GOE 387 AIRFOIL (goe387-il)
GOE 387 AIRFOIL - Gottingen 387 airfoil
| Details | Dat file | Parser | |
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(goe387-il) GOE 387 AIRFOIL Gottingen 387 airfoil Max thickness 14.9% at 30% chord. Max camber 5.5% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 387 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0308800
0.0250000 0.0452600
0.0500000 0.0645200
0.0750000 0.0787900
0.1000000 0.0905500
0.1500000 0.1065800
0.2000000 0.1181000
0.3000000 0.1276500
0.4000000 0.1262000
0.5000000 0.1167500
0.6000000 0.0998000
0.7000000 0.0783500
0.8000000 0.0539000
0.9000000 0.0279500
0.9500000 0.0144700
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0186200
0.0250000 -.0217400
0.0500000 -.0249700
0.0750000 -.0272100
0.1000000 -.0279500
0.1500000 -.0274300
0.2000000 -.0259000
0.3000000 -.0208500
0.4000000 -.0158000
0.5000000 -.0122500
0.6000000 -.0087000
0.7000000 -.0061500
0.8000000 -.0046000
0.9000000 -.0030500
0.9500000 -.0025200
1.0000000 0.0000000
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Polars for GOE 387 AIRFOIL (goe387-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe387-il | 50,000 | 9 | 6.1 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe387-il | 50,000 | 5 | 22.6 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe387-il | 100,000 | 9 | 43.6 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe387-il | 100,000 | 5 | 50.3 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe387-il | 200,000 | 9 | 71.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe387-il | 200,000 | 5 | 69.8 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe387-il | 500,000 | 9 | 101 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe387-il | 500,000 | 5 | 93 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe387-il | 1,000,000 | 9 | 122.5 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe387-il | 1,000,000 | 5 | 114.2 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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