An error indicator for finite difference methods using spectral techniques with application to aerofoil simulation
An error indicator for finite difference methods using spectral techniques with application to aerofoil simulation
This work focusses on the development of an error indicator which can be used to determine areas of insufficient numerical resolution in unfiltered finite difference simulations. The approach adopts spectral techniques, applying small-domain Fourier transforms to a finite number of blocks which span the domain. The indicator is evaluated in the context of a NACA-0012 aerofoil simulation.
Computational Fluid Dynamics, aerofoil, simulation and modelling, error indicators, Finite Difference Method, Graphics Processing Units
Jacobs, Christian
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Sandham, Neil
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De Tullio, Nicola
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Jacobs, Christian
0ffde78b-6ae2-4b44-a916-666f6be2b92c
Sandham, Neil
0024d8cd-c788-4811-a470-57934fbdcf97
De Tullio, Nicola
db4397b2-3fab-476c-a0f4-4caf9848d5f7
Jacobs, Christian, Sandham, Neil and De Tullio, Nicola
(2017)
An error indicator for finite difference methods using spectral techniques with application to aerofoil simulation.
29th International Conference on Parallel Computational Fluid Dynamics, , Glasgow, United Kingdom.
15 - 17 May 2017.
2 pp
.
(In Press)
Record type:
Conference or Workshop Item
(Other)
Abstract
This work focusses on the development of an error indicator which can be used to determine areas of insufficient numerical resolution in unfiltered finite difference simulations. The approach adopts spectral techniques, applying small-domain Fourier transforms to a finite number of blocks which span the domain. The indicator is evaluated in the context of a NACA-0012 aerofoil simulation.
Text
Jacobs_etal_Accepted_ParCFD_2017_extended_abstract
- Accepted Manuscript
More information
Submitted date: 16 January 2017
Accepted/In Press date: 27 February 2017
Venue - Dates:
29th International Conference on Parallel Computational Fluid Dynamics, , Glasgow, United Kingdom, 2017-05-15 - 2017-05-17
Keywords:
Computational Fluid Dynamics, aerofoil, simulation and modelling, error indicators, Finite Difference Method, Graphics Processing Units
Organisations:
Aeronautics, Astronautics & Comp. Eng, Aerodynamics & Flight Mechanics Group
Identifiers
Local EPrints ID: 407655
URI: http://eprints.soton.ac.uk/id/eprint/407655
PURE UUID: 75b6c26a-5ec7-41af-a3d4-0e97596567d7
Catalogue record
Date deposited: 16 Apr 2017 17:09
Last modified: 16 Mar 2024 03:03
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Contributors
Author:
Christian Jacobs
Author:
Neil Sandham
Author:
Nicola De Tullio
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