AUGUST 160 (august160-il)
AUGUST 160 - AUGUST 160 airfoil
| Details | Dat file | Parser | |
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(august160-il) AUGUST 160 AUGUST 160 airfoil Max thickness 16% at 25% chord. Max camber 5.4% at 25% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
AUGUST 160 1.00000 0.00000 0.99893 0.00111 0.99572 0.00175 0.99039 0.00272 0.98296 0.00406 0.97347 0.00578 0.96194 0.00788 0.94844 0.01033 0.93301 0.01318 0.91573 0.01634 0.89668 0.01986 0.87592 0.02365 0.85355 0.02773 0.82967 0.03214 0.80438 0.03688 0.77779 0.04193 0.75000 0.04732 0.72114 0.05309 0.69134 0.05913 0.66072 0.06546 0.62941 0.07195 0.59755 0.07869 0.56526 0.08545 0.53270 0.09232 0.50000 0.09903 0.46730 0.10571 0.43474 0.11203 0.40245 0.11795 0.37059 0.12317 0.33928 0.12765 0.30866 0.13107 0.27886 0.13338 0.25000 0.13406 0.22221 0.13301 0.19562 0.12969 0.17033 0.12467 0.14645 0.11787 0.12408 0.11026 0.10332 0.10130 0.08427 0.09207 0.06699 0.08178 0.05156 0.07169 0.03806 0.06078 0.02653 0.05061 0.01704 0.04100 0.00961 0.03150 0.00428 0.02200 0.00107 0.01311 0.00000 0.00000 0.00107 -0.00360 0.00428 -0.00741 0.00961 -0.01000 0.01704 -0.01250 0.02653 -0.01500 0.03806 -0.01712 0.05156 -0.01900 0.06699 -0.02075 0.08427 -0.02241 0.10332 -0.02320 0.12408 -0.02435 0.14645 -0.02484 0.17033 -0.02562 0.19562 -0.02584 0.22221 -0.02629 0.25000 -0.02632 0.27886 -0.02650 0.30866 -0.02638 0.33928 -0.02633 0.37059 -0.02606 0.40245 -0.02582 0.43474 -0.02538 0.46730 -0.02498 0.50000 -0.02439 0.53270 -0.02385 0.56526 -0.02312 0.59755 -0.02243 0.62941 -0.02158 0.66072 -0.02077 0.69134 -0.01977 0.72114 -0.01881 0.75000 -0.01768 0.77779 -0.01653 0.80438 -0.01521 0.82967 -0.01366 0.85355 -0.01200 0.87592 -0.01024 0.89668 -0.00844 0.91573 -0.00674 0.93301 -0.00517 0.94844 -0.00376 0.96194 -0.00261 0.97347 -0.00172 0.98296 -0.00113 0.99039 -0.00086 0.99572 -0.00082 0.99893 -0.00085 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 AUGUST 160 (august160-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| august160-il | 50,000 | 9 | 4.7 at α=-0.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| august160-il | 50,000 | 5 | 17.3 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| august160-il | 100,000 | 9 | 20.8 at α=0° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| august160-il | 100,000 | 5 | 34.7 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| august160-il | 200,000 | 9 | 42.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| august160-il | 200,000 | 5 | 56.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| august160-il | 500,000 | 9 | 82.1 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| august160-il | 500,000 | 5 | 90.3 at α=8.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| august160-il | 1,000,000 | 9 | 117.2 at α=11° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| august160-il | 1,000,000 | 5 | 120.2 at α=9.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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