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Assembly speed-up for the wave expansion method using a uniform background mesh
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Aerodynamics.ORCID iD: 0000-0002-6813-4764
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering.ORCID iD: 0000-0003-0176-5358
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering.ORCID iD: 0000-0002-9061-4174
(English)Manuscript (preprint) (Other academic)
National Category
Fluid Mechanics and Acoustics
Identifiers
URN: urn:nbn:se:kth:diva-196678OAI: oai:DiVA.org:kth-196678DiVA: diva2:1047469
Note

QC 20161118

Available from: 2016-11-17 Created: 2016-11-17 Last updated: 2016-12-08Bibliographically approved
In thesis
1. A Wave Expansion Method for Aeroacoustic Propagation
Open this publication in new window or tab >>A Wave Expansion Method for Aeroacoustic Propagation
2016 (English)Licentiate thesis, comprehensive summary (Other academic)
Abstract [en]

Although it is possible to directly solve an entire flow-acoustics problem in one computation, this approach remains prohibitively large in terms of the computational resource required for most practical applications. Aeroacoustic problems are therefore usually split into two parts; one consisting of the source computation and one of the source propagation. Although both these parts entail great challenges on the computational method, in terms of accuracy and efficiency, it is still better than the direct solution alternative. The source usually consists of highly turbulent flows, which for most cases will need to be, at least partly, resolved. Then, acoustic waves generated by these sources often have to be propagated for long distances compared to the wavelength and might be subjected to scattering by solid objects or convective effects by the flow. Numerical methods used solve these problems therefore have to possess low dispersion and dissipation error qualities for the solution to be accurate and resource efficient.

The wave expansion method (WEM) is an efficient discretization technique, which is used for wave propagation problems. The method uses fundamental solutions to the wave operator in the discretization procedure and will thus produce accurate results at two to three points per wavelength. This thesis presents a method that uses the WEM in an aeroacoustic context. Addressing the propagation of acoustic waves and transfer of sources from flow to acoustic simulations. The proposed computational procedure is applied to a co-rotating vortex pair and a cylinder in cross-flow. Overall, the computed results agree well with analytical solutions.

Although the WEM is efficient in terms of the spatial discretization, the procedure requires that a Moore-Penrose pseudo-inverse is evaluated at each unique node-neighbour stencil in the grid. This evaluation significantly slows the procedure. In this thesis, a method with a regular grid is explored to speed-up this process.

Place, publisher, year, edition, pages
KTH Royal Institute of Technology, 2016. 59 p.
Series
TRITA-AVE, ISSN 1651-7660 ; 2016:86
Keyword
Sound propagation, Sound generation, Aeroacoustics, Aerodynamics, Computational fluid dynamics, Computational aeroacoustics, Numerical methods, Lighthill, Curle, Ffowcs Williams and Hawkings, Frequency-domain propagation, Wave expansion method.
National Category
Fluid Mechanics and Acoustics
Research subject
Vehicle and Maritime Engineering
Identifiers
urn:nbn:se:kth:diva-196689 (URN)978-91-7729-215-9 (ISBN)
Presentation
2016-12-15, B1, Brinellvägen 23, Stockholm, 10:30 (English)
Opponent
Supervisors
Note

QC 20161121

Available from: 2016-11-22 Created: 2016-11-18 Last updated: 2016-12-02Bibliographically approved

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