Proceedings of the 2018 3rd International Conference on Electrical, Automation and Mechanical Engineering (EAME 2018)

Dynamic and Elastic Response of Aircraft in Gust Loads

Authors
Yi Zhang, Lei Deng, Gang Sun, Xiangzheng Tu
Corresponding Author
Yi Zhang
Available Online June 2018.
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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Volume Title
Proceedings of the 2018 3rd International Conference on Electrical, Automation and Mechanical Engineering (EAME 2018)
Series
Advances in Engineering Research
Publication Date
June 2018
ISBN
978-94-6252-538-2
ISSN
2352-5401
DOI
10.2991/eame-18.2018.54How to use a DOI?
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/).

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  -