Damping of flexural vibrations in turbofan blades using the acoustic black hole effect-Reference-Cited by-同舟云学术

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Damping of flexural vibrations in turbofan blades using the acoustic black hole effect

Published:2014-02 Issue: Volume:76 Page:359-365
ISSN:0003-682X
Container-title:Applied Acoustics
language:en
Short-container-title:Applied Acoustics

Author:

Bowyer E.P.,Krylov V.V.

Funder

EPSRC

Publisher

Elsevier BV

Subject

Acoustics and Ultrasonics

Reference15 articles.

1. Turbomachine blade vibration;Rao,1991

2. Structure-borne sound;Cremer,1988

3. Passive vibration control;Mead,1998

4. Damping of plate flexural vibrations by means of viscoelastic laminae;Ross,1960

5. Attenuation of waves in plates and bars using a graded impedance interface at edges;Vemula;J Sound Vib,1996

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