Aeroelasticity Analysis of High-aspect-ratio Composite Wing
- DOI
- 10.2991/itms-15.2015.114How to use a DOI?
- Keywords
- high aspect ratio; composite; fluid structure interaction; pneumatic elasticity
- Abstract
The pneumatic elastic model establishing and analysis of the high-aspect-ratio composite wing is an important task for the long-endurance aircraft’s design. The pneumatic elastic analysis theory and fluid-structure interaction(FSI) analysis method are applied in this paper to establish the structured finite element model for the high-aspect-ratio composite wing. Based on the analysis of initialized static model, the software MpCCI is used to analyze the model with the bidirectional FSI theory, and discuss the pneumatic elasticity characteristics of the wing model in the coupling state. And the relative structure and flow field parameters are supported.
- Copyright
- © 2015, 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 - K.X. Liu AU - W. Zhou AU - X.R. Wang PY - 2015/11 DA - 2015/11 TI - Aeroelasticity Analysis of High-aspect-ratio Composite Wing BT - Proceedings of the 2015 International Conference on Industrial Technology and Management Science PB - Atlantis Press SP - 474 EP - 477 SN - 2352-538X UR - https://doi.org/10.2991/itms-15.2015.114 DO - 10.2991/itms-15.2015.114 ID - Liu2015/11 ER -