GOE 497 AIRFOIL (goe497-il)
GOE 497 AIRFOIL - Gottingen 497 airfoil
| Details | Dat file | Parser | |
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(goe497-il) GOE 497 AIRFOIL Gottingen 497 airfoil Max thickness 12.7% at 30% chord. Max camber 5.3% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 497 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0249600
0.0250000 0.0364200
0.0500000 0.0518500
0.0750000 0.0632700
0.1000000 0.0727000
0.1500000 0.0875500
0.2000000 0.0969000
0.3000000 0.1081000
0.4000000 0.1088000
0.5000000 0.1040000
0.6000000 0.0922000
0.7000000 0.0754000
0.8000000 0.0536000
0.9000000 0.0283000
0.9500000 0.0145500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0155400
0.0250000 -.0215800
0.0500000 -.0276500
0.0750000 -.0307200
0.1000000 -.0318000
0.1500000 -.0314500
0.2000000 -.0286000
0.3000000 -.0189000
0.4000000 -.0077000
0.5000000 0.0025000
0.6000000 0.0092000
0.7000000 0.0124000
0.8000000 0.0126000
0.9000000 0.0088000
0.9500000 0.0051500
1.0000000 0.0000000
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Polars for GOE 497 AIRFOIL (goe497-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe497-il | 50,000 | 9 | 28.4 at α=11.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe497-il | 50,000 | 5 | 34.8 at α=8.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe497-il | 100,000 | 9 | 58.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe497-il | 100,000 | 5 | 60.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe497-il | 200,000 | 9 | 85 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe497-il | 200,000 | 5 | 82 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe497-il | 500,000 | 9 | 118 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe497-il | 500,000 | 5 | 105.3 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe497-il | 1,000,000 | 9 | 135.2 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe497-il | 1,000,000 | 5 | 114.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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