GOE 289 (MVA 289) AIRFOIL (goe289-il)
GOE 289 (MVA 289) AIRFOIL - Gottingen 289 (MVA 289) airfoil
| Details | Dat file | Parser | |
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(goe289-il) GOE 289 (MVA 289) AIRFOIL Gottingen 289 (MVA 289) airfoil Max thickness 16.8% at 30% chord. Max camber 6.1% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 289 (MVA 289) AIRFOIL
17. 17.
0.0000000 0.0000000
0.0125000 0.0260100
0.0250000 0.0390100
0.0500000 0.0605200
0.0750000 0.0770400
0.1000000 0.0915500
0.1500000 0.1140800
0.2000000 0.1291000
0.3000000 0.1416500
0.4000000 0.1402000
0.5000000 0.1292500
0.6000000 0.1118000
0.7000000 0.0888500
0.8000000 0.0629000
0.9000000 0.0329500
0.9500000 0.0174700
1.0000000 0.0000000
0.0000000 0.0000000
0.0125000 -.0194900
0.0250000 -.0244900
0.0500000 -.0304700
0.0750000 -.0334600
0.1000000 -.0344500
0.1500000 -.0339200
0.2000000 -.0324000
0.3000000 -.0263500
0.4000000 -.0178000
0.5000000 -.0117500
0.6000000 -.0067000
0.7000000 -.0026500
0.8000000 -.0006000
0.9000000 -.0000500
0.9500000 -.0005200
1.0000000 0.0000000
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Polars for GOE 289 (MVA 289) AIRFOIL (goe289-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe289-il | 50,000 | 9 | 4.3 at α=11.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe289-il | 50,000 | 5 | 20.7 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe289-il | 100,000 | 9 | 38.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe289-il | 100,000 | 5 | 46.5 at α=6° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe289-il | 200,000 | 9 | 65.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe289-il | 200,000 | 5 | 64.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe289-il | 500,000 | 9 | 92.1 at α=5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe289-il | 500,000 | 5 | 87.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe289-il | 1,000,000 | 9 | 115.9 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe289-il | 1,000,000 | 5 | 109.2 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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