GOE 501 AIRFOIL (goe501-il)
GOE 501 AIRFOIL - Gottingen 501 airfoil
| Details | Dat file | Parser | |
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(goe501-il) GOE 501 AIRFOIL Gottingen 501 airfoil Max thickness 12.8% at 30% chord. Max camber 6.3% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 501 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0273700
0.0250000 0.0392400
0.0500000 0.0554800
0.0750000 0.0682100
0.1000000 0.0789500
0.1500000 0.0934200
0.2000000 0.1054000
0.3000000 0.1188500
0.4000000 0.1203000
0.5000000 0.1142500
0.6000000 0.1032000
0.7000000 0.0841500
0.8000000 0.0606000
0.9000000 0.0320500
0.9500000 0.0155300
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0146300
0.0250000 -.0202600
0.0500000 -.0245300
0.0750000 -.0256900
0.1000000 -.0265500
0.1500000 -.0240800
0.2000000 -.0201000
0.3000000 -.0091500
0.4000000 0.0028000
0.5000000 0.0117500
0.6000000 0.0187000
0.7000000 0.0211500
0.8000000 0.0186000
0.9000000 0.0115500
0.9500000 0.0065200
1.0000000 0.0000000
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Polars for GOE 501 AIRFOIL (goe501-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe501-il | 50,000 | 9 | 9.4 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe501-il | 50,000 | 5 | 29.7 at α=8° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe501-il | 100,000 | 9 | 56.5 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe501-il | 100,000 | 5 | 60.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe501-il | 200,000 | 9 | 85.4 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe501-il | 200,000 | 5 | 80.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe501-il | 500,000 | 9 | 113.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe501-il | 500,000 | 5 | 106.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe501-il | 1,000,000 | 9 | 137.9 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe501-il | 1,000,000 | 5 | 113.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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