GOE 795 smoothed (goe795sm-il)
GOE 795 smoothed - Gottingen 795 airfoil (smoothed)
| Details | Dat file | Parser | |
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(goe795sm-il) GOE 795 smoothed Gottingen 795 airfoil (smoothed) Max thickness 8% at 30.9% chord. Max camber 2.4% at 43.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
GOE 795 smoothed 1.00000 0.0 0.99572 0.00101 0.98296 0.00382 0.96194 0.00793 0.93301 0.01294 0.89668 0.01862 0.85355 0.02487 0.80438 0.03156 0.75000 0.03845 0.69134 0.04524 0.62941 0.05149 0.56526 0.05680 0.50000 0.06078 0.43474 0.06319 0.37059 0.06395 0.33928 0.06373 0.30866 0.06312 0.27886 0.06210 0.25000 0.06066 0.22221 0.05877 0.19562 0.05643 0.17033 0.05367 0.14645 0.05053 0.12408 0.04706 0.10332 0.04332 0.08427 0.03934 0.06699 0.03513 0.05156 0.03071 0.03806 0.02610 0.02653 0.02135 0.01704 0.01659 0.00961 0.01195 0.00428 0.00759 0.00107 0.00357 0.0 -0.00009 0.00107 -0.00349 0.00428 -0.00669 0.00961 -0.00966 0.01704 -0.01230 0.02653 -0.01450 0.03806 -0.01622 0.05156 -0.01753 0.06699 -0.01857 0.08427 -0.01943 0.10332 -0.02013 0.12408 -0.02058 0.14645 -0.02071 0.17033 -0.02049 0.19562 -0.01997 0.22221 -0.01928 0.25000 -0.01855 0.27886 -0.01784 0.30866 -0.01716 0.33928 -0.01648 0.37059 -0.01579 0.43474 -0.01440 0.50000 -0.01301 0.56526 -0.01166 0.62941 -0.01035 0.69134 -0.00910 0.75000 -0.00788 0.80438 -0.00674 0.85355 -0.00569 0.89668 -0.00475 0.93301 -0.00382 0.96194 -0.00275 0.98296 -0.00153 0.99572 -0.00044 1.00000 0.0 ZZ |
Dat file parser warnings
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
Similar airfoils
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Polars for GOE 795 smoothed (goe795sm-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe795sm-il | 50,000 | 9 | 37.7 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795sm-il | 50,000 | 5 | 38 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795sm-il | 100,000 | 9 | 56.5 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795sm-il | 100,000 | 5 | 54.2 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795sm-il | 200,000 | 9 | 76.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795sm-il | 200,000 | 5 | 69.7 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795sm-il | 500,000 | 9 | 101.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795sm-il | 500,000 | 5 | 86.2 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe795sm-il | 1,000,000 | 9 | 116.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe795sm-il | 1,000,000 | 5 | 96.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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