A Fixed-loaded Interface Component Mode Synthesis Method for Dynamic Analysis of a Folding Wing

DOI

10.2991/icaset-16.2016.1How to use a DOI?

Keywords

Folding wing, Component mode synthesis, Model reduction, Dynamic analysis

Abstract

A fixed-loaded interface component mode synthesis method is presented for carrying out a dynamic analysis for a folding wing. The present method has the advantages of the fixed interface method and loaded interface method, in which the effects of the elastic and inertia force at interfaces are included and the size of dynamic problem is highly reduced through elimination of interface coordinates. It is shown in the paper that the present method is able to predict the natural frequency accurately. Further, it can be integrated with the multibody dynamic code to perform the transient dynamic analysis during the morphing process.

Copyright

© 2016, 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/).

Download article (PDF)

TY  - CONF
AU  - Yingge Ni
AU  - Xiaopeng Wan
AU  - Meiying Zhao
PY  - 2016/05
DA  - 2016/05
TI  - A Fixed-loaded Interface Component Mode Synthesis Method for Dynamic Analysis of a Folding Wing
BT  - Proceedings of the 2016 6th International Conference on Applied Science, Engineering and Technology
PB  - Atlantis Press
SP  - 1
EP  - 7
SN  - 2352-5401
UR  - https://doi.org/10.2991/icaset-16.2016.1
DO  - 10.2991/icaset-16.2016.1
ID  - Ni2016/05
ER  -