A Non-reflective Boundary Condition for Prediction of Acoustic Tones in Turbomachinery using Computational Fluid Dynamics-Reference-Cited by-同舟云学术

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A Non-reflective Boundary Condition for Prediction of Acoustic Tones in Turbomachinery using Computational Fluid Dynamics

Published:2019-05-18 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA/CEAS Aeroacoustics Conference
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Author:

Zaabar Kamran¹,Wilson Alexander G.¹

Affiliation:

1. University of Southampton

Publisher

American Institute of Aeronautics and Astronautics

Reference23 articles.

1. Johnson,S.G.“NotesonPerfectlyMatchedLayers(PMLs),”2010.

2. Mani,A.“OntheReflectivityofSpongeZonesinCompressibleFlowSimulations,”2010.

3. Analysis of sponge zones for computational fluid mechanics

4. Giles,M.B.“Non-ReflectingBoundaryConditionsfortheEulerEquations,”Report,1988.

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Acoustic Mode Attenuation in Ducts (Using CFD) with Time-Domain Impedance Boundary Condition;AIAA Journal;2022-12

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