GOE 565 AIRFOIL (goe565-il)
GOE 565 AIRFOIL - Gottingen 565 airfoil
| Details | Dat file | Parser | |
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(goe565-il) GOE 565 AIRFOIL Gottingen 565 airfoil Max thickness 8.4% at 30% chord. Max camber 2.8% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 565 AIRFOIL
16. 16.
0.0000000 0.0000000
0.0125000 0.0166300
0.0250000 0.0234500
0.0500000 0.0341100
0.0750000 0.0417600
0.1000000 0.0479200
0.1500000 0.0557300
0.2000000 0.0615400
0.3000000 0.0671600
0.4000000 0.0677800
0.5000000 0.0644000
0.6000000 0.0580200
0.7000000 0.0476400
0.8000000 0.0347600
0.9000000 0.0183800
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0113700
0.0250000 -.0155400
0.0500000 -.0183900
0.0750000 -.0202300
0.1000000 -.0205800
0.1500000 -.0212700
0.2000000 -.0209600
0.3000000 -.0168400
0.4000000 -.0127200
0.5000000 -.0086000
0.6000000 -.0044800
0.7000000 -.0013600
0.8000000 -.0007400
0.9000000 -.0001200
1.0000000 0.0000000
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Polars for GOE 565 AIRFOIL (goe565-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe565-il | 50,000 | 9 | 37.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe565-il | 50,000 | 5 | 39.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe565-il | 100,000 | 9 | 56.9 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe565-il | 100,000 | 5 | 55 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe565-il | 200,000 | 9 | 76.2 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe565-il | 200,000 | 5 | 69 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe565-il | 500,000 | 9 | 98.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe565-il | 500,000 | 5 | 80.7 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe565-il | 1,000,000 | 9 | 110.1 at α=1.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe565-il | 1,000,000 | 5 | 89.9 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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