GOE 414 AIRFOIL (goe414-il)
GOE 414 AIRFOIL - Gottingen 414 airfoil
| Details | Dat file | Parser | |
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(goe414-il) GOE 414 AIRFOIL Gottingen 414 airfoil Max thickness 13.6% at 29.7% chord. Max camber 5.3% at 39.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 414 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0119600 0.0190400
0.0241500 0.0300800
0.0486400 0.0480700
0.0732500 0.0618700
0.0979400 0.0729700
0.1474100 0.0916600
0.1970700 0.1037700
0.2966700 0.1177800
0.3966700 0.1179100
0.4968400 0.1117400
0.5972200 0.0984700
0.6977100 0.0811100
0.7983500 0.0583500
0.8991200 0.0313000
0.9495400 0.0162200
1.0000000 0.0010500
0.0000000 0.0000000
0.0128500 -.0124400
0.0254800 -.0168800
0.0506400 -.0225700
0.0757000 -.0246600
0.1007200 -.0253500
0.1507100 -.0250400
0.2006700 -.0236300
0.3005100 -.0181100
0.4003600 -.0126900
0.5002600 -.0092700
0.6002000 -.0070400
0.7001500 -.0052200
0.8001100 -.0040000
0.9000800 -.0028700
0.9500700 -.0024600
1.0000000 -.0010500
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Polars for GOE 414 AIRFOIL (goe414-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe414-il | 50,000 | 9 | 8.6 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe414-il | 50,000 | 5 | 28.7 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe414-il | 100,000 | 9 | 52.1 at α=9.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe414-il | 100,000 | 5 | 54.6 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe414-il | 200,000 | 9 | 74.5 at α=7° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe414-il | 200,000 | 5 | 73 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe414-il | 500,000 | 9 | 100 at α=7.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe414-il | 500,000 | 5 | 97 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe414-il | 1,000,000 | 9 | 124.9 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe414-il | 1,000,000 | 5 | 119 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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