Lattice Boltzmann method and immersed boundary method for the simulation of viscous fluid flows
dc.contributor.advisor
Ingram, David
en
dc.contributor.advisor
Mueller, Markus
en
dc.contributor.advisor
Friedrich, Daniel
en
dc.contributor.advisor
Viola, Ignazio Maria
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dc.contributor.author
Falagkaris, Emmanouil
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dc.contributor.sponsor
other
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dc.date.accessioned
2018-10-24T09:34:17Z
dc.date.available
2018-10-24T09:34:17Z
dc.date.issued
2018-11-29
dc.description.abstract
Most realistic fluid flow problems are characterised by high Reynolds numbers
and complex boundaries. Over the last ten years, immersed boundary methods
(IBM) that are able to cope with realistic geometries have been applied to Lattice-
Boltzmann methods (LBM). These methods, however, have normally been applied
to low Reynolds number problems. In the present work, an iterative direct forcing
IBM has been successfully coupled with a multi-domain cascaded LBM in order to
investigate viscous flows around rigid, moving and wilfully deformed boundaries
at a wide range of Reynolds numbers. The iterative force-correction immersed
boundary method of (Zhang et al., 2016) has been selected due to the improved
accuracy of the computation, while the cascaded LB formulation is used due to its
superior stability at high Reynolds numbers. The coupling is shown to improve
both the stability and numerical accuracy of the solution. The resulting solver
has been applied to viscous flow (up to a Reynolds number of 100000) passed a
NACA-0012 airfoil at a 10 degree angle of attack. Good agreement with results
obtained using a body-fitted Navier-Stokes solver has been obtained.
At moving or deformable boundary applications, emphasis should be given on
the influence of the internal mass on the computation of the aerodynamic forces,
focusing on deforming boundary motions where the rigid body approximation
is no longer valid. Both the rigid body and the internal Lagrangian points
approximations are examined. The resulting solver has been applied to viscous
flows around an in-line oscillating cylinder, a pitching foil, a plunging SD7003
airfoil and a plunging and flapping NACA-0014 airfoil. Good agreement with
experimental results and other numerical schemes has been obtained. It is
shown that the internal Lagrangian points approximation accurately captures
the internal mass effects in linear and angular motions, as well as in deforming
motions, at Reynolds numbers up to 4 • 104.
Finally, an expanded higher-order immersed boundary method which addresses
two major drawbacks of the conventional IBM will be presented. First, an
expanded velocity profile scheme has been developed, in order to compensate
for the discontinuities caused by the gradient of the velocity across the boundary.
Second, a numerical method derived from the Navier-Stokes equations in order
to correct the pressure distribution across the boundary has been examined.
The resulting hybrid solver has been applied to viscous flows around stationary
and oscillating cylinders and examined the hovering flight of elliptical wings
at low Reynolds numbers. It is shown that the proposed scheme smoothly
expands the velocity profile across the boundary and increases the accuracy of
the immersed boundary method. In addition, the pressure correction algorithm
correctly expands the pressure profile across the boundary leading to very accurate
pressure coefficient values along the boundary surface.
The proposed numerical schemes are shown to be very efficient in terms of
computational cost. The majority of the presented results are obtained within a
few hours of CPU time on a 2.8 GHz Intel Core i7 MacBook Pro computer with
a 16GB memory.
en
dc.identifier.uri
http://hdl.handle.net/1842/33165
dc.language.iso
en
dc.publisher
The University of Edinburgh
en
dc.relation.hasversion
E. J. Falagkaris, D. M. Ingram, I. M. Viola, and K. Markakis. PROTEUS: A coupled iterative force-correction immersed-boundary multi-domain cascaded lattice boltzmann solver. Comput. Math. Appl., 74(10).
en
dc.relation.hasversion
E. J. Falagkaris, D. M. Ingram, K. Markakis, and I. M. Viola. PROTEUS: A coupled iterative force-correction immersed-boundary cascaded lattice boltzmann solver for moving and deformable boundary applications. Comput. Math. Appl., 75(4):1330 - 1354, 2018.
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dc.subject
aerodynamic behaviour of immersed bodies
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dc.subject
flow characteristics
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dc.subject
immersed boundary methods
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dc.subject
Lattice- Boltzmann methods
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dc.subject
iterative force-correction immersed boundary method
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dc.title
Lattice Boltzmann method and immersed boundary method for the simulation of viscous fluid flows
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dc.type
Thesis or Dissertation
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dc.type.qualificationlevel
Doctoral
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dc.type.qualificationname
PhD Doctor of Philosophy
en
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