Dynamic and Elastic Response of Aircraft in Gust Loads

DOI

10.2991/eame-18.2018.54How to use a DOI?

Keywords

gust load; aircraft; dynamic; aeroelasticity

Abstract

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.

Copyright

© 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/).

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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  -