GOE 361 AIRFOIL (goe361-il)
GOE 361 AIRFOIL - Gottingen 361 airfoil
| Details | Dat file | Parser | |
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(goe361-il) GOE 361 AIRFOIL Gottingen 361 airfoil Max thickness 6.8% at 20% chord. Max camber 5.5% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 361 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0170900
0.0250000 0.0256900
0.0500000 0.0408800
0.0750000 0.0525600
0.1000000 0.0617500
0.1500000 0.0756300
0.2000000 0.0825000
0.3000000 0.0872500
0.4000000 0.0845000
0.5000000 0.0772500
0.6000000 0.0660000
0.7000000 0.0527500
0.8000000 0.0375000
0.9000000 0.0197500
0.9500000 0.0106300
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0084100
0.0250000 -.0073100
0.0500000 -.0041200
0.0750000 -.0004400
0.1000000 0.0032500
0.1500000 0.0096200
0.2000000 0.0145000
0.3000000 0.0222500
0.4000000 0.0260000
0.5000000 0.0277500
0.6000000 0.0265000
0.7000000 0.0227500
0.8000000 0.0175000
0.9000000 0.0087500
0.9500000 0.0036300
1.0000000 0.0000000
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Polars for GOE 361 AIRFOIL (goe361-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe361-il | 50,000 | 9 | 39.3 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe361-il | 50,000 | 5 | 42.4 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe361-il | 100,000 | 9 | 57.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe361-il | 100,000 | 5 | 59.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe361-il | 200,000 | 9 | 76.6 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe361-il | 200,000 | 5 | 77.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe361-il | 500,000 | 9 | 103.8 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe361-il | 500,000 | 5 | 101.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe361-il | 1,000,000 | 9 | 123.4 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe361-il | 1,000,000 | 5 | 119.5 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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