GOE 447 AIRFOIL (goe447-il)
GOE 447 AIRFOIL - Gottingen 447 airfoil
| Details | Dat file | Parser | |
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(goe447-il) GOE 447 AIRFOIL Gottingen 447 airfoil Max thickness 12.7% at 29.7% chord. Max camber 8% at 39.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 447 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0120000 0.0252400
0.0242600 0.0376800
0.0488600 0.0578600
0.0735600 0.0732500
0.0982900 0.0870400
0.1479100 0.1061100
0.1976300 0.1200900
0.2972900 0.1377600
0.3972100 0.1418300
0.4972900 0.1374000
0.5975800 0.1228700
0.6980300 0.0999500
0.7986000 0.0709300
0.8992299 0.0390100
0.9495800 0.0213100
1.0000000 0.0016000
0.0000000 0.0000000
0.0128200 -.0162500
0.0253800 -.0192000
0.0503900 -.0198100
0.0753200 -.0163200
0.1002500 -.0129200
0.1501400 -.0071400
0.2000200 -.0008600
0.2997800 0.0112100
0.3996400 0.0184700
0.4996000 0.0204400
0.5996400 0.0182100
0.6997300 0.0137800
0.7998300 0.0088600
0.8999299 0.0033300
0.9499800 0.0011100
1.0000000 -.0016000
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Polars for GOE 447 AIRFOIL (goe447-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe447-il | 50,000 | 9 | 6.1 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe447-il | 50,000 | 5 | 16 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe447-il | 100,000 | 9 | 40 at α=12° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe447-il | 100,000 | 5 | 49.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe447-il | 200,000 | 9 | 84 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe447-il | 200,000 | 5 | 84.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe447-il | 500,000 | 9 | 129.4 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe447-il | 500,000 | 5 | 116.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe447-il | 1,000,000 | 9 | 161.3 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe447-il | 1,000,000 | 5 | 126.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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