WORTMANN FX 77-W-343 AIRFOIL (fx77w343-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 77-W-343 AIRFOIL (fx77w343-il) Reynolds number: 500,000 Max Cl/Cd: 59.58 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx77w343-il-500000-n5.txt Download as CSV file: xf-fx77w343-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 77-W-343 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-19.500 -0.9929 0.10319 0.09534 -0.0141 0.4633 0.0212
-19.250 -0.9867 0.10052 0.09261 -0.0150 0.4616 0.0213
-19.000 -0.9816 0.09772 0.08974 -0.0159 0.4598 0.0214
-18.750 -0.9743 0.09523 0.08719 -0.0167 0.4579 0.0216
-18.500 -0.9673 0.09273 0.08463 -0.0174 0.4561 0.0218
-18.250 -0.9609 0.09016 0.08200 -0.0181 0.4543 0.0220
-18.000 -0.9526 0.08784 0.07963 -0.0187 0.4525 0.0223
-17.750 -0.9451 0.08543 0.07717 -0.0193 0.4507 0.0226
-17.500 -0.9365 0.08317 0.07487 -0.0199 0.4490 0.0229
-17.250 -0.9268 0.08105 0.07270 -0.0204 0.4473 0.0233
-17.000 -0.9178 0.07886 0.07049 -0.0209 0.4462 0.0237
-16.750 -0.9077 0.07682 0.06843 -0.0213 0.4454 0.0241
-16.500 -0.8964 0.07494 0.06655 -0.0216 0.4445 0.0245
-16.250 -0.8850 0.07308 0.06469 -0.0220 0.4436 0.0263
-16.000 -0.8742 0.07114 0.06273 -0.0223 0.4426 0.0276
-15.750 -0.8613 0.06943 0.06097 -0.0226 0.4415 0.0296
-15.500 -0.8481 0.06776 0.05925 -0.0229 0.4404 0.0305
-15.250 -0.8353 0.06606 0.05750 -0.0232 0.4393 0.0312
-15.000 -0.8212 0.06451 0.05591 -0.0234 0.4382 0.0317
-14.750 -0.8074 0.06296 0.05432 -0.0237 0.4371 0.0322
-14.500 -0.7939 0.06138 0.05270 -0.0239 0.4360 0.0328
-14.250 -0.7802 0.05984 0.05111 -0.0241 0.4349 0.0334
-14.000 -0.7649 0.05847 0.04970 -0.0242 0.4338 0.0340
-13.750 -0.7493 0.05715 0.04833 -0.0244 0.4327 0.0346
-13.500 -0.7336 0.05584 0.04697 -0.0246 0.4316 0.0351
-13.250 -0.7181 0.05452 0.04561 -0.0247 0.4304 0.0355
-13.000 -0.7027 0.05323 0.04427 -0.0249 0.4292 0.0359
-12.750 -0.6885 0.05187 0.04288 -0.0249 0.4281 0.0364
-12.500 -0.6737 0.05056 0.04154 -0.0249 0.4272 0.0369
-12.250 -0.6589 0.04924 0.04020 -0.0249 0.4267 0.0374
-12.000 -0.6437 0.04797 0.03892 -0.0250 0.4262 0.0379
-11.750 -0.6273 0.04683 0.03775 -0.0250 0.4256 0.0384
-11.500 -0.6107 0.04571 0.03661 -0.0250 0.4249 0.0388
-11.250 -0.5942 0.04460 0.03548 -0.0250 0.4240 0.0393
-11.000 -0.5775 0.04351 0.03436 -0.0249 0.4231 0.0397
-10.750 -0.5621 0.04236 0.03321 -0.0248 0.4222 0.0404
-10.500 -0.5464 0.04126 0.03210 -0.0247 0.4212 0.0410
-10.250 -0.5303 0.04020 0.03102 -0.0245 0.4203 0.0416
-10.000 -0.5142 0.03915 0.02996 -0.0244 0.4194 0.0423
-9.750 -0.4983 0.03812 0.02891 -0.0242 0.4187 0.0429
-9.500 -0.4812 0.03720 0.02798 -0.0240 0.4179 0.0436
-9.250 -0.4644 0.03629 0.02707 -0.0238 0.4172 0.0444
-9.000 -0.4481 0.03539 0.02617 -0.0235 0.4165 0.0452
-8.750 -0.4321 0.03450 0.02527 -0.0232 0.4158 0.0461
-8.500 -0.4165 0.03359 0.02436 -0.0228 0.4151 0.0470
-8.250 -0.4010 0.03269 0.02347 -0.0224 0.4144 0.0482
-8.000 -0.3870 0.03173 0.02255 -0.0218 0.4138 0.0521
-7.750 -0.3695 0.03097 0.02177 -0.0215 0.4131 0.0586
-7.500 -0.3517 0.03024 0.02101 -0.0211 0.4125 0.0611
-7.250 -0.3357 0.02942 0.02018 -0.0207 0.4118 0.0631
-7.000 -0.3192 0.02867 0.01940 -0.0201 0.4112 0.0648
-6.750 -0.3029 0.02793 0.01864 -0.0196 0.4105 0.0661
-6.500 -0.2905 0.02716 0.01784 -0.0184 0.4098 0.0671
-6.250 -0.2893 0.02630 0.01695 -0.0156 0.4092 0.0681
-6.000 -0.2751 0.02556 0.01621 -0.0149 0.4088 0.0694
-5.750 -0.2550 0.02488 0.01552 -0.0152 0.4085 0.0709
-5.500 -0.2314 0.02424 0.01489 -0.0160 0.4081 0.0729
-5.250 -0.2056 0.02359 0.01427 -0.0173 0.4077 0.0759
-5.000 -0.1784 0.02275 0.01353 -0.0193 0.4073 0.0929
-4.750 -0.1473 0.02230 0.01308 -0.0212 0.4068 0.1018
-4.500 -0.1152 0.02180 0.01260 -0.0234 0.4062 0.1073
-4.250 -0.0818 0.02114 0.01203 -0.0262 0.4055 0.1192
-4.000 -0.0481 0.02060 0.01157 -0.0288 0.4048 0.1473
-3.750 -0.0143 0.02021 0.01125 -0.0311 0.4040 0.1598
-3.500 0.0204 0.01971 0.01087 -0.0338 0.4033 0.1939
-3.250 0.0551 0.01938 0.01062 -0.0361 0.4026 0.2099
-3.000 0.0917 0.01874 0.01019 -0.0394 0.4020 0.2616
-2.750 0.1297 0.01804 0.00974 -0.0430 0.4013 0.3209
-2.500 0.1709 0.01705 0.00915 -0.0477 0.4006 0.4174
-2.250 0.2070 0.01681 0.00903 -0.0501 0.4000 0.4500
-2.000 0.2430 0.01659 0.00896 -0.0525 0.3992 0.4855
-1.750 0.2776 0.01656 0.00895 -0.0543 0.3985 0.5021
-1.500 0.3122 0.01654 0.00900 -0.0560 0.3978 0.5157
-1.250 0.3464 0.01658 0.00913 -0.0577 0.3970 0.5338
-1.000 0.3802 0.01666 0.00921 -0.0593 0.3962 0.5506
-0.750 0.4138 0.01675 0.00929 -0.0608 0.3955 0.5583
-0.500 0.4472 0.01688 0.00943 -0.0622 0.3948 0.5665
-0.250 0.4807 0.01700 0.00951 -0.0637 0.3939 0.5745
0.000 0.5133 0.01724 0.00979 -0.0650 0.3930 0.5810
0.250 0.5458 0.01750 0.01004 -0.0662 0.3919 0.5867
0.500 0.5787 0.01769 0.01022 -0.0676 0.3911 0.5915
0.750 0.6116 0.01785 0.01040 -0.0690 0.3907 0.5951
1.000 0.6442 0.01802 0.01059 -0.0703 0.3901 0.5983
1.250 0.6769 0.01817 0.01075 -0.0717 0.3895 0.6012
1.500 0.7096 0.01834 0.01090 -0.0731 0.3889 0.6050
1.750 0.7426 0.01849 0.01103 -0.0746 0.3883 0.6093
2.000 0.7748 0.01869 0.01124 -0.0759 0.3877 0.6123
2.250 0.8064 0.01893 0.01150 -0.0771 0.3870 0.6149
2.500 0.8381 0.01914 0.01173 -0.0783 0.3863 0.6173
2.750 0.8699 0.01934 0.01194 -0.0795 0.3856 0.6197
3.000 0.9016 0.01953 0.01214 -0.0808 0.3849 0.6222
3.250 0.9333 0.01973 0.01233 -0.0821 0.3841 0.6248
3.500 0.9650 0.01993 0.01251 -0.0835 0.3833 0.6271
3.750 0.9966 0.02013 0.01270 -0.0848 0.3826 0.6289
4.000 1.0274 0.02027 0.01286 -0.0860 0.3818 0.6306
4.250 1.0580 0.02043 0.01304 -0.0871 0.3811 0.6318
4.500 1.0884 0.02060 0.01321 -0.0883 0.3803 0.6327
4.750 1.1186 0.02077 0.01340 -0.0894 0.3795 0.6336
5.000 1.1485 0.02095 0.01358 -0.0904 0.3787 0.6345
5.250 1.1781 0.02114 0.01378 -0.0915 0.3779 0.6355
5.500 1.2072 0.02136 0.01399 -0.0924 0.3770 0.6367
5.750 1.2358 0.02161 0.01423 -0.0933 0.3759 0.6379
6.000 1.2641 0.02189 0.01451 -0.0942 0.3748 0.6390
6.250 1.2919 0.02218 0.01482 -0.0950 0.3738 0.6400
6.500 1.3188 0.02244 0.01512 -0.0957 0.3732 0.6410
6.750 1.3449 0.02273 0.01545 -0.0963 0.3724 0.6420
7.000 1.3701 0.02305 0.01582 -0.0968 0.3716 0.6429
7.250 1.3941 0.02340 0.01621 -0.0971 0.3706 0.6439
7.500 1.4167 0.02379 0.01665 -0.0972 0.3696 0.6448
7.750 1.4373 0.02424 0.01714 -0.0971 0.3685 0.6458
8.000 1.4543 0.02476 0.01770 -0.0964 0.3672 0.6467
8.250 1.4582 0.02558 0.01857 -0.0936 0.3657 0.6475
8.500 1.4686 0.02659 0.01963 -0.0925 0.3642 0.6483
8.750 1.4806 0.02770 0.02077 -0.0920 0.3628 0.6491
9.000 1.4933 0.02884 0.02195 -0.0918 0.3613 0.6503
9.250 1.5054 0.03010 0.02324 -0.0916 0.3597 0.6513
9.500 1.5161 0.03152 0.02468 -0.0915 0.3579 0.6521
9.750 1.5209 0.03356 0.02683 -0.0913 0.3560 0.6529
10.000 1.5217 0.03603 0.02942 -0.0910 0.3535 0.6536
10.250 1.5186 0.03891 0.03241 -0.0906 0.3505 0.6542
10.500 1.5100 0.04235 0.03593 -0.0902 0.3475 0.6548
10.750 1.5003 0.04595 0.03960 -0.0897 0.3445 0.6554
11.000 1.4822 0.05041 0.04412 -0.0891 0.3416 0.6559
11.250 1.3126 0.07082 0.06494 -0.0841 0.3332 0.6556
11.500 1.3150 0.07357 0.06767 -0.0844 0.3301 0.6562
11.750 1.3372 0.07414 0.06819 -0.0852 0.3279 0.6568
12.000 1.1619 0.09689 0.09129 -0.0813 0.3165 0.6564
12.250 1.1931 0.09644 0.09081 -0.0823 0.3153 0.6571
12.500 1.2261 0.09579 0.09011 -0.0834 0.3141 0.6578
12.750 1.2575 0.09528 0.08956 -0.0844 0.3127 0.6586
13.000 1.2875 0.09491 0.08914 -0.0854 0.3112 0.6596
13.500 1.1842 0.11371 0.10821 -0.0848 0.2971 0.6600
13.750 1.2099 0.11381 0.10828 -0.0858 0.2960 0.6609
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