GOE 528 AIRFOIL (goe528-il)
GOE 528 AIRFOIL - Gottingen 528 airfoil
| Details | Dat file | Parser | |
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(goe528-il) GOE 528 AIRFOIL Gottingen 528 airfoil Max thickness 12.5% at 29.8% chord. Max camber 6.2% at 39.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 528 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0120500 0.0301800
0.0243600 0.0423700
0.0491000 0.0597400
0.0739000 0.0731100
0.0987300 0.0849800
0.1484700 0.1017300
0.1983100 0.1124700
0.2981600 0.1224700
0.3981900 0.1209700
0.4983400 0.1109800
0.5985600 0.0959800
0.6988600 0.0759800
0.7992100 0.0524900
0.8995900 0.0274900
0.9497800 0.0147500
1.0000000 0.0000000
0.0000000 0.0000000
0.0126600 -.0108100
0.0252000 -.0131200
0.0502100 -.0142500
0.0752100 -.0138700
0.1002000 -.0130000
0.1501600 -.0107500
0.2001200 -.0080000
0.3000300 -.0020000
0.3999600 0.0030000
0.4999000 0.0065000
0.5998900 0.0075000
0.6998900 0.0075000
0.7999099 0.0060000
0.8999600 0.0030000
0.9499700 0.0017500
1.0000000 0.0000000
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Polars for GOE 528 AIRFOIL (goe528-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe528-il | 50,000 | 9 | 9 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe528-il | 50,000 | 5 | 29.8 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe528-il | 100,000 | 9 | 46.6 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe528-il | 100,000 | 5 | 55.7 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe528-il | 200,000 | 9 | 75.5 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe528-il | 200,000 | 5 | 77.6 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe528-il | 500,000 | 9 | 110.5 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe528-il | 500,000 | 5 | 106.7 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe528-il | 1,000,000 | 9 | 137.7 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe528-il | 1,000,000 | 5 | 128.9 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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