GOE 514 AIRFOIL (goe514-il)
GOE 514 AIRFOIL - Gottingen 514 airfoil
| Details | Dat file | Parser | |
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(goe514-il) GOE 514 AIRFOIL Gottingen 514 airfoil Max thickness 16.6% at 19.7% chord. Max camber 6.4% at 39.7% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 514 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0118100 0.0322500
0.0239600 0.0485200
0.0484400 0.0725400
0.0730500 0.0905700
0.0977700 0.1036000
0.1473500 0.1231700
0.1970800 0.1357400
0.2968900 0.1448800
0.3969500 0.1420300
0.4971300 0.1336900
0.5974400 0.1188500
0.6976500 0.0987800
0.7984200 0.0736700
0.8991400 0.0398300
0.9495500 0.0209200
1.0000000 0.0000000
0.0000000 0.0000000
0.0127500 -.0117300
0.0253900 -.0179500
0.0505500 -.0254100
0.0756300 -.0293700
0.1007000 -.0323400
0.1506900 -.0322600
0.2006400 -.0296900
0.3004200 -.0195400
0.4002800 -.0128900
0.5003200 -.0147400
0.6004400 -.0205900
0.7004400 -.0204400
0.8003700 -.0172900
0.9002301 -.0106500
0.9501300 -.0060700
1.0000000 0.0000000
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Polars for GOE 514 AIRFOIL (goe514-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe514-il | 50,000 | 9 | 7.2 at α=2.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe514-il | 50,000 | 5 | 26.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe514-il | 100,000 | 9 | 45.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe514-il | 100,000 | 5 | 41.9 at α=6.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe514-il | 200,000 | 9 | 57.2 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe514-il | 200,000 | 5 | 51.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe514-il | 500,000 | 9 | 69.2 at α=6.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe514-il | 500,000 | 5 | 64.7 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe514-il | 1,000,000 | 9 | 84.1 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe514-il | 1,000,000 | 5 | 78.1 at α=9° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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