GOE 342 AIRFOIL (goe342-il)
GOE 342 AIRFOIL - Gottingen 342 airfoil
| Details | Dat file | Parser | |
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(goe342-il) GOE 342 AIRFOIL Gottingen 342 airfoil Max thickness 5.4% at 20% chord. Max camber 6.2% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 342 AIRFOIL
16. 16.
0.0000000 0.0000000
0.0125000 0.0201000
0.0250000 0.0292000
0.0500000 0.0414000
0.0750000 0.0506000
0.1000000 0.0578000
0.1500000 0.0702000
0.2000000 0.0786000
0.3000000 0.0854000
0.4000000 0.0872000
0.5000000 0.0850000
0.6000000 0.0778000
0.7000000 0.0636000
0.8000000 0.0464000
0.9000000 0.0262000
1.0000000 0.0030000
0.0000000 0.0000000
0.0125000 -.0079000
0.0250000 -.0058000
0.0500000 0.0004000
0.0750000 0.0046000
0.1000000 0.0098000
0.1500000 0.0177000
0.2000000 0.0246000
0.3000000 0.0334000
0.4000000 0.0372000
0.5000000 0.0375000
0.6000000 0.0358000
0.7000000 0.0306000
0.8000000 0.0224000
0.9000000 0.0122000
1.0000000 0.0000000
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Polars for GOE 342 AIRFOIL (goe342-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe342-il | 50,000 | 9 | 44.4 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe342-il | 50,000 | 5 | 47.8 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe342-il | 100,000 | 9 | 71.3 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe342-il | 100,000 | 5 | 71.4 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe342-il | 200,000 | 9 | 99.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe342-il | 200,000 | 5 | 85.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe342-il | 500,000 | 9 | 109.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe342-il | 500,000 | 5 | 105.8 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe342-il | 1,000,000 | 9 | 130.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe342-il | 1,000,000 | 5 | 111.7 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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