Activity: Talk or presentation › Oral presentation
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.
11 Jun 2018
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