GOE 598 AIRFOIL (goe598-il)
GOE 598 AIRFOIL - Gottingen 598 airfoil
| Details | Dat file | Parser | |
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(goe598-il) GOE 598 AIRFOIL Gottingen 598 airfoil Max thickness 6.5% at 39.8% chord. Max camber 1% at 49.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 598 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0121700 0.0084800
0.0244900 0.0129700
0.0492500 0.0189500
0.0740600 0.0239300
0.0989200 0.0274100
0.1487200 0.0323700
0.1985600 0.0363400
0.2984100 0.0402900
0.3983500 0.0417300
0.4984100 0.0401900
0.5986300 0.0346500
0.6988700 0.0276700
0.7992300 0.0195700
0.8995600 0.0110300
0.9497600 0.0060200
1.0000000 0.0010000
0.0000000 0.0000000
0.0128600 -.0089900
0.0254700 -.0119900
0.0506700 -.0170000
0.0757500 -.0190100
0.1008100 -.0205200
0.1509100 -.0230400
0.2009500 -.0240600
0.3009700 -.0246100
0.4009400 -.0236600
0.5008200 -.0207200
0.6006600 -.0167700
0.7005100 -.0128300
0.8003500 -.0088900
0.9001999 -.0049400
0.9501200 -.0029700
1.0000000 -.0010000
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Polars for GOE 598 AIRFOIL (goe598-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe598-il | 50,000 | 9 | 31.7 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe598-il | 50,000 | 5 | 30.5 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe598-il | 100,000 | 9 | 43.1 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe598-il | 100,000 | 5 | 40.4 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe598-il | 200,000 | 9 | 54.8 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe598-il | 200,000 | 5 | 48.6 at α=2.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe598-il | 500,000 | 9 | 66.9 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe598-il | 500,000 | 5 | 54.6 at α=2° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe598-il | 1,000,000 | 9 | 72.5 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe598-il | 1,000,000 | 5 | 60.8 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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