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An immersed boundary method for high-fidelity simulations of moving objects on a Cartesian mesh

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Title: An immersed boundary method for high-fidelity simulations of moving objects on a Cartesian mesh
Authors: Giannenas, Athanasios Emmanouil
Item Type: Thesis or dissertation
Abstract: Despite breakthroughs in the field of computational fluid dynamics, performing simulations of moving objects with complex geometries on supercomputers remains a considerable challenge. Body-conforming methods are costly (due to re-meshing) and suffer from mesh-related issues. Hence, non-body-conforming Immersed Boundary Methods (IBMs), which eliminate re-meshing have emerged. Here, a simple and scalable Alternating Direction Reconstruction IBM (ADR-IBM) is proposed for high-fidelity simulations with multiple moving geometries in laminar and turbulent flows. The method imposes the boundary conditions at the walls via 1D cubic spline interpolations and is combined with high-order finite-difference schemes. The accuracy and convergence of the method are assessed for the flow around a cylinder at Re = 40. A comparison of second- and sixth-order schemes with the ADR-IBM is presented for 2D and 3D flows. The scalability of the method is demonstrated for up to 65,536 cores for the flow over a moving sphere at Re = 3700. Further, a Smooth Interface IBM is proposed for turbulent simulations of multiple moving geometries on supercomputers. It suppresses spurious force oscillations (SFOs) by smoothing the boundary interface. However, the ADR-IBM remains superior by providing lower error levels at lower cost with no treatment for the SFOs. Additionally, a harmonically forced laminar bluff body wake by two rear pitching flaps is studied. The forced flow over a 2D rectangle at Re = 100 is considered with in-phase and out-of-phase forcing. A fundamental (subharmonic) resonance is observed for the in-phase (out-of-phase) forcing. Both strategies produce significant drag reductions through a wake symmetrisation and propulsion mechanisms. It is postulated that the ejection of two vortex dipoles leads to the symmetrisation of the wake. Further, a single scaling parameter is proposed to predict the mean drag reduction of the forced flow. To identify the strategy with the highest net energy saving potential, the efficiency is assessed.
Content Version: Open Access
Issue Date: Sep-2021
Date Awarded: Mar-2022
URI: http://hdl.handle.net/10044/1/102733
DOI: https://doi.org/10.25560/102733
Copyright Statement: Creative Commons Attribution NonCommercial NoDerivatives Licence
Supervisor: Laizet, Sylvain
Sponsor/Funder: Imperial College London
Engineering and Physical Sciences Research Council (EPSRC)
PRACE
UKRI COVID-19 Grant Extension
Funder's Grant Number: EPSRC (grant number: EP/R029326/1)
PRACE (grant number: 2019215138)
Department: Aeronautics
Publisher: Imperial College London
Qualification Level: Doctoral
Qualification Name: Doctor of Philosophy (PhD)
Appears in Collections:Aeronautics PhD theses



This item is licensed under a Creative Commons License Creative Commons