GOE 256 (JUNKERS E) AIRFOIL (goe256-il)
GOE 256 (JUNKERS E) AIRFOIL - Gottingen 256 (JUNKERS E) airfoil
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(goe256-il) GOE 256 (JUNKERS E) AIRFOIL Gottingen 256 (JUNKERS E) airfoil Max thickness 16% at 29.6% chord. Max camber 4.7% at 39.6% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 256 (JUNKERS E) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0117200 0.0248700
0.0238300 0.0375400
0.0482000 0.0575100
0.0727500 0.0719700
0.0974100 0.0830400
0.1468700 0.1000900
0.1964700 0.1129400
0.2960900 0.1252500
0.3960700 0.1258800
0.4962600 0.1197100
0.5966500 0.1071500
0.6973000 0.0864900
0.7980800 0.0614400
0.8989900 0.0323900
0.9494600 0.0173700
1.0000000 0.0012500
0.0000000 0.0000000
0.0131900 -.0220900
0.0258900 -.0283900
0.0510400 -.0334000
0.0760900 -.0348200
0.1011100 -.0356400
0.1511300 -.0362800
0.2011400 -.0365100
0.3010800 -.0345900
0.4009800 -.0314700
0.5008900 -.0283500
0.6007900 -.0252300
0.7006900 -.0221000
0.8005900 -.0189800
0.9003800 -.0120600
0.9502000 -.0064100
1.0000000 -.0012500
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Polars for GOE 256 (JUNKERS E) AIRFOIL (goe256-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe256-il | 50,000 | 9 | 6.2 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe256-il | 50,000 | 5 | 22.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe256-il | 100,000 | 9 | 45.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe256-il | 100,000 | 5 | 48.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe256-il | 200,000 | 9 | 69.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe256-il | 200,000 | 5 | 64.5 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe256-il | 500,000 | 9 | 92.6 at α=2.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe256-il | 500,000 | 5 | 86.2 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe256-il | 1,000,000 | 9 | 112.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe256-il | 1,000,000 | 5 | 103.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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