GOE 377 AIRFOIL (goe377-il)
GOE 377 AIRFOIL - Gottingen 377 airfoil
| Details | Dat file | Parser | |
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(goe377-il) GOE 377 AIRFOIL Gottingen 377 airfoil Max thickness 6.5% at 30% chord. Max camber 3.9% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 377 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0145700
0.0250000 0.0226500
0.0500000 0.0338000
0.0750000 0.0429500
0.1000000 0.0496000
0.1500000 0.0594000
0.2000000 0.0652000
0.3000000 0.0703000
0.4000000 0.0704000
0.5000000 0.0660000
0.6000000 0.0586000
0.7000000 0.0482000
0.8000000 0.0348000
0.9000000 0.0184000
0.9500000 0.0097000
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0064200
0.0250000 -.0073500
0.0500000 -.0062000
0.0750000 -.0045500
0.1000000 -.0029000
0.1500000 -.0001000
0.2000000 0.0027000
0.3000000 0.0058000
0.4000000 0.0074000
0.5000000 0.0060000
0.6000000 0.0036000
0.7000000 0.0022000
0.8000000 0.0003000
0.9000000 -.0011000
0.9500000 -.0013000
1.0000000 0.0000000
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Polars for GOE 377 AIRFOIL (goe377-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe377-il | 50,000 | 9 | 37.9 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe377-il | 50,000 | 5 | 41 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe377-il | 100,000 | 9 | 57.3 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe377-il | 100,000 | 5 | 58.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe377-il | 200,000 | 9 | 77.9 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe377-il | 200,000 | 5 | 73.9 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe377-il | 500,000 | 9 | 101.5 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe377-il | 500,000 | 5 | 91.7 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe377-il | 1,000,000 | 9 | 115.8 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe377-il | 1,000,000 | 5 | 105.2 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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