GOE 379 AIRFOIL (goe379-il)
GOE 379 AIRFOIL - Gottingen 379 airfoil
| Details | Dat file | Parser | |
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(goe379-il) GOE 379 AIRFOIL Gottingen 379 airfoil Max thickness 6.5% at 30% chord. Max camber 5.2% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 379 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124500 0.0150400
0.0249200 0.0240900
0.0498700 0.0381700
0.0748300 0.0487600
0.0998000 0.0578500
0.1497500 0.0700200
0.1997300 0.0782000
0.2997000 0.0845500
0.3997100 0.0834000
0.4997300 0.0767500
0.5997700 0.0666000
0.6998100 0.0529500
0.7998700 0.0368000
0.8999299 0.0191500
0.9499700 0.0098200
1.0000000 0.0000000
0.0000000 0.0000000
0.0125100 -.0039600
0.0250200 -.0044100
0.0500100 -.0018200
0.0749900 0.0017600
0.0999800 0.0053500
0.1499600 0.0110200
0.1999400 0.0157000
0.2999300 0.0200500
0.3999300 0.0214000
0.4999300 0.0192500
0.5999500 0.0151000
0.6999600 0.0104500
0.7999800 0.0048000
0.9000000 0.0001500
0.9500000 -.0011700
1.0000000 0.0000000
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Polars for GOE 379 AIRFOIL (goe379-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe379-il | 50,000 | 9 | 39.6 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe379-il | 50,000 | 5 | 41 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe379-il | 100,000 | 9 | 58.2 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe379-il | 100,000 | 5 | 60.3 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe379-il | 200,000 | 9 | 77.7 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe379-il | 200,000 | 5 | 79.1 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe379-il | 500,000 | 9 | 106 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe379-il | 500,000 | 5 | 103.8 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe379-il | 1,000,000 | 9 | 126.3 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe379-il | 1,000,000 | 5 | 121.5 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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