Reducing aerodynamic vibration of rigid rotors with retreating side active control avoidance

Author:

LYU WeiLiang

Funder

Chinese Aeronautical Establishment Aeronautical Science Foundation

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Reference23 articles.

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2. Quackenbush TR, Wachspress DA. Next generation modeling technology for high speed rotorcraft. Washington, D.C.: NASA; 2007. Report No.: 07-15.

3. Johnson W. Influence of lift offset on rotorcraft performance. In: AHS specialist’s conference on aeromechanics; San Francisco, California; 2008.

4. A study of coaxial rotor aerodynamic interaction mechanism in hover with high-efficient trim model;Qi;Aerosp Sci Technol,2019

5. An offset hub active vibration control system for mitigating helicopter vibrations during power loss: simulation and experimental demonstration;Kakaley;Aerosp Sci Technol,2018

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