GOE 564 AIRFOIL (goe564-il)
GOE 564 AIRFOIL - Gottingen 564 airfoil
| Details | Dat file | Parser | |
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(goe564-il) GOE 564 AIRFOIL Gottingen 564 airfoil Max thickness 8.2% at 30% chord. Max camber 2.7% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 564 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0162900
0.0250000 0.0235800
0.0500000 0.0346500
0.0750000 0.0417300
0.1000000 0.0478000
0.1500000 0.0554500
0.2000000 0.0601000
0.3000000 0.0659000
0.4000000 0.0672000
0.5000000 0.0645000
0.6000000 0.0578000
0.7000000 0.0491000
0.8000000 0.0359000
0.9000000 0.0202000
0.9500000 0.0108500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0117100
0.0250000 -.0154300
0.0500000 -.0193500
0.0750000 -.0207800
0.1000000 -.0207000
0.1500000 -.0195500
0.2000000 -.0184000
0.3000000 -.0161000
0.4000000 -.0138000
0.5000000 -.0115000
0.6000000 -.0092000
0.7000000 -.0069000
0.8000000 -.0046000
0.9000000 -.0023000
0.9500000 -.0011500
1.0000000 0.0000000
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Polars for GOE 564 AIRFOIL (goe564-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe564-il | 50,000 | 9 | 37.1 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 50,000 | 5 | 37.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 100,000 | 9 | 56 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 100,000 | 5 | 52.6 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 200,000 | 9 | 75.4 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 200,000 | 5 | 65.6 at α=3° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 500,000 | 9 | 95.7 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 500,000 | 5 | 77.6 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe564-il | 1,000,000 | 9 | 103.8 at α=2° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe564-il | 1,000,000 | 5 | 89.2 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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