2000
DOI: 10.1016/s0924-0136(00)00564-1
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Damping of honeycomb sandwich beams

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Cited by 49 publications
(24 citation statements)
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“…Honeycomb sandwich materials are being used widely in weight sensitive and damping structures where high flexural rigidity is required, in many fields especially in the automobile industry [1][2][3]. Honeycomb core sandwich panel is formed by adhering two high-rigidity thin-face sheets with a low-density honeycomb core possessing less strength and stiffness.…”
Section: Introductionmentioning
confidence: 99%
“…Honeycomb sandwich materials are being used widely in weight sensitive and damping structures where high flexural rigidity is required, in many fields especially in the automobile industry [1][2][3]. Honeycomb core sandwich panel is formed by adhering two high-rigidity thin-face sheets with a low-density honeycomb core possessing less strength and stiffness.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, the current findings may seem smaller due to being averaged over a wider frequency range where a number of modes contribute to the response. Damping by cork inserts achieves better efficiency for nearly all filling degrees compared to particles used by Wang and Yang [12]. Their host structure is assembled out of a paper-resin honeycomb core covered by carbon fibre sheets.…”
Section: Comparison With Literaturementioning
confidence: 99%
“…However, the studies to demonstrate the above mentioned factors on the damping loss factor of the honeycomb sandwich FRP composites have been limited. The use of a honeycomb material in a composite laminate is witnessed in aerospace structures, where weight reduction and high flexural rigidity constitute the primary concern in designing structures (Bassani et al 2013, Wang andYang 2000). The FRP composite has a high in-plane stiffness-to-weight ratio, whereas the honeycomb sandwich possesses a high bending stiffness-to-weight ratio, in addition to the high in-plane stiffness to weight ratio (Maheri et al 2008).…”
Section: Introductionmentioning
confidence: 99%
“…More recently, they (Maheri et al 2008) have used the basic laminate theory, together with the Rayleigh-Ritz method, the finite element analysis and the experimental method, to predict damping and frequency of the honeycomb sandwich for space applications and considered the inherent damping of aluminum and carbon fibrereinforced plastic (CFRP) skins in sandwich panels. The damping effect of sandwich beams was also experimentally investigated with fine solder balls inserted in the honeycomb cells, losing the advantage of its light-weight (Wang and Yang (2000)). It was found that the damping was quite effective on measuring the reduction in amplitude from the first two modes of vibration.…”
Section: Introductionmentioning
confidence: 99%