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Numerical optimization of helicopter rotor blade design for active twist control

    Andrejs Kovalovs Affiliation
    ; Evgeny Barkanov Affiliation
    ; Sergejs Gluhihs Affiliation
DOI: https://doi.org/10.3846/16487788.2007.9635962

Abstract

The vibration of a helicopter has several different sources, such as the rotor, engine and transmission system. This creates a number of problems with performance, for example poor manoeuvrability, discomfort of the pilot, low fatigue life of the structural components, and, consequently, high operating costs.


First published online: 14 Oct 2010

Keyword : active twist, macro fibre composite (MFC), helicopter rotor blade, optimization

How to Cite
Kovalovs, A., Barkanov, E., & Gluhihs, S. (2007). Numerical optimization of helicopter rotor blade design for active twist control. Aviation, 11(3), 3-9. https://doi.org/10.3846/16487788.2007.9635962
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Sep 30, 2007
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This work is licensed under a Creative Commons Attribution 4.0 International License.