GOE 397 AIRFOIL (goe397-il)
GOE 397 AIRFOIL - Gottingen 397 airfoil
| Details | Dat file | Parser | |
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(goe397-il) GOE 397 AIRFOIL Gottingen 397 airfoil Max thickness 5.1% at 30% chord. Max camber 4% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 397 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0130800
0.0250000 0.0191600
0.0500000 0.0273300
0.0750000 0.0339900
0.1000000 0.0396500
0.1500000 0.0489800
0.2000000 0.0563000
0.3000000 0.0634500
0.4000000 0.0646000
0.5000000 0.0613500
0.6000000 0.0524000
0.7000000 0.0415500
0.8000000 0.0282000
0.9000000 0.0148500
0.9500000 0.0076700
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0074200
0.0250000 -.0073400
0.0500000 -.0051700
0.0750000 -.0030100
0.1000000 -.0003500
0.1500000 0.0044700
0.2000000 0.0078000
0.3000000 0.0124500
0.4000000 0.0146000
0.5000000 0.0137500
0.6000000 0.0119000
0.7000000 0.0085500
0.8000000 0.0052000
0.9000000 0.0018500
0.9500000 0.0001800
1.0000000 0.0000000
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Polars for GOE 397 AIRFOIL (goe397-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe397-il | 50,000 | 9 | 42.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe397-il | 50,000 | 5 | 43 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe397-il | 100,000 | 9 | 61.4 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe397-il | 100,000 | 5 | 61 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe397-il | 200,000 | 9 | 81.7 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe397-il | 200,000 | 5 | 79.1 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe397-il | 500,000 | 9 | 110 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe397-il | 500,000 | 5 | 102.1 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe397-il | 1,000,000 | 9 | 129.9 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe397-il | 1,000,000 | 5 | 97.6 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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