The University of Southampton
University of Southampton Institutional Repository

Adaptive mesh refinement computation of acoustic radiation from an engine intake

Adaptive mesh refinement computation of acoustic radiation from an engine intake
Adaptive mesh refinement computation of acoustic radiation from an engine intake
A block-structured adaptive mesh refinement (AMR) method is applied to the problem of computing acoustic radiation from an aeroengine intake. The aim is to improve the efficiency of the computation through reduction of computational cells. A parallel implementation of the adaptive mesh refinement algorithm is achieved using message passing interface. It combines a range of 2nd- and 4th-order spatial stencils, a 4th-order low-dissipation and low-dispersion Runge-Kutta scheme for time integration and several different interpolation methods. To solve the problem of acoustic radiation from an aeroengine intake, the code is extended to support body-fitted grid structures. The problem of acoustic radiation is solved with linearised Euler equations. The results demonstrate the efficiency of the current adaptive mesh refinement algorithm.
1-13
Huang, Xun
57c88e52-954d-4e5a-94ca-3547a4cb9440
Zhang, Xin
3056a795-80f7-4bbd-9c75-ecbc93085421
Huang, Xun
57c88e52-954d-4e5a-94ca-3547a4cb9440
Zhang, Xin
3056a795-80f7-4bbd-9c75-ecbc93085421

Huang, Xun and Zhang, Xin (2006) Adaptive mesh refinement computation of acoustic radiation from an engine intake. 12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference), Cambridge, USA. 07 - 09 May 2006. pp. 1-13 .

Record type: Conference or Workshop Item (Paper)

Abstract

A block-structured adaptive mesh refinement (AMR) method is applied to the problem of computing acoustic radiation from an aeroengine intake. The aim is to improve the efficiency of the computation through reduction of computational cells. A parallel implementation of the adaptive mesh refinement algorithm is achieved using message passing interface. It combines a range of 2nd- and 4th-order spatial stencils, a 4th-order low-dissipation and low-dispersion Runge-Kutta scheme for time integration and several different interpolation methods. To solve the problem of acoustic radiation from an aeroengine intake, the code is extended to support body-fitted grid structures. The problem of acoustic radiation is solved with linearised Euler equations. The results demonstrate the efficiency of the current adaptive mesh refinement algorithm.

This record has no associated files available for download.

More information

Published date: 2006
Additional Information: AIAA 2006-2694
Venue - Dates: 12th AIAA/CEAS Aeroacoustics Conference (27th AIAA Aeroacoustics Conference), Cambridge, USA, 2006-05-07 - 2006-05-09
Organisations: Aerodynamics & Flight Mechanics

Identifiers

Local EPrints ID: 42978
URI: http://eprints.soton.ac.uk/id/eprint/42978
PURE UUID: bcb723d8-4235-4271-b368-683bc32b4cc0

Catalogue record

Date deposited: 05 Jan 2007
Last modified: 08 Jan 2022 12:59

Export record

Contributors

Author: Xun Huang
Author: Xin Zhang

Download statistics

Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.

View more statistics

Atom RSS 1.0 RSS 2.0

Contact ePrints Soton: eprints@soton.ac.uk

ePrints Soton supports OAI 2.0 with a base URL of http://eprints.soton.ac.uk/cgi/oai2

This repository has been built using EPrints software, developed at the University of Southampton, but available to everyone to use.

We use cookies to ensure that we give you the best experience on our website. If you continue without changing your settings, we will assume that you are happy to receive cookies on the University of Southampton website.

×