GOE 418 AIRFOIL (goe418-il)
GOE 418 AIRFOIL - Gottingen 418 airfoil
| Details | Dat file | Parser | |
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(goe418-il) GOE 418 AIRFOIL Gottingen 418 airfoil Max thickness 12.7% at 20% chord. Max camber 5.1% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 418 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0344600
0.0250000 0.0459300
0.0500000 0.0628500
0.0750000 0.0747700
0.1000000 0.0827000
0.1500000 0.0955500
0.2000000 0.1044000
0.3000000 0.1111000
0.4000000 0.1088000
0.5000000 0.0985000
0.6000000 0.0832000
0.7000000 0.0659000
0.8000000 0.0456000
0.9000000 0.0233000
0.9500000 0.0121500
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0195400
0.0250000 -.0270700
0.0500000 -.0331500
0.0750000 -.0342200
0.1000000 -.0323000
0.1500000 -.0274500
0.2000000 -.0226000
0.3000000 -.0129000
0.4000000 -.0072000
0.5000000 -.0035000
0.6000000 -.0018000
0.7000000 -.0011000
0.8000000 0.0006000
0.9000000 0.0003000
0.9500000 0.0001500
1.0000000 0.0000000
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Polars for GOE 418 AIRFOIL (goe418-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe418-il | 50,000 | 9 | 12.5 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe418-il | 50,000 | 5 | 32.3 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe418-il | 100,000 | 9 | 52.6 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe418-il | 100,000 | 5 | 54 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe418-il | 200,000 | 9 | 75.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe418-il | 200,000 | 5 | 71.6 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe418-il | 500,000 | 9 | 101.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe418-il | 500,000 | 5 | 90.2 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe418-il | 1,000,000 | 9 | 117.7 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe418-il | 1,000,000 | 5 | 92.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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