Pages that link to "Item:Q2295120"
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The following pages link to Modeling large amplitude vibration of matrix cracked hybrid laminated plates containing CNTR-FG layers (Q2295120):
Displaying 9 items.
- Nonlinear dynamics of matrix-cracked hybrid laminated plates containing carbon nanotube-reinforced composite layers resting on elastic foundations (Q333018) (← links)
- Computation of elastodynamic behavior of a hybrid laminated plate containing CNTR-FG layers and FRC layers under dynamic loading (Q1657104) (← links)
- On the dynamics of rotating matrix cracked FG-GPLRC cylindrical shells via the element-free IMLS-Ritz method (Q1980170) (← links)
- Modeling geometrically nonlinear large deformation behaviors of matrix cracked hybrid composite deep shells containing CNTRC layers (Q1988250) (← links)
- A size-dependent differential quadrature element model for vibration analysis of FG CNT reinforced composite microrods based on the higher order Love-Bishop rod model and the nonlocal strain gradient theory (Q2127980) (← links)
- Effect of cracks on dynamical responses of double-variable-edge plates made of graphene nanoplatelets-reinforced porous matrix and sur-bonded by piezoelectric layers subjected to thermo-mechanical loads (Q2168495) (← links)
- Modeling large amplitude vibration of pretwisted hybrid composite blades containing CNTRC layers and matrix cracked FRC layers (Q2182999) (← links)
- On the analysis of nonlinear dynamic behavior of an isolation system with irrational restoring force and fractional damping (Q2285599) (← links)
- Stability analyses of cracked functionally graded graphene-platelets reinforced composite beam covered with piezoelectric layers (Q6538326) (← links)
