WORTMANN FX 73-170 (fx73170-il)
WORTMANN FX 73-170 - Wortmann FX 73-170 airfoil
| Details | Dat file | Parser | |
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(fx73170-il) WORTMANN FX 73-170 Wortmann FX 73-170 airfoil Max thickness 17.1% at 43.5% chord. Max camber 4.4% at 56.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
WORTMANN FX 73-170 1.00000 0.00000 0.99893 0.00137 0.99572 0.00263 0.99039 0.00441 0.98296 0.00655 0.97347 0.00917 0.96194 0.01226 0.94844 0.01580 0.93301 0.01983 0.91573 0.02441 0.89668 0.02963 0.87592 0.03555 0.85355 0.04214 0.82967 0.04935 0.80438 0.05718 0.77779 0.06564 0.75000 0.07463 0.72114 0.08388 0.69134 0.09297 0.66072 0.10148 0.62941 0.10905 0.59755 0.11545 0.56526 0.12056 0.53270 0.12434 0.50000 0.12680 0.46730 0.12801 0.43474 0.12809 0.40245 0.12715 0.37059 0.12531 0.33928 0.12264 0.30866 0.11922 0.27886 0.11509 0.25000 0.11031 0.22221 0.10494 0.19562 0.09904 0.17033 0.09267 0.14645 0.08589 0.12408 0.07876 0.10332 0.07136 0.08427 0.06376 0.06699 0.05604 0.05156 0.04827 0.03806 0.04055 0.02653 0.03299 0.01704 0.02567 0.00961 0.01859 0.00428 0.01177 0.00107 0.00545 0.00000 0.00000 0.00107 -0.00442 0.00428 -0.00805 0.00961 -0.01131 0.01704 -0.01447 0.02653 -0.01757 0.03806 -0.02056 0.05156 -0.02343 0.06699 -0.02618 0.08427 -0.02880 0.10332 -0.03127 0.12408 -0.03356 0.14645 -0.03567 0.17033 -0.03759 0.19562 -0.03929 0.22221 -0.04076 0.25000 -0.04198 0.27886 -0.04293 0.30866 -0.04359 0.33928 -0.04394 0.37059 -0.04395 0.40245 -0.04358 0.43474 -0.04281 0.46730 -0.04157 0.50000 -0.03972 0.53270 -0.03699 0.56526 -0.03317 0.59755 -0.02833 0.62941 -0.02285 0.66072 -0.01724 0.69134 -0.01196 0.72114 -0.00727 0.75000 -0.00326 0.77779 0.00001 0.80438 0.00255 0.82967 0.00440 0.85355 0.00562 0.87592 0.00626 0.89668 0.00641 0.91573 0.00616 0.93301 0.00558 0.94844 0.00477 0.96194 0.00378 0.97347 0.00271 0.98296 0.00162 0.99039 0.00057 0.99572 -0.00016 0.99893 -0.00081 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 73-170 (fx73170-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| fx73170-il | 50,000 | 9 | 17.8 at α=14.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx73170-il | 50,000 | 5 | 15.1 at α=13.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx73170-il | 100,000 | 9 | 24.9 at α=12.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx73170-il | 100,000 | 5 | 24.5 at α=11.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx73170-il | 200,000 | 9 | 43.1 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx73170-il | 200,000 | 5 | 45.6 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx73170-il | 500,000 | 9 | 110.3 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx73170-il | 500,000 | 5 | 112.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| fx73170-il | 1,000,000 | 9 | 151.5 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| fx73170-il | 1,000,000 | 5 | 147.3 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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