GOE 380 AIRFOIL (goe380-il)
GOE 380 AIRFOIL - Gottingen 380 airfoil
| Details | Dat file | Parser | |
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(goe380-il) GOE 380 AIRFOIL Gottingen 380 airfoil Max thickness 6.6% at 30% chord. Max camber 5.6% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 380 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0124500 0.0180300
0.0249300 0.0280600
0.0498900 0.0441200
0.0748600 0.0556900
0.0998400 0.0642500
0.1498100 0.0758700
0.1997900 0.0835000
0.2997800 0.0887500
0.3997800 0.0870000
0.4998000 0.0792500
0.5998300 0.0690000
0.6998600 0.0557500
0.7999000 0.0395000
0.8999500 0.0212500
0.9499700 0.0108700
1.0000000 0.0000000
0.0000000 0.0000000
0.0125100 -.0024700
0.0250100 -.0024400
0.0500000 0.0006200
0.0749900 0.0051900
0.0999700 0.0102500
0.1499600 0.0153700
0.1999500 0.0195000
0.2999400 0.0232500
0.3999400 0.0235000
0.4999500 0.0207500
0.5999600 0.0170000
0.6999700 0.0117500
0.7999800 0.0065000
0.9000000 0.0012500
0.9500000 0.0003700
1.0000000 0.0000000
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Polars for GOE 380 AIRFOIL (goe380-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe380-il | 50,000 | 9 | 31.1 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe380-il | 50,000 | 5 | 40.9 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe380-il | 100,000 | 9 | 54.4 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe380-il | 100,000 | 5 | 60 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe380-il | 200,000 | 9 | 75.6 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe380-il | 200,000 | 5 | 78 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe380-il | 500,000 | 9 | 103.4 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe380-il | 500,000 | 5 | 103.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe380-il | 1,000,000 | 9 | 125.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe380-il | 1,000,000 | 5 | 124.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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