An effective computer modelling approach to the study of aeroelastic characteristics of an aircraft composite wing with high aspect ratio
DOI10.1080/13873954.2014.903283zbMath1310.93028OpenAlexW1989924129MaRDI QIDQ5248057
Shengjun Qiao, S. H. Huo, Junran Zhang, Fu-Sheng Wang, Zhu-Feng Yue
Publication date: 27 April 2015
Published in: Mathematical and Computer Modelling of Dynamical Systems (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1080/13873954.2014.903283
flutterstiffness distributionstatic aeroelasticityCFD/CSD coupled methodhigh-aspect ratio winghoneycomb core sandwich composite
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Cites Work
- Automatic mesh update with the solid-extension mesh moving technique
- A finite volume unstructured mesh approach to dynamic fluid--structure interaction: an assessment of the challenge of predicting the onset of flutter
- A dynamic variational multiscale method for large eddy simulations on unstructured meshes
- Aeroelastic optimization of an aerobatic aircraft wing structure
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