Aerodynamic Performance Analysis of Trailing Edge Serrations on a Wells Turbine
The primary objective of this investigation was to explore the aerodynamic impact of adding trailing edge serrations to a Wells turbine. The baseline turbine consists of eight NACA 0015 blades. The blade chord length was 0.125 m and the span was 0.100 m. Two modified serrated blade configurations we...
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| Format: | Artigo |
| Sprache: | Inglês |
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MDPI AG
2022-11-01
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| Schriftenreihe: | Energies |
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| Online-Zugang: | https://www.mdpi.com/1996-1073/15/23/9075 |
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