GOE 389 AIRFOIL (goe389-il)
GOE 389 AIRFOIL - Gottingen 389 airfoil
| Details | Dat file | Parser | |
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(goe389-il) GOE 389 AIRFOIL Gottingen 389 airfoil Max thickness 10.3% at 29.8% chord. Max camber 4% at 39.8% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 389 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0121500 0.0171400
0.0244400 0.0279900
0.0491500 0.0421900
0.0739300 0.0532900
0.0987700 0.0611900
0.1485000 0.0743900
0.1983200 0.0833000
0.2981700 0.0906100
0.3982200 0.0884200
0.4983900 0.0821700
0.5985400 0.0723600
0.6988400 0.0574800
0.7991600 0.0415000
0.8995500 0.0223300
0.9497400 0.0127400
1.0000000 0.0010500
0.0000000 0.0000000
0.0127500 -.0124400
0.0253100 -.0153900
0.0503600 -.0179900
0.0753700 -.0185800
0.1003900 -.0191800
0.1503700 -.0186700
0.2003500 -.0171600
0.3002500 -.0125500
0.4001800 -.0089400
0.5001200 -.0058200
0.6000600 -.0028100
0.7000400 -.0017900
0.8000300 -.0013800
0.9000200 -.0009600
0.9500200 -.0009600
1.0000000 -.0010500
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Polars for GOE 389 AIRFOIL (goe389-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe389-il | 50,000 | 9 | 32.7 at α=10.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe389-il | 50,000 | 5 | 37.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe389-il | 100,000 | 9 | 55 at α=9° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe389-il | 100,000 | 5 | 56.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe389-il | 200,000 | 9 | 75.1 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe389-il | 200,000 | 5 | 73.4 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe389-il | 500,000 | 9 | 101.4 at α=6° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe389-il | 500,000 | 5 | 94.6 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe389-il | 1,000,000 | 9 | 119.7 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe389-il | 1,000,000 | 5 | 108.1 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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