Pages that link to "Item:Q1756254"
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The following pages link to A new approach to reinforce the fiber of nanocomposite reinforced by CNTs to analyze free vibration of hybrid laminated cylindrical shell using beam modal function method (Q1756254):
Displaying 10 items.
- Modeling large amplitude vibration of pretwisted hybrid composite blades containing CNTRC layers and matrix cracked FRC layers (Q2182999) (← links)
- Nonlinear hygrothermal vibration and buckling analysis of imperfect FG-CNTRC cylindrical panels embedded in viscoelastic foundations (Q2224647) (← links)
- A size-dependent elastic theory for magneto-electro-elastic materials (Q2229673) (← links)
- The effect of agglomeration and slightly weakened CNT-matrix interface on free vibration response of cylindrical nanocomposites (Q2234286) (← links)
- Three-dimensional thermoelasticity analysis of graphene platelets reinforced cylindrical panel (Q2307772) (← links)
- Effect of carbon nanotube waviness on active damping of laminated hybrid composite shells (Q2516706) (← links)
- Bifurcation and Chaos of Functionally Graded Carbon Nanotube Reinforced Composite Beam with Piezoelectric Layer (Q5157058) (← links)
- An analytical approach for the nonlinear free vibration analysis of thin-walled circular cylindrical shells (Q6491540) (← links)
- Nonlinear dynamics of nanocomposite beam-like aerospace structures (Q6578078) (← links)
- Free vibration analysis of hybrid laminated thin-walled cylindrical shells containing multilayer FG-CNTRC plies (Q6661905) (← links)