FX 76-MP-140 (fx76mp140-il)
FX 76-MP-140 - Wortmann FX 76-MP-140 airfoil
| Details | Dat file | Parser | |
|
(fx76mp140-il) FX 76-MP-140 Wortmann FX 76-MP-140 airfoil Max thickness 14.1% at 33.9% chord. Max camber 7.1% at 46.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
FX 76-MP-140 1.00000 0.00000 0.99893 0.00145 0.99572 0.00293 0.99039 0.00509 0.98296 0.00787 0.97347 0.01118 0.96194 0.01496 0.94844 0.01936 0.93301 0.02433 0.91573 0.02995 0.89668 0.03617 0.87592 0.04303 0.85355 0.05048 0.82967 0.05851 0.80438 0.06708 0.77779 0.07613 0.75000 0.08541 0.72114 0.09466 0.69134 0.10341 0.66072 0.11139 0.62941 0.11842 0.59755 0.12451 0.56526 0.12952 0.53270 0.13352 0.50000 0.13652 0.46730 0.13862 0.43474 0.13977 0.40245 0.14003 0.37059 0.13935 0.33928 0.13779 0.30866 0.13531 0.27886 0.13200 0.25000 0.12779 0.22221 0.12277 0.19562 0.11695 0.17033 0.11043 0.14645 0.10324 0.12408 0.09557 0.10332 0.08734 0.08427 0.07869 0.06699 0.06946 0.05156 0.05986 0.03806 0.04998 0.02653 0.04044 0.01704 0.03121 0.00961 0.02273 0.00428 0.01459 0.00107 0.00750 0.00000 0.00000 0.00107 -0.00489 0.00428 -0.00938 0.00961 -0.01359 0.01704 -0.01688 0.02653 -0.01936 0.03806 -0.02085 0.05156 -0.02163 0.06699 -0.02171 0.08427 -0.02131 0.10332 -0.02043 0.12408 -0.01916 0.14645 -0.01755 0.17033 -0.01573 0.19562 -0.01376 0.22221 -0.01169 0.25000 -0.00958 0.27886 -0.00743 0.30866 -0.00534 0.33928 -0.00329 0.37059 -0.00136 0.40245 0.00048 0.43474 0.00218 0.46730 0.00381 0.50000 0.00532 0.53270 0.00675 0.56526 0.00806 0.59755 0.00933 0.62941 0.01051 0.66072 0.01171 0.69134 0.01287 0.72114 0.01404 0.75000 0.01510 0.77779 0.01599 0.80438 0.01651 0.82967 0.01668 0.85355 0.01639 0.87592 0.01572 0.89668 0.01461 0.91573 0.01319 0.93301 0.01147 0.94844 0.00959 0.96194 0.00755 0.97347 0.00549 0.98296 0.00349 0.99039 0.00171 0.99572 0.00032 0.99893 0.00016 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 FX 76-MP-140 (fx76mp140-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx76mp140-il | 50,000 | 9 | 5.9 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76mp140-il | 50,000 | 5 | 14.1 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76mp140-il | 100,000 | 9 | 37.8 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76mp140-il | 100,000 | 5 | 37.3 at α=9.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76mp140-il | 200,000 | 9 | 78.1 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76mp140-il | 200,000 | 5 | 78.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76mp140-il | 500,000 | 9 | 138.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76mp140-il | 500,000 | 5 | 131.5 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx76mp140-il | 1,000,000 | 9 | 181.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx76mp140-il | 1,000,000 | 5 | 153.4 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| Reynolds number calculator | |||||||