GOE 446 AIRFOIL (goe446-il)
GOE 446 AIRFOIL - Gottingen 446 airfoil
Details | Dat file | Parser | |
(goe446-il) GOE 446 AIRFOIL Gottingen 446 airfoil Max thickness 12.9% at 29.7% chord. Max camber 6.3% at 39.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 446 AIRFOIL 17. 17. 0.0000000 0.0000000 0.0119600 0.0231800 0.0241900 0.0345700 0.0487400 0.0538400 0.0734200 0.0677200 0.0981700 0.0784000 0.1477700 0.0954600 0.1974700 0.1083200 0.2971000 0.1239500 0.3970300 0.1268900 0.4971400 0.1222300 0.5974300 0.1096800 0.6979000 0.0897300 0.7984700 0.0654800 0.8991500 0.0364400 0.9495600 0.0190200 1.0000000 0.0016000 0.0000000 0.0000000 0.0129200 -.0178000 0.0255000 -.0212000 0.0505600 -.0238200 0.0755400 -.0232300 0.1004900 -.0210500 0.1503800 -.0161800 0.2002800 -.0118100 0.3001100 -.0046800 0.4000100 -.0002400 0.4999400 0.0027000 0.5998800 0.0050400 0.6998900 0.0046800 0.7999200 0.0033200 0.8999700 0.0013600 0.9499900 0.0004300 1.0000000 -.0016000 |
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Polars for GOE 446 AIRFOIL (goe446-il)
Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
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goe446-il | 50,000 | 9 | 7.6 at α=12.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
goe446-il | 50,000 | 5 | 21.2 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
goe446-il | 100,000 | 9 | 50.9 at α=10.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
goe446-il | 100,000 | 5 | 56.7 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
goe446-il | 200,000 | 9 | 83.8 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
goe446-il | 200,000 | 5 | 83.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
goe446-il | 500,000 | 9 | 122 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
goe446-il | 500,000 | 5 | 111.7 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
goe446-il | 1,000,000 | 9 | 148.7 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
goe446-il | 1,000,000 | 5 | 130.4 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
Reynolds number calculator |