GOE 407 AIRFOIL (goe407-il)
GOE 407 AIRFOIL - Gottingen 407 airfoil
| Details | Dat file | Parser | |
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(goe407-il) GOE 407 AIRFOIL Gottingen 407 airfoil Max thickness 9.5% at 29.9% chord. Max camber 4.8% at 39.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 407 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0123500 0.0218800
0.0247800 0.0325700
0.0496800 0.0474300
0.0746100 0.0579000
0.0995600 0.0660700
0.1494700 0.0797000
0.1994100 0.0880400
0.2993600 0.0950100
0.3993700 0.0946800
0.4994000 0.0889500
0.5994900 0.0768200
0.6995800 0.0622900
0.7997000 0.0452600
0.8998200 0.0267300
0.9498800 0.0141700
1.0000000 0.0000000
0.0000000 0.0000000
0.0125900 -.0132200
0.0251000 -.0142300
0.0500900 -.0135600
0.0750800 -.0112000
0.1000600 -.0094300
0.1500400 -.0053900
0.2000200 -.0024600
0.3000000 0.0004100
0.3999900 0.0008800
0.5000000 0.0001500
0.6000100 -.0007800
0.7000200 -.0028100
0.8000300 -.0047400
0.9000500 -.0067700
0.9500500 -.0055300
1.0000000 0.0000000
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Polars for GOE 407 AIRFOIL (goe407-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe407-il | 50,000 | 9 | 27.9 at α=10.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe407-il | 50,000 | 5 | 37.5 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe407-il | 100,000 | 9 | 56.2 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe407-il | 100,000 | 5 | 57.7 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe407-il | 200,000 | 9 | 79.4 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe407-il | 200,000 | 5 | 75.2 at α=3.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe407-il | 500,000 | 9 | 106.5 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe407-il | 500,000 | 5 | 95.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe407-il | 1,000,000 | 9 | 121.6 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe407-il | 1,000,000 | 5 | 114.1 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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