The University of Southampton
University of Southampton Institutional Repository

Flow and noise predictions for a tandem cylinder configuration using novel hybrid RANS/LES approaches

Flow and noise predictions for a tandem cylinder configuration using novel hybrid RANS/LES approaches
Flow and noise predictions for a tandem cylinder configuration using novel hybrid RANS/LES approaches
The performance of several novel hybrid RANS/LES methodologies for accurate flow and noise predictions of the NASA Tandem Cylinder Experiment are investigated. Simulations are performed using three different hybrid RANS/LES methodologies which employ different techniques to transform the baseline RANS model into a turbulence resolving subgrid scale model. The approaches investigated are the Scale-Adaptive-Simulation which computes the subgrid dissipation-rate from a transport equation that is sensitive to the v. Karman length scale, the IDDES approach and a modified Flow-Simulation-Methodology (FSM) which both rely on replacing the modeled turbulent length scale with a measure of the local grid spacing. Since we expect that the predictions in the RANS and LES region depend on the capabilities of the baseline RANS model, the hybrid RANS/LES approaches used in this study are based on an Explicit-Algebraic-Stress Model. These models are assessed and compared with formulations based on a traditional two-equation model. The simulations are performed with the open-source finite volume code OpenFOAM and acoustic predictions are obtained using an acoustic analogy based on Curle's theory. The IDDES and FSM approaches were found to predict the hydrodynamic field in very good agreement with reference data but showed some deficiencies in capturing the higher harmonics in the acoustic spectra and broadband noise levels at high Strouhal numbers. The SAS approaches lack in accuracy for predicting the hydrodynamic field but resolve the higher harmonics in the acoustic spectra.
Weinmann, M.
05a3c2f0-4ec9-4bc3-957f-98c55392de8f
Sandberg, R.D.
41d03f60-5d12-4f2d-a40a-8ff89ef01cfa
Weinmann, M.
05a3c2f0-4ec9-4bc3-957f-98c55392de8f
Sandberg, R.D.
41d03f60-5d12-4f2d-a40a-8ff89ef01cfa

Weinmann, M. and Sandberg, R.D. (2010) Flow and noise predictions for a tandem cylinder configuration using novel hybrid RANS/LES approaches. 16th AIAA/CEAS Aeroacoustics Conference, , Stockholm, Sweden. 06 - 08 Jun 2010. 20 pp .

Record type: Conference or Workshop Item (Paper)

Abstract

The performance of several novel hybrid RANS/LES methodologies for accurate flow and noise predictions of the NASA Tandem Cylinder Experiment are investigated. Simulations are performed using three different hybrid RANS/LES methodologies which employ different techniques to transform the baseline RANS model into a turbulence resolving subgrid scale model. The approaches investigated are the Scale-Adaptive-Simulation which computes the subgrid dissipation-rate from a transport equation that is sensitive to the v. Karman length scale, the IDDES approach and a modified Flow-Simulation-Methodology (FSM) which both rely on replacing the modeled turbulent length scale with a measure of the local grid spacing. Since we expect that the predictions in the RANS and LES region depend on the capabilities of the baseline RANS model, the hybrid RANS/LES approaches used in this study are based on an Explicit-Algebraic-Stress Model. These models are assessed and compared with formulations based on a traditional two-equation model. The simulations are performed with the open-source finite volume code OpenFOAM and acoustic predictions are obtained using an acoustic analogy based on Curle's theory. The IDDES and FSM approaches were found to predict the hydrodynamic field in very good agreement with reference data but showed some deficiencies in capturing the higher harmonics in the acoustic spectra and broadband noise levels at high Strouhal numbers. The SAS approaches lack in accuracy for predicting the hydrodynamic field but resolve the higher harmonics in the acoustic spectra.

This record has no associated files available for download.

More information

Published date: 7 June 2010
Additional Information: AIAA 2010-3787
Venue - Dates: 16th AIAA/CEAS Aeroacoustics Conference, , Stockholm, Sweden, 2010-06-06 - 2010-06-08
Organisations: Aerodynamics & Flight Mechanics

Identifiers

Local EPrints ID: 185781
URI: http://eprints.soton.ac.uk/id/eprint/185781
PURE UUID: 2aef2e81-134f-4bc9-a799-922438cd238b
ORCID for R.D. Sandberg: ORCID iD orcid.org/0000-0001-5199-3944

Catalogue record

Date deposited: 11 May 2011 08:20
Last modified: 08 Jan 2022 14:36

Export record

Contributors

Author: M. Weinmann
Author: R.D. Sandberg ORCID iD

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.

×