Abstract
A blade aerodynamic design method for a 1MW stall-regulated wind turbine based on Schmitz theory was presented. To aquire optimum aerodynamic performance and satisfy strength s conditions, 6 airfoils were selected acording to specified rules. The blade tip, blade root and the conections of diffirent airfoils were processed to satisfy technics and real situations. To account for the invalidation of schmitz theory at low or high wind speed, the schmitz theory was amended to calculate the partial load character of designed wind turbine, in which swirl losses, airfoil losses, tip losses were taken into consideration. The blade design results and partial load characters are in good agreement with real wind turbine.
| Original language | English |
|---|---|
| Pages (from-to) | 122-128 |
| Number of pages | 7 |
| Journal | Taiyangneng Xuebao/Acta Energiae Solaris Sinica |
| Volume | 30 |
| Issue number | 1 |
| State | Published - Jan 2009 |
UN SDGs
This output contributes to the following UN Sustainable Development Goals (SDGs)
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SDG 7 Affordable and Clean Energy
Keywords
- Airfoil
- Blade tip speed ratio
- Chord length
- Schmitz theory
- Twist angle
- Wind turbine
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