2014
DOI: 10.1016/j.apacoust.2013.09.009
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Damping of flexural vibrations in turbofan blades using the acoustic black hole effect

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Cited by 68 publications
(27 citation statements)
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“…11. Steel (a) and composite (b) plates containing slots of power-law profile [27] Following the idea first proposed in [4], experimental investigations into damping of flexural vibrations in turbofan blades with trailing edges tapered according to a power-law profile have been carried out in the papers [32,33]. Obviously, wedges of power-law profile fit naturally with a fan blade geometry (see Fig.…”
Section: Some Other Acoustic Black Hole Configurations and Applicamentioning
confidence: 99%
“…11. Steel (a) and composite (b) plates containing slots of power-law profile [27] Following the idea first proposed in [4], experimental investigations into damping of flexural vibrations in turbofan blades with trailing edges tapered according to a power-law profile have been carried out in the papers [32,33]. Obviously, wedges of power-law profile fit naturally with a fan blade geometry (see Fig.…”
Section: Some Other Acoustic Black Hole Configurations and Applicamentioning
confidence: 99%
“…Consequently, the waves take an infinite time to reach the zerothickness edge and do not reflect back, resulting in an acoustic black hole. Further development 2 and experimental work 3 has been performed, including ABH implementation in structures, 4,5 sound radiation, 6 and energy harvesting. 7 However, there is still a need to systematically understand the limitations and assumptions of the theory for the design, optimization, and implementation of ABHs in real structural systems.…”
Section: Introductionmentioning
confidence: 99%
“…An experimental work of damping of flexural vibrations in turbofan blades using ABH was studied by Bowyer and Krylov [46]. Figure 18a shows the fan blade profile with a tapered ABH geometry.…”
Section: Vibration Damping Of Turbofan Blades With Abhmentioning
confidence: 99%
“…Acceleration for a twisted reference blade (dashed line) compared to a twisted blade with a 1D ABH and damping layer (solid line). Reprinted from[46] under a CC BY 3.0 license. Copyright Bowyer, E.P.…”
mentioning
confidence: 99%