GOE 529 AIRFOIL (goe529-il)
GOE 529 AIRFOIL - Gottingen 529 airfoil
| Details | Dat file | Parser | |
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(goe529-il) GOE 529 AIRFOIL Gottingen 529 airfoil Max thickness 9.7% at 29.9% chord. Max camber 5.8% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 529 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122600 0.0206400
0.0246300 0.0317800
0.0494500 0.0475700
0.0743100 0.0603500
0.0992000 0.0696400
0.1490200 0.0852100
0.1989000 0.0952900
0.2987900 0.1049400
0.3988000 0.1040900
0.4988900 0.0962400
0.5990600 0.0813900
0.6992600 0.0645400
0.7994900 0.0446900
0.8997300 0.0233500
0.9498600 0.0119200
1.0000000 0.0000000
0.0000000 0.0000000
0.0126100 -.0098500
0.0251300 -.0117100
0.0501400 -.0119200
0.0751200 -.0101400
0.1000900 -.0078500
0.1500300 -.0027700
0.1999800 0.0018000
0.2999100 0.0079500
0.3998700 0.0116000
0.4998600 0.0122500
0.5998700 0.0109000
0.6999000 0.0090500
0.7999300 0.0062000
0.8999600 0.0033500
0.9499800 0.0019200
1.0000000 0.0000000
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Polars for GOE 529 AIRFOIL (goe529-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe529-il | 50,000 | 9 | 12.9 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe529-il | 50,000 | 5 | 33.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe529-il | 100,000 | 9 | 54.8 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe529-il | 100,000 | 5 | 60 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe529-il | 200,000 | 9 | 81.4 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe529-il | 200,000 | 5 | 81.9 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe529-il | 500,000 | 9 | 114.6 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe529-il | 500,000 | 5 | 109 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe529-il | 1,000,000 | 9 | 138.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe529-il | 1,000,000 | 5 | 127.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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