2016
DOI: 10.1016/j.compstruct.2016.07.062
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On global bending–shear core transition effects for the vibroacoustic of sandwich structures: Analytical and numerical investigations

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Cited by 7 publications
(8 citation statements)
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“…The analysis of transition frequencies does not correspond only to the study at specific frequencies but also to transition ranges in which the structure can be characterized by a specific dynamic behavior. It can be defined in terms of wavemotion [39] but also in terms of strain energy [43].…”
Section: Transition Frequencymentioning
confidence: 99%
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“…The analysis of transition frequencies does not correspond only to the study at specific frequencies but also to transition ranges in which the structure can be characterized by a specific dynamic behavior. It can be defined in terms of wavemotion [39] but also in terms of strain energy [43].…”
Section: Transition Frequencymentioning
confidence: 99%
“…The analytical formulation of the flexural waves can be used to perform a numerical identification using the WFEM to obtain the dynamic bending and shear modulus. Similarly, this numerical identification strategy can be applied on the group velocity of bending waves [43,44]. Besides, an energetic method based on the calculation of the wavemode energy and the energy storage inside the core and the skins turned out the conversion of bending waves into shear waves located in the core.…”
Section: Introductionmentioning
confidence: 99%
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“…Baho et al [17], for instance, used a wavemode energy method, coupled with a wave assurance criterion, to predict the transition frequency of honeycomb panels modelled using a single periodic cells. In addition, the core geometry effects on the shear-core transition and sound transmission loss of honeycomb sandwich plates, are investigated in [18].…”
Section: Introductionmentioning
confidence: 99%
“…There have been many investigations aiming the modeling of the behavior of sandwich beam under Bending load [28][29][30] has been extensively investigated for both the static 3-Point Bending [31][32][33][34][35] and static 4-Point Bending [36][37][38][39]. There are also different studies with respect to the modeling of honeycomb sandwich structures especially [40,41].…”
Section: Introductionmentioning
confidence: 99%