GOE 746 AIRFOIL (goe746-il)
GOE 746 AIRFOIL - Gottingen 746 airfoil
| Details | Dat file | Parser | |
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(goe746-il) GOE 746 AIRFOIL Gottingen 746 airfoil Max thickness 9.8% at 30% chord. Max camber 5% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 746 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0194900
0.0250000 0.0299700
0.0500000 0.0474500
0.0750000 0.0599200
0.1000000 0.0704000
0.1500000 0.0848500
0.2000000 0.0933000
0.3000000 0.0992000
0.4000000 0.0921000
0.5000000 0.0755000
0.6000000 0.0559000
0.7000000 0.0353000
0.8000000 0.0167000
0.9000000 0.0051000
0.9500000 0.0020500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0093100
0.0250000 -.0095200
0.0500000 -.0085500
0.0750000 -.0070700
0.1000000 -.0061000
0.1500000 -.0036500
0.2000000 -.0017000
0.3000000 0.0017000
0.4000000 0.0026000
0.5000000 0.0005000
0.6000000 -.0041000
0.7000000 -.0092000
0.8000000 -.0108000
0.9000000 -.0084000
0.9500000 -.0049500
1.0000000 0.0000000
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Polars for GOE 746 AIRFOIL (goe746-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe746-il | 50,000 | 9 | 7.9 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe746-il | 50,000 | 5 | 20.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe746-il | 100,000 | 9 | 46.3 at α=10° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe746-il | 100,000 | 5 | 49.1 at α=8.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe746-il | 200,000 | 9 | 73.4 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe746-il | 200,000 | 5 | 73.8 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe746-il | 500,000 | 9 | 106.3 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe746-il | 500,000 | 5 | 102.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe746-il | 1,000,000 | 9 | 129.6 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe746-il | 1,000,000 | 5 | 118.6 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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