GOE 369 AIRFOIL (goe369-il)
GOE 369 AIRFOIL - Gottingen 369 airfoil
| Details | Dat file | Parser | |
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(goe369-il) GOE 369 AIRFOIL Gottingen 369 airfoil Max thickness 5.9% at 30% chord. Max camber 5.4% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 369 AIRFOIL
17. 17.
0.0000000 0.0010000
0.0125000 0.0250000
0.0250000 0.0350000
0.0500000 0.0476400
0.0750000 0.0560000
0.1000000 0.0625000
0.1500000 0.0715000
0.2000000 0.0780000
0.3000000 0.0835000
0.4000000 0.0825000
0.5000000 0.0750000
0.6000000 0.0625000
0.7000000 0.0480000
0.8000000 0.0330000
0.9000000 0.0180000
0.9500000 0.0095000
1.0000000 0.0000000
0.0000000 0.0010000
0.0125000 0.0000000
0.0250000 0.0025000
0.0500000 0.0060000
0.0750000 0.0100000
0.1000000 0.0135000
0.1500000 0.0176400
0.2000000 0.0210400
0.3000000 0.0250000
0.4000000 0.0265000
0.5000000 0.0245000
0.6000000 0.0205000
0.7000000 0.0150000
0.8000000 0.0100000
0.9000000 0.0050000
0.9500000 0.0020000
1.0000000 0.0000000
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Polars for GOE 369 AIRFOIL (goe369-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe369-il | 50,000 | 9 | 37.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe369-il | 50,000 | 5 | 43.6 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe369-il | 100,000 | 9 | 59.2 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe369-il | 100,000 | 5 | 63.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe369-il | 200,000 | 9 | 80.2 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe369-il | 200,000 | 5 | 83 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe369-il | 500,000 | 9 | 105.9 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe369-il | 500,000 | 5 | 94.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe369-il | 1,000,000 | 9 | 121.8 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe369-il | 1,000,000 | 5 | 112.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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