GOE 613 AIRFOIL (goe613-il)
GOE 613 AIRFOIL - Gottingen 613 airfoil
| Details | Dat file | Parser | |
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(goe613-il) GOE 613 AIRFOIL Gottingen 613 airfoil Max thickness 10.3% at 30% chord. Max camber 4.1% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 613 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0181900
0.0250000 0.0293900
0.0500000 0.0457700
0.0750000 0.0576600
0.1000000 0.0665500
0.1500000 0.0793200
0.2000000 0.0866000
0.3000000 0.0921500
0.4000000 0.0912000
0.5000000 0.0852500
0.6000000 0.0763000
0.7000000 0.0623500
0.8000000 0.0454000
0.9000000 0.0244500
0.9500000 0.0132200
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0118100
0.0250000 -.0141100
0.0500000 -.0142300
0.0750000 -.0143400
0.1000000 -.0139500
0.1500000 -.0131700
0.2000000 -.0124000
0.3000000 -.0108500
0.4000000 -.0093000
0.5000000 -.0077500
0.6000000 -.0062000
0.7000000 -.0046500
0.8000000 -.0031000
0.9000000 -.0015500
0.9500000 -.0007800
1.0000000 0.0000000
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Polars for GOE 613 AIRFOIL (goe613-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe613-il | 50,000 | 9 | 30.3 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe613-il | 50,000 | 5 | 37 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe613-il | 100,000 | 9 | 53.3 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe613-il | 100,000 | 5 | 52.8 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe613-il | 200,000 | 9 | 72.3 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe613-il | 200,000 | 5 | 67.9 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe613-il | 500,000 | 9 | 93.8 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe613-il | 500,000 | 5 | 88.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe613-il | 1,000,000 | 9 | 112 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe613-il | 1,000,000 | 5 | 106 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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