Meshless Method Applied to Low Speed Wing Aeroelasticity

Mohammaedreza Moosavi

Research output: Contribution to conferenceAbstract

Abstract

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.

Conference

ConferenceThe 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 titleECCM-ECFD 2018
CountryUnited Kingdom
CityGlasgow
Period11/06/1815/06/18
Internet address

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  • Cite this

    Moosavi, M. (Accepted/In press). Meshless Method Applied to Low Speed Wing Aeroelasticity. Abstract from 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), Glasgow, United Kingdom.