Finite Element Method Based Modeling of a Flexible Wing Structure
F. Svoboda, M. Hromčík
Czech Technical University in Prague
Abstract
The finite element based structural model of a flexible wing is presented. The structural model will be a part of a servoelastic wing used for flutter analysis and designing flutter suppression control systems. It also allows modal analysis of a wing with given parameters. A finite element model consists of Euler-Bernoulli beams joined together. This approach is able to reach high accuracy and various properties of a particular wing element can be modeled.
Full paper
Session
Modelling, Simulation, and Identification of Processes (Poster)
Reference
Svoboda, F.; Hromčík, M.: Finite Element Method Based Modeling of a Flexible Wing Structure. Editors: Fikar, M. and Kvasnica, M., In Proceedings of the 2017 21st International Conference on Process Control (PC), Štrbské Pleso, Slovakia, June 6 – 9, 222–227, 2017.
BibTeX
| @inProceedings{pc2017-037, | ||
| author | = { | Svoboda, F. and Hrom\v{c}\'ik, M.}, |
| title | = { | Finite Element Method Based Modeling of a Flexible Wing Structure}, |
| booktitle | = { | Proceedings of the 2017 21st International Conference on Process Control (PC)}, |
| year | = { | 2017}, |
| pages | = { | 222-227}, |
| editor | = { | Fikar, M. and Kvasnica, M.}, |
| address | = { | \v{S}trbsk\'e Pleso, Slovakia}} |