Abstract
In this research contribution, size-dependent forced vibration analysis of embedded cross/angle-plies laminated composite nanoplate in a viscoelastic foundation while subjected to a moving load is investigated. Through Hamiltonian principle, the governing motion equations are derived on the basis of a four-variable refined higher-order shear deformation theory (RHSDT) in Cartesian coordinate and Eringen nonlocal differential model (ENDM) is used in order to predict the size-dependent effects. Afterwards, in order to solve the equations, a time-dependent system of state-space in conjunction with an analytical solution method is implemented over the structures. For the first time, the effect of lay-up numbers and sequences, fiber orientations of involved layers, elastic/viscoelastic foundation coefficients, and nanoplate geometries on the size-dependent dynamic response of laminated composite nanoplate under moving concentrated load with different values of velocity and time history is examined.
| Original language | English |
|---|---|
| Article number | 116540 |
| Journal | Composite Structures |
| Volume | 305 |
| DOIs | |
| State | Published - 1 Feb 2023 |
| Externally published | Yes |
Keywords
- Laminated composite materials
- Moving load
- State-space method
- Viscoelastic foundation
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