GOE 563 AIRFOIL (goe563-il)
GOE 563 AIRFOIL - Gottingen 563 airfoil
| Details | Dat file | Parser | |
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(goe563-il) GOE 563 AIRFOIL Gottingen 563 airfoil Max thickness 8.9% at 29.8% chord. Max camber 2.2% at 49.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 563 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0119400 0.0159200
0.0241900 0.0228600
0.0488200 0.0332300
0.0735600 0.0406100
0.0983700 0.0459900
0.1480700 0.0542600
0.1978900 0.0595200
0.2977100 0.0645700
0.3976700 0.0656200
0.4977800 0.0626700
0.5980000 0.0562300
0.6983600 0.0462900
0.7988200 0.0333600
0.8993800 0.0174300
0.9496900 0.0087100
1.0000000 0.0000000
0.0000000 0.0000000
0.0129800 -.0135400
0.0256200 -.0175900
0.0507700 -.0217000
0.0758500 -.0238100
0.1008700 -.0244200
0.1508900 -.0251400
0.2008800 -.0248700
0.3008600 -.0243200
0.4007600 -.0212700
0.5006300 -.0177300
0.6005000 -.0141800
0.7003800 -.0106400
0.8002500 -.0070900
0.9001300 -.0035500
0.9500600 -.0017700
1.0000000 0.0000000
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Polars for GOE 563 AIRFOIL (goe563-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe563-il | 50,000 | 9 | 35.9 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe563-il | 50,000 | 5 | 36.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe563-il | 100,000 | 9 | 54.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe563-il | 100,000 | 5 | 51 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe563-il | 200,000 | 9 | 73.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe563-il | 200,000 | 5 | 64.2 at α=3.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe563-il | 500,000 | 9 | 95.4 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe563-il | 500,000 | 5 | 76.6 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe563-il | 1,000,000 | 9 | 105.6 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe563-il | 1,000,000 | 5 | 86.6 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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