GOE 63 AIRFOIL (goe63-il)
GOE 63 AIRFOIL - Gottingen 63 airfoil
| Details | Dat file | Parser | |
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(goe63-il) GOE 63 AIRFOIL Gottingen 63 airfoil Max thickness 8.3% at 19.9% chord. Max camber 6.7% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 63 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122000 0.0266400
0.0245500 0.0394800
0.0493400 0.0576600
0.0742000 0.0699500
0.0991000 0.0790300
0.1489500 0.0918000
0.1988600 0.0998700
0.2987900 0.1062100
0.3988000 0.1056500
0.4988800 0.0979900
0.5990500 0.0834300
0.6992500 0.0654700
0.7994800 0.0456100
0.8997100 0.0257600
0.9498300 0.0150300
1.0000000 0.0035000
0.0000000 0.0000000
0.0126600 -.0142600
0.0251500 -.0135100
0.0500900 -.0077300
0.0750200 -.0017400
0.0999600 0.0037400
0.1498700 0.0113100
0.1998000 0.0173800
0.2997200 0.0244200
0.3996800 0.0282600
0.4996900 0.0273000
0.5997200 0.0241400
0.6998000 0.0178800
0.7998800 0.0107200
0.8999600 0.0035600
0.9499900 0.0008300
1.0000000 -.0035000
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Polars for GOE 63 AIRFOIL (goe63-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe63-il | 50,000 | 9 | 30.4 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe63-il | 50,000 | 5 | 41.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe63-il | 100,000 | 9 | 61 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe63-il | 100,000 | 5 | 63.3 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe63-il | 200,000 | 9 | 86.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe63-il | 200,000 | 5 | 80.7 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe63-il | 500,000 | 9 | 110.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe63-il | 500,000 | 5 | 102.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe63-il | 1,000,000 | 9 | 128.4 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe63-il | 1,000,000 | 5 | 121.5 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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