WORTMANN FX 75-141 (fx75141-il)
WORTMANN FX 75-141 - Wortmann FX 75-141 airfoil
| Details | Dat file | Parser | |
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(fx75141-il) WORTMANN FX 75-141 Wortmann FX 75-141 airfoil Max thickness 14.1% at 37.1% chord. Max camber 3.4% at 53.3% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
WORTMANN FX 75-141 1.00000 0.00000 0.99893 0.00130 0.99572 0.00259 0.99039 0.00427 0.98296 0.00627 0.97347 0.00863 0.96194 0.01130 0.94844 0.01425 0.93301 0.01751 0.91573 0.02112 0.89668 0.02513 0.87592 0.02957 0.85355 0.03447 0.82967 0.03983 0.80438 0.04571 0.77779 0.05219 0.75000 0.05921 0.72114 0.06646 0.69134 0.07345 0.66072 0.07969 0.62941 0.08500 0.59755 0.08945 0.56526 0.09322 0.53270 0.09636 0.50000 0.09886 0.46730 0.10070 0.43474 0.10182 0.40245 0.10219 0.37059 0.10176 0.33928 0.10054 0.30866 0.09856 0.27886 0.09590 0.25000 0.09265 0.22221 0.08884 0.19562 0.08455 0.17033 0.07982 0.14645 0.07473 0.12408 0.06928 0.10332 0.06346 0.08427 0.05728 0.06699 0.05082 0.05156 0.04420 0.03806 0.03753 0.02653 0.03091 0.01704 0.02436 0.00961 0.01791 0.00428 0.01160 0.00107 0.00558 0.00000 0.00000 0.00107 -0.00508 0.00428 -0.00973 0.00961 -0.01402 0.01704 -0.01795 0.02653 -0.02153 0.03806 -0.02474 0.05156 -0.02765 0.06699 -0.03028 0.08427 -0.03262 0.10332 -0.03466 0.12408 -0.03643 0.14645 -0.03793 0.17033 -0.03914 0.19562 -0.04006 0.22221 -0.04070 0.25000 -0.04107 0.27886 -0.04117 0.30866 -0.04100 0.33928 -0.04049 0.37059 -0.03958 0.40245 -0.03820 0.43474 -0.03631 0.46730 -0.03400 0.50000 -0.03137 0.53270 -0.02851 0.56526 -0.02541 0.59755 -0.02197 0.62941 -0.01809 0.66072 -0.01379 0.69134 -0.00934 0.72114 -0.00511 0.75000 -0.00143 0.77779 0.00155 0.80438 0.00382 0.82967 0.00546 0.85355 0.00655 0.87592 0.00714 0.89668 0.00726 0.91573 0.00694 0.93301 0.00628 0.94844 0.00537 0.96194 0.00431 0.97347 0.00319 0.98296 0.00207 0.99039 0.00093 0.99572 0.00021 0.99893 0.00001 1.00000 0.00000 |
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
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Polars for WORTMANN FX 75-141 (fx75141-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx75141-il | 50,000 | 9 | 30.3 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75141-il | 50,000 | 5 | 26.7 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75141-il | 100,000 | 9 | 54.3 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75141-il | 100,000 | 5 | 53.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75141-il | 200,000 | 9 | 83.8 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75141-il | 200,000 | 5 | 77.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75141-il | 500,000 | 9 | 111.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75141-il | 500,000 | 5 | 103.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx75141-il | 1,000,000 | 9 | 134.9 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx75141-il | 1,000,000 | 5 | 120.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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