Computational fluid-structure Interaction of membranes and shells with application to bat flight
Computational fluid-structure Interaction of membranes and shells with application to bat flight
Fluid-Structure Interaction of thin, flexible structures is omnipresent in nature and engineering. Numerical simulation of this kind of system is challenging due to the large non-linear deformations and the strong added-mass effect. In this thesis, we develop a novel immersed boundary fluid-structure structure interaction solver to deal with those challenging cases. First, we show that immersed boundary methods must explicitly impose the Neumann condition on the pressure field for accurate results when the structure is thin and dynamic. We develop an extension to an existing immersed boundary method, BDIM-sigma, that enforces this boundary condition regardless of the body's thickness. The method relies on a variable coefficient Poisson equation to impose the Neumann condition on the interface. Standard linear algebra methods solve the resulting linear system. The method drastically outperforms Direct-Forcing methods and the standard immersed boundary method for problems with thin dynamic structures.
We couple our immersed boundary method with a three-dimensional shell solver via an implicit partitioned approach. A quasi-Newton method solves the resulting fixed-point problem. The method constructs an approximation of the Jacobian of the interface via input-output pairs of the coupling variables from the previously converged time steps. These pairs form an inverse least-square problem whose solution is the (inverse) Jacobian of the interface. With various fluid-structure interaction examples, we show that the method possesses excellent spatial convergence properties, is stable and efficient for a large range of flexibility and mass ratios and outperforms standard Gauss-Seidel relaxation methods.
Finally, we demonstrate the capability of our coupled solver to deal with practical examples by simulating bat flight. We investigate the effects of Strouhal number, membrane elasticity and fibre reinforcement on the aerodynamic efficiencies of bats. We show that the three-dimensional nature of the kinematics results in aerodynamic efficiencies peaking well outside the optimal Strouhal number range. Additionally, we show that propulsive efficiency is well correlated with membrane elasticity, where elastic membranes outperform stiff ones until flutter occurs. To extend the flutter envelope of the wing, we reinforce the isotropic membrane with anisotropic fibres. The response of this modified membrane shows a drastic reduction in the flutter and large improvements in aerodynamic efficiencies.
computational, Fluid-structure interaction, membranes, Shells, bio-locomotion, bat flight
University of Southampton
Lauber, Marin
c8fa4bb5-81ad-4ccc-b24d-17dcc2d229af
2023
Lauber, Marin
c8fa4bb5-81ad-4ccc-b24d-17dcc2d229af
Weymouth, Gabriel
b0c85fda-dfed-44da-8cc4-9e0cc88e2ca0
Limbert, Georges
a1b88cb4-c5d9-4c6e-b6c9-7f4c4aa1c2ec
Lauber, Marin
(2023)
Computational fluid-structure Interaction of membranes and shells with application to bat flight.
University of Southampton, Doctoral Thesis, 212pp.
Record type:
Thesis
(Doctoral)
Abstract
Fluid-Structure Interaction of thin, flexible structures is omnipresent in nature and engineering. Numerical simulation of this kind of system is challenging due to the large non-linear deformations and the strong added-mass effect. In this thesis, we develop a novel immersed boundary fluid-structure structure interaction solver to deal with those challenging cases. First, we show that immersed boundary methods must explicitly impose the Neumann condition on the pressure field for accurate results when the structure is thin and dynamic. We develop an extension to an existing immersed boundary method, BDIM-sigma, that enforces this boundary condition regardless of the body's thickness. The method relies on a variable coefficient Poisson equation to impose the Neumann condition on the interface. Standard linear algebra methods solve the resulting linear system. The method drastically outperforms Direct-Forcing methods and the standard immersed boundary method for problems with thin dynamic structures.
We couple our immersed boundary method with a three-dimensional shell solver via an implicit partitioned approach. A quasi-Newton method solves the resulting fixed-point problem. The method constructs an approximation of the Jacobian of the interface via input-output pairs of the coupling variables from the previously converged time steps. These pairs form an inverse least-square problem whose solution is the (inverse) Jacobian of the interface. With various fluid-structure interaction examples, we show that the method possesses excellent spatial convergence properties, is stable and efficient for a large range of flexibility and mass ratios and outperforms standard Gauss-Seidel relaxation methods.
Finally, we demonstrate the capability of our coupled solver to deal with practical examples by simulating bat flight. We investigate the effects of Strouhal number, membrane elasticity and fibre reinforcement on the aerodynamic efficiencies of bats. We show that the three-dimensional nature of the kinematics results in aerodynamic efficiencies peaking well outside the optimal Strouhal number range. Additionally, we show that propulsive efficiency is well correlated with membrane elasticity, where elastic membranes outperform stiff ones until flutter occurs. To extend the flutter envelope of the wing, we reinforce the isotropic membrane with anisotropic fibres. The response of this modified membrane shows a drastic reduction in the flutter and large improvements in aerodynamic efficiencies.
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Published date: 2023
Keywords:
computational, Fluid-structure interaction, membranes, Shells, bio-locomotion, bat flight
Identifiers
Local EPrints ID: 476005
URI: http://eprints.soton.ac.uk/id/eprint/476005
PURE UUID: 1a17fe8d-1a4b-4cdb-b28b-cb0cd91dfc40
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Date deposited: 04 Apr 2023 16:31
Last modified: 20 Mar 2024 05:01
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Author:
Marin Lauber
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