GOE 515 AIRFOIL (goe515-il)
GOE 515 AIRFOIL - Gottingen 515 airfoil
| Details | Dat file | Parser | |
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(goe515-il) GOE 515 AIRFOIL Gottingen 515 airfoil Max thickness 8.5% at 30% chord. Max camber 2.8% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 515 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0153200
0.0250000 0.0226400
0.0500000 0.0327700
0.0750000 0.0404100
0.1000000 0.0460500
0.1500000 0.0548300
0.2000000 0.0616000
0.3000000 0.0681500
0.4000000 0.0692000
0.5000000 0.0662500
0.6000000 0.0588000
0.7000000 0.0478500
0.8000000 0.0334000
0.9000000 0.0174500
0.9500000 0.0087300
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0131800
0.0250000 -.0178600
0.0500000 -.0227300
0.0750000 -.0245900
0.1000000 -.0244500
0.1500000 -.0231800
0.2000000 -.0209000
0.3000000 -.0163500
0.4000000 -.0133000
0.5000000 -.0107500
0.6000000 -.0097000
0.7000000 -.0081500
0.8000000 -.0071000
0.9000000 -.0045500
0.9500000 -.0027800
1.0000000 0.0000000
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Polars for GOE 515 AIRFOIL (goe515-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe515-il | 50,000 | 9 | 37.6 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe515-il | 50,000 | 5 | 37.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe515-il | 100,000 | 9 | 56.8 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe515-il | 100,000 | 5 | 54.9 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe515-il | 200,000 | 9 | 77.2 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe515-il | 200,000 | 5 | 71 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe515-il | 500,000 | 9 | 103.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe515-il | 500,000 | 5 | 88 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe515-il | 1,000,000 | 9 | 119 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe515-il | 1,000,000 | 5 | 95.1 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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