GOE 484 AIRFOIL (goe484-il)
GOE 484 AIRFOIL - Gottingen 484 airfoil
Details | Dat file | Parser | |
(goe484-il) GOE 484 AIRFOIL Gottingen 484 airfoil Max thickness 6.3% at 30% chord. Max camber 5% at 50% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 484 AIRFOIL 16. 16. 0.0000000 0.0000000 0.0125000 0.0171500 0.0250000 0.0233000 0.0500000 0.0321000 0.0750000 0.0399000 0.1000000 0.0467000 0.1500000 0.0578000 0.2000000 0.0654000 0.3000000 0.0751000 0.4000000 0.0793000 0.5000000 0.0765000 0.6000000 0.0697000 0.7000000 0.0598000 0.8000000 0.0441000 0.9000000 0.0248000 1.0000000 0.0000000 0.0000000 0.0000000 0.0125000 -.0115500 0.0250000 -.0122000 0.0500000 -.0115000 0.0750000 -.0096000 0.1000000 -.0068000 0.1500000 -.0002000 0.2000000 0.0054000 0.3000000 0.0126000 0.4000000 0.0188000 0.5000000 0.0225000 0.6000000 0.0242000 0.7000000 0.0219000 0.8000000 0.0171000 0.9000000 0.0088000 1.0000000 0.0000000 |
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Similar airfoils
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Polars for GOE 484 AIRFOIL (goe484-il)
Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
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goe484-il | 50,000 | 9 | 45 at α=5.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
goe484-il | 50,000 | 5 | 44.4 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
goe484-il | 100,000 | 9 | 67.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
goe484-il | 100,000 | 5 | 65.4 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
goe484-il | 200,000 | 9 | 93.3 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
goe484-il | 200,000 | 5 | 86.4 at α=2.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
goe484-il | 500,000 | 9 | 128 at α=1.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
goe484-il | 500,000 | 5 | 93.4 at α=2.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
goe484-il | 1,000,000 | 9 | 136.7 at α=2.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
goe484-il | 1,000,000 | 5 | 92.7 at α=1.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
Reynolds number calculator |