Application of the sliding-mesh interface method to the high order spectral difference solver for aeroacoustic problems with rotating flows

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Abstract

In this study a sliding-mesh interface method is implemented to the high order spectral difference solver for aeroacoustic problems with rotating flows. The high order interpolation method is utilized for data exchange on the sliding interface for non-uniform unstructured mesh. The method is validated with both inviscid and viscous problems with rotating flows. The numerical results show that the present method is able to retain the high order accuracy of the SD method. Finally the developed solver is applied to simulate the flow field of a low speed propeller. The flow field and acoustic data are analyzed and presented.

Original languageEnglish
Title of host publication"Advances in Acoustics, Noise and Vibration - 2021" Proceedings of the 27th International Congress on Sound and Vibration, ICSV 2021
EditorsEleonora Carletti, Malcolm Crocker, Marek Pawelczyk, Jiri Tuma
PublisherSilesian University Press
ISBN (Electronic)9788378807995
StatePublished - 2021
Event27th International Congress on Sound and Vibration, ICSV 2021 - Virtual, Online
Duration: 11 Jul 202116 Jul 2021

Publication series

Name"Advances in Acoustics, Noise and Vibration - 2021" Proceedings of the 27th International Congress on Sound and Vibration, ICSV 2021
ISSN (Print)2329-3675

Conference

Conference27th International Congress on Sound and Vibration, ICSV 2021
CityVirtual, Online
Period11/07/2116/07/21

Keywords

  • Aero-acoustics
  • Rotating flow
  • Sliding Interface
  • Spectral Difference Method

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