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A Methodology of Resonance Avoidance for Helicopter Rotor Blade Considering the Stiffness Characteristics of a Torsion-Type Elastic Hub

Published Online: 2024-10-04

Published Print: 2024-06

Authors

Nikolaev, S. E.
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Text and Data Mining valid from 2024-06-01

Version of Record valid from 2024-06-01
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Article History

Received: 11 June 2024

Revised: 19 June 2024

Accepted: 19 June 2024

First Online: 4 October 2024

CONFLICT OF INTEREST

: The author of this work declares that he has no conflicts of interest.

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