GOE 286 AIRFOIL (goe286-il)
GOE 286 AIRFOIL - Gottingen 286 airfoil
| Details | Dat file | Parser | |
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(goe286-il) GOE 286 AIRFOIL Gottingen 286 airfoil Max thickness 9.4% at 29.9% chord. Max camber 4.1% at 29.9% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 286 AIRFOIL
17. 17.
0.0000000 0.0000000
0.0122500 0.0207500
0.0246200 0.0315000
0.0494500 0.0447000
0.0743100 0.0568100
0.0992200 0.0636100
0.1490700 0.0759200
0.1989800 0.0836300
0.2989300 0.0877500
0.3989700 0.0842700
0.4990600 0.0766900
0.5992100 0.0644100
0.6993700 0.0520300
0.7995600 0.0362500
0.8997600 0.0197800
0.9498800 0.0101900
1.0000000 0.0025000
0.0000000 0.0000000
0.0126400 -.0116500
0.0251600 -.0131900
0.0501700 -.0140900
0.0751600 -.0132800
0.1001500 -.0122800
0.1501200 -.0099700
0.2001000 -.0081600
0.3000700 -.0057400
0.4000400 -.0033200
0.5000300 -.0027000
0.6000300 -.0020800
0.7000300 -.0020600
0.8000400 -.0031400
0.9000400 -.0031200
0.9500400 -.0031100
1.0000000 -.0025000
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Polars for GOE 286 AIRFOIL (goe286-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe286-il | 50,000 | 9 | 27.9 at α=8° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe286-il | 50,000 | 5 | 37.6 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe286-il | 100,000 | 9 | 52.2 at α=8.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe286-il | 100,000 | 5 | 54.5 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe286-il | 200,000 | 9 | 72.3 at α=7.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe286-il | 200,000 | 5 | 65.5 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe286-il | 500,000 | 9 | 83.6 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe286-il | 500,000 | 5 | 78.8 at α=6.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe286-il | 1,000,000 | 9 | 95.3 at α=6.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe286-il | 1,000,000 | 5 | 89.9 at α=7° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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