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

The results of the experimental study into the damping of flexural vibrations in turbofan blades with trailing edges tapered according to a power-law profile are reported. Trailing edges of power-law profile (wedges), with small pieces of attached absorbing layers, materialise one-dimensional acoust...

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Bibliographic Details
Main Authors: E.P. Bowyer, Victor V. Krylov
Format: Default Article
Published: 2014
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Online Access:https://hdl.handle.net/2134/13815
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