Gust Response Characteristics of Helicopter Rotor Blade

DOI

10.2991/mmeceb-15.2016.192How to use a DOI?

Keywords

helicopter; rotor blade; gust response

Abstract

The deformation of blades effected by gust would endanger the safety of wind turbine. Based on blades elastic deformation theory ,We established a model of blades rotation transient response ,studied the characteristics of blades transient response effected by gust, and confirmed the procedure of blades response to gust.

Copyright

© 2016, the Authors. Published by Atlantis Press.

Open Access

This is an open access article distributed under the CC BY-NC license (http://creativecommons.org/licenses/by-nc/4.0/).

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TY  - CONF
AU  - Hong-ru Ma
AU  - Wen-Sheng Sun
AU  - Zhi-tao Mu
AU  - Guang-yao Yan
PY  - 2015/12
DA  - 2015/12
TI  - Gust Response Characteristics of Helicopter Rotor Blade
BT  - Proceedings of the 2015 2nd International Conference on Machinery, Materials Engineering, Chemical Engineering and Biotechnology
PB  - Atlantis Press
SP  - 957
EP  - 960
SN  - 2352-5401
UR  - https://doi.org/10.2991/mmeceb-15.2016.192
DO  - 10.2991/mmeceb-15.2016.192
ID  - Ma2015/12
ER  -