WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il)
WORTMANN FX 62-K-131 AIRFOIL - Wortmann FX 62-K-131/17 airfoil
| Details | Dat file | Parser | |
|
(fx62k131-il) WORTMANN FX 62-K-131 AIRFOIL Wortmann FX 62-K-131/17 airfoil Max thickness 13.1% at 40.2% chord. Max camber 3.9% at 53.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
WORTMANN FX 62-K-131 AIRFOIL
49.0 49.0
0.00000 0.00000
0.00107 0.00516
0.00428 0.01037
0.00961 0.01606
0.01704 0.02207
0.02653 0.02855
0.03806 0.03511
0.05156 0.04175
0.06699 0.04830
0.08427 0.05477
0.10332 0.06108
0.12408 0.06721
0.14645 0.07306
0.17033 0.07859
0.19562 0.08369
0.22221 0.08829
0.25000 0.09232
0.27886 0.09577
0.30866 0.09860
0.33928 0.10084
0.37059 0.10245
0.40245 0.10337
0.43474 0.10355
0.46730 0.10300
0.50000 0.10173
0.53270 0.09983
0.56526 0.09728
0.59755 0.09402
0.62941 0.09000
0.66072 0.08523
0.69134 0.07976
0.72114 0.07374
0.75000 0.06732
0.77779 0.06076
0.80438 0.05425
0.82967 0.04797
0.85355 0.04203
0.87592 0.03645
0.89668 0.03123
0.91573 0.02637
0.93301 0.02183
0.94844 0.01759
0.96194 0.01363
0.97347 0.00994
0.98296 0.00661
0.99039 0.00394
0.99572 0.00180
0.99893 0.00034
1.00000 0.00000
0.00000 0.00000
0.00107 -0.00159
0.00428 -0.00386
0.00961 -0.00613
0.01704 -0.00837
0.02653 -0.01061
0.03806 -0.01282
0.05156 -0.01486
0.06699 -0.01682
0.08427 -0.01862
0.10332 -0.02037
0.12408 -0.02195
0.14645 -0.02345
0.17033 -0.02476
0.19562 -0.02596
0.22221 -0.02696
0.25000 -0.02776
0.27886 -0.02828
0.30866 -0.02853
0.33928 -0.02846
0.37059 -0.02814
0.40245 -0.02752
0.43474 -0.02666
0.46730 -0.02548
0.50000 -0.02395
0.53270 -0.02199
0.56526 -0.01962
0.59755 -0.01683
0.62941 -0.01370
0.66072 -0.01025
0.69134 -0.00646
0.72114 -0.00239
0.75000 0.00177
0.77779 0.00573
0.80438 0.00919
0.82967 0.01191
0.85355 0.01386
0.87592 0.01503
0.89668 0.01548
0.91573 0.01523
0.93301 0.01437
0.94844 0.01293
0.96194 0.01102
0.97347 0.00876
0.98296 0.00636
0.99039 0.00427
0.99572 0.00228
0.99893 0.00062
1.00000 0.00000
|
No parser warnings |
Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
Similar airfoils
|
Polars for WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx62k131-il | 50,000 | 5 | 29 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 50,000 | 0 | 30.5 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k131-il | 100,000 | 5 | 55.1 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 100,000 | 0 | 56.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k131-il | 200,000 | 5 | 84.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 200,000 | 0 | 83.7 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k131-il | 500,000 | 5 | 125.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 500,000 | 0 | 124 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx62k131-il | 1,000,000 | 5 | 153.3 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx62k131-il | 1,000,000 | 0 | 162.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| Reynolds number calculator | |||||||