0.0250 1.0000
17.000 0.9401 0.11218 0.10757 0.0132 0.0249 1.0000
17.250 0.8467 0.13781 0.13356 -0.0015 0.0253 1.0000
|
Polar data table (+)
Polar graphs
<< Back to WORTMANN FX 76-120 (fx76120-il)