GOE 417 AIRFOIL (goe417-il)
GOE 417 AIRFOIL - Gottingen 417 airfoil
| Details | Dat file | Parser | |
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(goe417-il) GOE 417 AIRFOIL Gottingen 417 airfoil Max thickness 6% at 20% chord. Max camber 6.1% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 417 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0195800
0.0250000 0.0296600
0.0500000 0.0443200
0.0750000 0.0564900
0.1000000 0.0646500
0.1500000 0.0759700
0.2000000 0.0833000
0.3000000 0.0884500
0.4000000 0.0876000
0.5000000 0.0822500
0.6000000 0.0729000
0.7000000 0.0605500
0.8000000 0.0437000
0.9000000 0.0233500
0.9500000 0.0116800
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0059200
0.0250000 -.0038400
0.0500000 0.0008300
0.0750000 0.0049900
0.1000000 0.0091500
0.1500000 0.0164800
0.2000000 0.0233000
0.3000000 0.0319500
0.4000000 0.0351000
0.5000000 0.0332500
0.6000000 0.0294000
0.7000000 0.0230500
0.8000000 0.0157000
0.9000000 0.0073500
0.9500000 0.0036800
1.0000000 0.0000000
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Polars for GOE 417 AIRFOIL (goe417-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe417-il | 50,000 | 9 | 38.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe417-il | 50,000 | 5 | 44.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe417-il | 100,000 | 9 | 62 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe417-il | 100,000 | 5 | 63.2 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe417-il | 200,000 | 9 | 82.8 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe417-il | 200,000 | 5 | 78.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe417-il | 500,000 | 9 | 105.3 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe417-il | 500,000 | 5 | 102.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe417-il | 1,000,000 | 9 | 127.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe417-il | 1,000,000 | 5 | 115.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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