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/).

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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  -