A piecewise linear mean flow model for studying stability in a lined channel-Reference-Cited by-同舟云学术

A piecewise linear mean flow model for studying stability in a lined channel

Published:2012-07 Issue:16 Volume:331 Page:3809-3823
ISSN:0022-460X
Container-title:Journal of Sound and Vibration
language:en
Short-container-title:Journal of Sound and Vibration

Author:

Marx David

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference33 articles.

1. Design and performance of duct acoustic treatment;Motsinger,1995

2. M. Brandes, D. Ronneberger, Sound amplification in flow ducts lined with a periodic sequence of resonators, Proceedings of the First AIAA/CEAS Aeroacoustic Conference, Munich, Germany, AIAA Paper 95-126, 1995.

3. PIV and LDV evidence of hydrodynamic instability over a liner in a duct with flow;Marx;Journal of Sound and Vibration,2010

4. On the stability of a laminar incompressible boundary layer over a flexible surface;Landahl;Journal of Fluid Mechanics,1962

5. The convective and absolute instability of fluid flow over viscoelastic compliant layers;Yeo;Journal of Sound and Vibration,1999

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