GOE 364 AIRFOIL (goe364-il)
GOE 364 AIRFOIL - Gottingen 364 airfoil
| Details | Dat file | Parser | |
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(goe364-il) GOE 364 AIRFOIL Gottingen 364 airfoil Max thickness 10.8% at 30% chord. Max camber 6.5% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 364 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0320900
0.0250000 0.0461700
0.0500000 0.0653500
0.0750000 0.0785200
0.1000000 0.0887000
0.1500000 0.1030500
0.2000000 0.1114000
0.3000000 0.1191000
0.4000000 0.1158000
0.5000000 0.1065000
0.6000000 0.0912000
0.7000000 0.0719000
0.8000000 0.0506000
0.9000000 0.0273000
0.9500000 0.0136500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0079100
0.0250000 -.0078300
0.0500000 -.0060500
0.0750000 -.0039800
0.1000000 -.0013000
0.1500000 0.0030500
0.2000000 0.0064000
0.3000000 0.0111000
0.4000000 0.0128000
0.5000000 0.0135000
0.6000000 0.0112000
0.7000000 0.0089000
0.8000000 0.0066000
0.9000000 0.0023000
0.9500000 0.0006500
1.0000000 0.0000000
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Polars for GOE 364 AIRFOIL (goe364-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe364-il | 50,000 | 9 | 13.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe364-il | 50,000 | 5 | 34.8 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe364-il | 100,000 | 9 | 52.5 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe364-il | 100,000 | 5 | 57 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe364-il | 200,000 | 9 | 76.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe364-il | 200,000 | 5 | 76.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe364-il | 500,000 | 9 | 107.8 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe364-il | 500,000 | 5 | 104 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe364-il | 1,000,000 | 9 | 133.4 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe364-il | 1,000,000 | 5 | 124.5 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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