GOE 314 (HANSA-BRANDENBURG) AIRFOIL (goe314-il)
GOE 314 (HANSA-BRANDENBURG) AIRFOIL - Gottingen 314 (Hansa-Brandenburg) airfoil
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(goe314-il) GOE 314 (HANSA-BRANDENBURG) AIRFOIL Gottingen 314 (Hansa-Brandenburg) airfoil Max thickness 8% at 29.9% chord. Max camber 4.7% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 314 (HANSA-BRANDENBURG) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0121400 0.0204800
0.0245500 0.0306600
0.0493500 0.0439300
0.0741800 0.0558900
0.0990400 0.0654600
0.1488700 0.0769900
0.1987700 0.0835200
0.2987200 0.0870900
0.3987800 0.0826600
0.4989000 0.0746300
0.5990600 0.0641100
0.6992600 0.0505800
0.7994900 0.0349500
0.8997200 0.0190300
0.9498500 0.0103600
1.0000000 0.0000000
0.0000000 0.0000000
0.0127100 -.0130100
0.0252100 -.0143300
0.0501500 -.0107600
0.0751100 -.0073000
0.1000500 -.0037300
0.1499900 0.0007000
0.1999400 0.0040400
0.2999000 0.0067100
0.3999000 0.0069800
0.4999100 0.0058500
0.5999300 0.0046200
0.6999700 0.0018900
0.7999800 0.0002500
0.9005300 -.0010300
0.9500000 -.0002300
1.0000000 0.0000000
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Polars for GOE 314 (HANSA-BRANDENBURG) AIRFOIL (goe314-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe314-il | 50,000 | 9 | 28.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe314-il | 50,000 | 5 | 36.8 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe314-il | 100,000 | 9 | 48.7 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe314-il | 100,000 | 5 | 54.1 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe314-il | 200,000 | 9 | 70.5 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe314-il | 200,000 | 5 | 71.3 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe314-il | 500,000 | 9 | 98.3 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe314-il | 500,000 | 5 | 91 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe314-il | 1,000,000 | 9 | 117.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe314-il | 1,000,000 | 5 | 104.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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