Pages that link to "Item:Q2035240"
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The following pages link to Free vibration analysis of laminated composite hybrid and GFRP shells based on higher order zigzag theory with experimental validation (Q2035240):
Displaying 6 items.
- Hybrid theoretical, experimental and numerical study of vibration and buckling of composite shells with scatter in elastic moduli (Q837783) (← links)
- Dynamic behavior of hybrid composite shallow shell panel-FEM HOSDT and experimental approach (Q2102548) (← links)
- Theoretical and experimental investigations of vibration and damping behaviors of carbon fiber-reinforced composite thin shells with partial bolt looseness constraints (Q2102648) (← links)
- Improved vibration based damage detection in laminated composite plate structures under free and forced modal analysis (Q6163047) (← links)
- Free vibration analysis of laminated doubly-curved shells with arbitrary material orientation distribution employing higher order theories and differential quadrature method (Q6539075) (← links)
- Straightforward free vibration solutions of open cylindrical shells by the finite integral transform method (Q6551614) (← links)
