An immersed boundary method based on domain decomposition

Journal Article (2020)
Author(s)

N Rajan (TU Delft - Wind Energy)

A Vire (TU Delft - Wind Energy)

R. Schmehl (TU Delft - Wind Energy)

Gerard J.W. Van Bussel (TU Delft - Wind Energy)

Research Group
Wind Energy
Copyright
© 2020 Navaneetha Krishnan, A.C. Viré, R. Schmehl, G.J.W. van Bussel
DOI related publication
https://doi.org/10.1016/j.compfluid.2020.104500
More Info
expand_more
Publication Year
2020
Language
English
Copyright
© 2020 Navaneetha Krishnan, A.C. Viré, R. Schmehl, G.J.W. van Bussel
Research Group
Wind Energy
Volume number
202
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

A novel immersed boundary method based on a domain decomposition approach is proposed in the context of a finite element discretisation method. It is applicable to incompressible flows past rigid, deforming, or moving bodies. In this method, unlike most immersed boundary methods, strong boundary conditions are imposed in the regions of the computational domain that are occupied by the structure. In order to achieve this, the proposed formulation decomposes the computational domain by splitting the finite element test functions into solid and fluid parts. In the continuous Galerkin formulation, this produces a smeared representation of the fluid-structure interface. The absence of an immersed boundary forcing term implies that the method itself has no influence on the CFL stability criterion. Furthermore, the stiffness matrix in the momentum equation is sparser than compared with other forcing immersed boundary methods, and symmetry and positive-definiteness of the Laplacian operator in the pressure equation is preserved. As shown in this paper, stability and accurate imposition of boundary conditions make the method promising for high Reynolds number flows. The method is applied to the simulations of two-dimensional laminar flow over stationary and moving cylinders, as well as a moderately high Reynolds number flow past an aerofoil. Good results are obtained when compared with those from previous experimental and numerical studies.

Files

1_s2.0_S0045793020300748_main.... (pdf)
(pdf | 1.75 Mb)
- Embargo expired in 01-10-2020
License info not available