期刊
JOURNAL OF COMPUTATIONAL AND APPLIED MATHEMATICS
卷 427, 期 -, 页码 -出版社
ELSEVIER
DOI: 10.1016/j.cam.2023.115125
关键词
Finite element method; Aeroelasticity
This paper focuses on numerically approximating a simplified two-dimensional aerelastic problem involving a flexibly supported airfoil with a control section. The coupling of the control section with other modes can lead to a decrease in flutter velocity. The problem is mathematically described using a fully coupled formulation of incompressible, viscous fluid flow over a flexible structure, modeled by a system of ordinary differential equations. The numerical approximation is treated using the variational multiscale approach with the algebraic subgrid scale model, and the ALE mapping is constructed using a robust mesh deformation method. Numerical results are provided. (c) 2023 Elsevier B.V. All rights reserved.
This paper focus on the numerical approximation of a simplified two dimensional aeroe-lastic problem, where the flexibly supported airfoil with a control section is considered. In this case the coupling of the control section with other mode can cause a decrease of the flutter velocity. The problem is mathematically described using the fully coupled formulation of the incompressible viscous fluid flow over a flexibly structure, whose motion is modeled by system of ordinary differential equations. The incompressible flow is described by the system of Navier-Stokes equations written in the Arbitrary Lagrangian Eulerian form in order to treat the motion of the computational domain. The numerical approximation is treated using the variational multiscale approach using the algebraic subgrid scale model. The construction of the ALE mapping is based on a robust mesh deformation method. The numerical results are presented.(c) 2023 Elsevier B.V. All rights reserved.
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