Coupled CFD/CSD simulation of the helicopter main rotor in high-speed forward flight


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The helicopter main rotor in forward flight is considered in this paper. The results for rigid blades and elastic blades are compared by the method of coupled simulation. The influence of the structural damping coefficient on the blade in-flight deformation is also considered.

作者简介

F. Dehaeze

University of Liverpool

Email: info@pleiadesonline.com
英国, Liverpool, L69 3BX

G. Barakos

University of Glasgow

Email: info@pleiadesonline.com
英国, Glasgow, G12 8QQ

L. Garipova

Tupolev Kazan National Research Technical University

Email: info@pleiadesonline.com
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111 Tatarstan

A. Kusyumov

Tupolev Kazan National Research Technical University

Email: info@pleiadesonline.com
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111 Tatarstan

S. Mikhailov

Tupolev Kazan National Research Technical University

Email: info@pleiadesonline.com
俄罗斯联邦, ul. Karla Marksa 10, Kazan, 420111 Tatarstan

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