GOE 113 AIRFOIL (goe113-il)
GOE 113 AIRFOIL - Gottingen 113 airfoil
| Details | Dat file | Parser | |
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(goe113-il) GOE 113 AIRFOIL Gottingen 113 airfoil Max thickness 6.7% at 30% chord. Max camber 3% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 113 AIRFOIL
16. 16.
0.0000000 0.0000000
0.0125000 0.0120700
0.0250000 0.0201500
0.0500000 0.0313000
0.0750000 0.0404500
0.1000000 0.0461000
0.1500000 0.0539000
0.2000000 0.0584000
0.3000000 0.0638000
0.4000000 0.0634000
0.5000000 0.0580000
0.6000000 0.0501000
0.7000000 0.0407000
0.8000000 0.0303000
0.9000000 0.0184000
1.0000000 0.0030000
0.0000000 0.0000000
0.0125000 -.0059200
0.0250000 -.0058500
0.0500000 -.0057000
0.0750000 -.0053500
0.1000000 -.0050000
0.1500000 -.0043000
0.2000000 -.0038000
0.3000000 -.0027000
0.4000000 -.0016000
0.5000000 -.0010000
0.6000000 -.0004000
0.7000000 -.0003000
0.8000000 -.0002000
0.9000000 0.0001000
1.0000000 0.0000000
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Polars for GOE 113 AIRFOIL (goe113-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe113-il | 50,000 | 9 | 37.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe113-il | 50,000 | 5 | 40 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe113-il | 100,000 | 9 | 54.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe113-il | 100,000 | 5 | 54.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe113-il | 200,000 | 9 | 70 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe113-il | 200,000 | 5 | 66.8 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe113-il | 500,000 | 9 | 86.8 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe113-il | 500,000 | 5 | 78 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe113-il | 1,000,000 | 9 | 97.1 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe113-il | 1,000,000 | 5 | 83.3 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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