GOE 274 (DAIMLER V) AIRFOIL (goe274-il)
GOE 274 (DAIMLER V) AIRFOIL - Gottingen 274 (DAIMLER V) airfoil
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(goe274-il) GOE 274 (DAIMLER V) AIRFOIL Gottingen 274 (DAIMLER V) airfoil Max thickness 8.7% at 29.9% chord. Max camber 4.8% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 274 (DAIMLER V) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123600 0.0201800
0.0247900 0.0310700
0.0496800 0.0481300
0.0746000 0.0592000
0.0995400 0.0684700
0.1494700 0.0796000
0.1994200 0.0865400
0.2993900 0.0917100
0.3994000 0.0893800
0.4994400 0.0834500
0.5994900 0.0755200
0.6995700 0.0638900
0.7996700 0.0485600
0.8998100 0.0289300
0.9498900 0.0170600
1.0000000 0.0040000
0.0000000 0.0000000
0.0125700 -.0106200
0.0250700 -.0099300
0.0500400 -.0060600
0.0750300 -.0043000
0.1000200 -.0025300
0.1499900 0.0008000
0.1999800 0.0026400
0.2999700 0.0052100
0.3999500 0.0074800
0.4999500 0.0081500
0.5999400 0.0082200
0.6999600 0.0062900
0.7999700 0.0042600
0.8999900 0.0014300
0.9500000 -.0006300
1.0000000 -.0040000
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Polars for GOE 274 (DAIMLER V) AIRFOIL (goe274-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe274-il | 50,000 | 9 | 37.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe274-il | 50,000 | 5 | 40.7 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe274-il | 100,000 | 9 | 55.8 at α=3° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe274-il | 100,000 | 5 | 57 at α=5.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe274-il | 200,000 | 9 | 73.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe274-il | 200,000 | 5 | 73.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe274-il | 500,000 | 9 | 99 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe274-il | 500,000 | 5 | 92.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe274-il | 1,000,000 | 9 | 115.1 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe274-il | 1,000,000 | 5 | 105.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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