The University of Southampton
University of Southampton Institutional Repository

Les prediction of installed jet flow and noise with experimental validation

Les prediction of installed jet flow and noise with experimental validation
Les prediction of installed jet flow and noise with experimental validation

Extra noise is introduced when jets are installed under a solid surface. In the paper, Large-Eddy Simulation (LES) has been performed to investigate the installation effects. The simulations on two jet configurations are presented: one isolated jet and one installed jet with L/D = 4 and H/D = 1. The LES is compared with experimental data from both hot wire and microphone measurements. Good agreement has been achieved between LES and experimental data on flow statistics, near-field spectra, space-time correlations and far-field sound spectra. The installed effects are also discussed from the perspectives of flows and acoustics.

American Institute of Aeronautics and Astronautics
Wang, Zhong Nan
7a3c76aa-40bc-462b-bdbf-7908aabe9136
Proenca, Anderson
575c4921-cf19-4301-bc7a-70a4432ea0df
Lawrence, Jack
59a5a96a-8824-4bae-a22a-739ad4ce9144
Tucker, Paul G.
d2369489-a7db-41e1-a309-ee2e07a551d9
Self, Rod
8b96166d-fc06-48e7-8c76-ebb3874b0ef7
Wang, Zhong Nan
7a3c76aa-40bc-462b-bdbf-7908aabe9136
Proenca, Anderson
575c4921-cf19-4301-bc7a-70a4432ea0df
Lawrence, Jack
59a5a96a-8824-4bae-a22a-739ad4ce9144
Tucker, Paul G.
d2369489-a7db-41e1-a309-ee2e07a551d9
Self, Rod
8b96166d-fc06-48e7-8c76-ebb3874b0ef7

Wang, Zhong Nan, Proenca, Anderson, Lawrence, Jack, Tucker, Paul G. and Self, Rod (2019) Les prediction of installed jet flow and noise with experimental validation. In 25th AIAA/CEAS Aeroacoustics Conference, 2019. American Institute of Aeronautics and Astronautics.. (doi:10.2514/6.2019-2453).

Record type: Conference or Workshop Item (Paper)

Abstract

Extra noise is introduced when jets are installed under a solid surface. In the paper, Large-Eddy Simulation (LES) has been performed to investigate the installation effects. The simulations on two jet configurations are presented: one isolated jet and one installed jet with L/D = 4 and H/D = 1. The LES is compared with experimental data from both hot wire and microphone measurements. Good agreement has been achieved between LES and experimental data on flow statistics, near-field spectra, space-time correlations and far-field sound spectra. The installed effects are also discussed from the perspectives of flows and acoustics.

Text
AIAAJournal_UCAM_UoS - Author's Original
Download (3MB)

More information

e-pub ahead of print date: 18 May 2019
Venue - Dates: 25th AIAA/CEAS Aeroacoustics Conference, 2019, , Delft, Netherlands, 2019-05-20 - 2019-05-23

Identifiers

Local EPrints ID: 439563
URI: http://eprints.soton.ac.uk/id/eprint/439563
PURE UUID: 9d0afdf1-3711-419d-9141-b99168b5186b
ORCID for Anderson Proenca: ORCID iD orcid.org/0000-0002-4002-1805

Catalogue record

Date deposited: 27 Apr 2020 16:30
Last modified: 17 Mar 2024 12:39

Export record

Altmetrics

Contributors

Author: Zhong Nan Wang
Author: Anderson Proenca ORCID iD
Author: Jack Lawrence
Author: Paul G. Tucker
Author: Rod Self

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.

×