GOE 610-B MOD. AIRFOIL (goe610bm-il)
GOE 610-B MOD. AIRFOIL - Gottingen 610-B MOD airfoil
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(goe610bm-il) GOE 610-B MOD. AIRFOIL Gottingen 610-B MOD airfoil Max thickness 7.7% at 30% chord. Max camber 5.5% at 40% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Lednicer format |
GOE 610-B MOD. AIRFOIL
15. 15.
0.0000000 0.0000000
0.0125000 0.0170900
0.0250000 0.0281800
0.0500000 0.0433500
0.1000000 0.0617000
0.1500000 0.0740500
0.2000000 0.0834000
0.3000000 0.0931000
0.4000000 0.0928000
0.5000000 0.0865000
0.6000000 0.0772000
0.7000000 0.0629000
0.8000000 0.0466000
0.9000000 0.0273000
1.0000000 0.0080000
0.0000000 0.0000000
0.0125000 -.0069100
0.0250000 -.0068300
0.0500000 -.0046500
0.1000000 -.0003000
0.1500000 0.0040500
0.2000000 0.0094000
0.3000000 0.0161000
0.4000000 0.0208000
0.5000000 0.0225000
0.6000000 0.0232000
0.7000000 0.0209000
0.8000000 0.0146000
0.9000000 0.0073000
1.0000000 0.0000000
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Polars for GOE 610-B MOD. AIRFOIL (goe610bm-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| goe610bm-il | 50,000 | 9 | 40.4 at α=8.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610bm-il | 50,000 | 5 | 43.4 at α=7.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610bm-il | 100,000 | 9 | 62.8 at α=7.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610bm-il | 100,000 | 5 | 63.5 at α=6.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610bm-il | 200,000 | 9 | 83.1 at α=6.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610bm-il | 200,000 | 5 | 82.3 at α=5.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610bm-il | 500,000 | 9 | 110.5 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610bm-il | 500,000 | 5 | 107.3 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| goe610bm-il | 1,000,000 | 9 | 130.3 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| goe610bm-il | 1,000,000 | 5 | 125 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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