Dynamic and Elastic Response of Aircraft in Gust Loads
Yi Zhang, Lei Deng, Gang Sun, Xiangzheng Tu
Available Online June 2018.
- 10.2991/eame-18.2018.54How to use a DOI?
- gust load; aircraft; dynamic; aeroelasticity
Aeroelastic response of gust is always an important problem in flight quality assessment. In this study, structure and aerodynamic solvers based on Lagrange equation and Euler equation are coupled with loose coupling method. Elastic general-purpose airplane and a high-aspect-ratio transport airplane with elastic wings are simulated. The simulations proved the capacity of the method and studied the dynamic response in gust with different conditions.
- © 2018, 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/).
Cite this article
TY - CONF AU - Yi Zhang AU - Lei Deng AU - Gang Sun AU - Xiangzheng Tu PY - 2018/06 DA - 2018/06 TI - Dynamic and Elastic Response of Aircraft in Gust Loads BT - Proceedings of the 2018 3rd International Conference on Electrical, Automation and Mechanical Engineering (EAME 2018) PB - Atlantis Press SP - 256 EP - 261 SN - 2352-5401 UR - https://doi.org/10.2991/eame-18.2018.54 DO - 10.2991/eame-18.2018.54 ID - Zhang2018/06 ER -