Low Frequency Flexural Wave Propagation in Laminated Composite Plates

1988 ◽  
pp. 45-65 ◽  
Author(s):  
B. Tang ◽  
E. G. Henneke ◽  
R. C. Stiffler
1988 ◽  
Vol 83 (6) ◽  
pp. 2020-2026 ◽  
Author(s):  
S. K. Datta ◽  
A. H. Shah ◽  
R. L. Bratton ◽  
T. Chakraborty

2020 ◽  
Vol 191-192 ◽  
pp. 99-109
Author(s):  
Nadine Bejjani ◽  
Pierre Margerit ◽  
Karam Sab ◽  
Joanna Bodgi ◽  
Arthur Lebée

2000 ◽  
Vol 68 (3) ◽  
pp. 503-505 ◽  
Author(s):  
M. R. Chitnis ◽  
Y. M. Desai ◽  
T. Kant

A higher order displacement based formulation has been developed to investigate wave propagation in fiber-reinforced polymer composite laminated (FRPCL) plates. The formulation has been applied, as an illustration, to a plate made up of transversely isotropic laminae with the axes of symmetry lying in the plane of the lamina. Results for the plane as well as the antiplane strain cases are shown to be in excellent agreement with the exact solutions for isotropic and transversely isotropic single layered plates. Also, numerical results have been obtained for crossply (0 deg/90 deg/0 deg/90 deg) laminated composite plates, which agree very well with the previously published numerical results. The formulation can be employed to expeditiously investigate the dispersion characteristics of waves propagating in a plate with an arbitrary number of anisotropic laminae.


1973 ◽  
Vol 40 (1) ◽  
pp. 193-200 ◽  
Author(s):  
C. T. Sun

Plate equations for the incremental deformation in composite plates with orthotropic constituent layers are derived according to Trefftz’s formulation for elastic bodies under initial stress. The plate theory thus derived includes the microdeformation which can account for the heterogeneity of the plate. Flexural wave propagation under initial stress and buckling of a simply supported rectangular composite plate are investigated. In a special case of harmonic wave propagation in a free composite plate dispersion curves predicted by the plate equations are compared with the exact curve. Good agreement is observed for the complete plate theory and Approximation I, while the adequacy of the other two sets of simplified equations, Approximations II and III, depends vitally on the ratio of the transverse shear rigidities of the constituent materials.


Author(s):  
Huan Zi ◽  
Yinggang Li

Sandwich structures are widely applied in modern industry such as aerospace, automobile as well as marine structures. However, the vibroacoustic properties of sandwich structures are adversely influenced by low effective mass. In this study, the flexural wave propagation characteristics and vibration mitigation performances of the periodic sandwich plate-type metastructures are investigated. The proposed sandwich plate-type metastructures are constituted of a sandwich plate with periodic thin-wall circular tube cores and periodically attached local stepped resonators. A finite element method combining Solid-Shell coupling numerical method and Bloch theory is presented to calculate the dispersion relations and the displacement fields of the eigenmodes of the infinite periodic sandwich plate-type metastructures. In addition, the acceleration frequency responses and vibration attenuation performances of finite periodic sandwich plate-type metastructures are numerically investigated and compared with the experimental measurements. Furthermore, the influences of geometric parameters on flexural wave band gaps are conducted. Results show that the sandwich plate-type metastructures can yield a low-frequency broad flexural wave band gap, in which the flexural wave propagation is conspicuously suppressed, resulting in significant flexural vibration attenuation. The flexural wave band gap and vibration attenuation performances can be effectively manipulated by designing geometric parameters of the sandwich plate-type metastructures.


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