Modelling, Parametric Study, and Optimisation of 3D Model-Scale Helicopter’s Rotor Blade with Piezoelectric Actuators
The concept of active blade twisting as a method for reducing helicopter noise and vibration during flight is presented. Active twisting is achieved through piezoelectric actuators embedded in the blade skin, which generate dynamic twist when subjected to an electric field. Such dynamic deformation...
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
MDPI AG
2026-01-01
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| Col·lecció: | Applied Sciences |
| Matèries: | |
| Accés en línia: | https://www.mdpi.com/2076-3417/16/3/1319 |
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