Towards a Generic Non-Reflective Characteristic Boundary Condition for Aeroacoustic Simulations

Ryu Fattah, James Gill, Xin Zhanga

Research output: Chapter in Book/Conference Proceeding/ReportConference Paper published in a bookpeer-review

1 Citation (Scopus)

Abstract

A blended zonal characteristic boundary condition is proposed following a quantitative investigation of the performance of several non-reective boundary conditions. Two test cases are considered that investigate the effects of acoustic and vortical plane waves impinging on the domain outflow region. A third test case investigates the effects of broad- band turbulent flow impinging on a non-reective outflow boundary condition. From these studies, two non-reective boundary conditions based on a zonal characteristic method are found to provide a minimal acoustic response for impinging acoustic and vortical disturbances, respectively. These methods both make use of the transverse characteristic terms to improve performance, although each method uses a different inclusion of these terms. A final boundary condition is proposed that blends the performance of the two zonal characteristic methods. A blending function is used that switches the characteristic boundary condition smoothly between regions dominated by acoustic, or vortical, disturbances. The feasibility of this novel method is demonstrated on a test case where broadband turbulence impinges on a small section of an outow region.

Original languageEnglish
Title of host publication22nd AIAA/CEAS Aeroacoustics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103865
DOIs
Publication statusPublished - 2016
Externally publishedYes
Event22nd AIAA/CEAS Aeroacoustics Conference, 2016 - Lyon, France
Duration: 30 May 20161 Jun 2016

Publication series

Name22nd AIAA/CEAS Aeroacoustics Conference, 2016

Conference

Conference22nd AIAA/CEAS Aeroacoustics Conference, 2016
Country/TerritoryFrance
CityLyon
Period30/05/161/06/16

Bibliographical note

Publisher Copyright:
© American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

Keywords

  • Computational aeroacoustics
  • Non-reective boundary conditions

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