GOE 738 AIRFOIL (goe738-il)
GOE 738 AIRFOIL - Gottingen 738 airfoil
| Details | Dat file | Parser | |
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(goe738-il) GOE 738 AIRFOIL Gottingen 738 airfoil Max thickness 15.4% at 30% chord. Max camber 2.1% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 738 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0266700
0.0250000 0.0388400
0.0500000 0.0539800
0.0750000 0.0653100
0.1000000 0.0738500
0.1500000 0.0864200
0.2000000 0.0932000
0.3000000 0.0984500
0.4000000 0.0934000
0.5000000 0.0809500
0.6000000 0.0636000
0.7000000 0.0435500
0.8000000 0.0243000
0.9000000 0.0091500
0.9500000 0.0038200
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0218300
0.0250000 -.0298600
0.0500000 -.0389200
0.0750000 -.0444900
0.1000000 -.0486500
0.1500000 -.0531800
0.2000000 -.0553000
0.3000000 -.0559500
0.4000000 -.0536000
0.5000000 -.0488500
0.6000000 -.0419000
0.7000000 -.0333500
0.8000000 -.0233000
0.9000000 -.0128500
0.9500000 -.0071700
1.0000000 0.0000000
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Polars for GOE 738 AIRFOIL (goe738-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe738-il | 50,000 | 9 | 10.1 at α=-1° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe738-il | 50,000 | 5 | 23.4 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe738-il | 100,000 | 9 | 41.3 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe738-il | 100,000 | 5 | 44.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe738-il | 200,000 | 9 | 62.4 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe738-il | 200,000 | 5 | 61.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe738-il | 500,000 | 9 | 87.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe738-il | 500,000 | 5 | 79.3 at α=7.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe738-il | 1,000,000 | 9 | 102.9 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe738-il | 1,000,000 | 5 | 93.6 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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