A meshless method is applied to a computational aeroelasticity problem. Both structure and fluid domains have been modelled with a meshless method. The moving least squares approximation scheme is used to interpolate field variables in the governing differential equations of the problem. The method is implemented to a wing subjected to a low speed velocity air flow. In order to investigate the proposed approach, convergence tests are performed and results has been compared with those of different approaches, such as collocation, finite volume, finite element, boundary element, and Trefftz methods.
|Publication status||Accepted/In press - 2017|
|Event||The 6th European Conference on Computational Mechanics (Solids, Structures and Coupled Problems) (ECCM 6) and the 7th European Conference on Computational Fluid Dynamics (ECFD 7): Computational Aeroelasticity - The University of Glasgow and The University of Edinburgh, Glasgow, United Kingdom|
Duration: 11 Jun 2018 → 15 Jun 2018
|Conference||The 6th European Conference on Computational Mechanics (Solids, Structures and Coupled Problems) (ECCM 6) and the 7th European Conference on Computational Fluid Dynamics (ECFD 7)|
|Abbreviated title||ECCM-ECFD 2018|
|Period||11/06/18 → 15/06/18|
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- School of Mechanical, Aerospace and Automotive Engineering - Assistant Lecturer in Engineering Simulation
Person: Teaching and Research