GOE 285 AIRFOIL (goe285-il)
GOE 285 AIRFOIL - Gottingen 285 airfoil
| Details | Dat file | Parser | |
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(goe285-il) GOE 285 AIRFOIL Gottingen 285 airfoil Max thickness 11.7% at 30% chord. Max camber 3.7% at 30% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 285 AIRFOIL
18. 18.
0.0000000 0.0000000
0.0125000 0.0251200
0.0250000 0.0344400
0.0500000 0.0495800
0.0750000 0.0607300
0.1000000 0.0695700
0.1500000 0.0836600
0.2000000 0.0905400
0.2500000 0.0942200
0.3000000 0.0958100
0.4000000 0.0930800
0.5000000 0.0861500
0.6000000 0.0744200
0.7000000 0.0602900
0.8000000 0.0431600
0.9000000 0.0249300
0.9500000 0.0147200
1.0000000 0.0030000
0.0000000 0.0000000
0.0125000 -.0167800
0.0250000 -.0210600
0.0500000 -.0254200
0.0750000 -.0264700
0.1000000 -.0266300
0.1500000 -.0253400
0.2000000 -.0240600
0.2500000 -.0227700
0.3000000 -.0214900
0.4000000 -.0189200
0.5000000 -.0163500
0.6000000 -.0137800
0.7000000 -.0112100
0.8000000 -.0086400
0.9000000 -.0051700
0.9500000 -.0027800
1.0000000 0.0000000
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Polars for GOE 285 AIRFOIL (goe285-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe285-il | 50,000 | 9 | 26.1 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe285-il | 50,000 | 5 | 34.6 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe285-il | 100,000 | 9 | 47.2 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe285-il | 100,000 | 5 | 50.1 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe285-il | 200,000 | 9 | 65.2 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe285-il | 200,000 | 5 | 65.2 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe285-il | 500,000 | 9 | 89.3 at α=8.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe285-il | 500,000 | 5 | 87 at α=7.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe285-il | 1,000,000 | 9 | 109.1 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe285-il | 1,000,000 | 5 | 103.5 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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