Enhancing Silo Discharge and Energy Efficiency with Vibrated Insert DOI Creative Commons
Guangyang Hong, Jie Gao, Qijun Zheng

et al.

International Journal of Mechanical Sciences, Journal Year: 2025, Volume and Issue: unknown, P. 110128 - 110128

Published: March 1, 2025

Language: Английский

Managing the surface piezoelectricity effect of the smart ZnO sandwich nanoplates using metal foam core layer and GPRL reinforced rim layers DOI
Mustafa Eroğlu, İsmail Esen, Mehmet Aki̇f Koç

et al.

Microsystem Technologies, Journal Year: 2024, Volume and Issue: unknown

Published: Sept. 24, 2024

Language: Английский

Citations

5

Variable-thickness higher-order sandwich beams with FG cellular core and CNT-RC patches: vibrational analysis in thermal environment DOI
Ehsan Arshid, Zahra Khoddami Maraghi, Ömer Cívalek

et al.

Archive of Applied Mechanics, Journal Year: 2024, Volume and Issue: 95(1)

Published: Nov. 21, 2024

Language: Английский

Citations

5

Free vibration and supersonic flutter analyses of a sandwich cylindrical shell with CNT-reinforced honeycomb core integrated with piezoelectric layers DOI

Soheyl Givi,

A. Ghorbanpour Arani, Zahra Khoddami Maraghi

et al.

Mechanics Based Design of Structures and Machines, Journal Year: 2024, Volume and Issue: unknown, P. 1 - 29

Published: Nov. 7, 2024

In this research, the free vibration and supersonic flutter analyses of a cylindrical sandwich shell with reinforced honeycomb core (RHC) integrated piezoelectric face sheets are investigated. The is structure enriched fibers carbon nanotubes (CNTs). layers modeled based on Cooper-Naghdi theory continuity conditions between considered. aerodynamic pressure flow using linear piston theory. Hamilton's principle used to derive governing equations. A semi-analytical solution presented including an exact in circumferential direction followed by numerical longitudinal via differential quadrature method (DQM). effects several parameters frequencies, corresponding damping coefficients, critical It concluded that improving stiffness CNTs does not necessarily improve aeroelastic stability shell. results can be design analysis aerospace structures.

Language: Английский

Citations

4

Enhancing Silo Discharge and Energy Efficiency with Vibrated Insert DOI Creative Commons
Guangyang Hong, Jie Gao, Qijun Zheng

et al.

International Journal of Mechanical Sciences, Journal Year: 2025, Volume and Issue: unknown, P. 110128 - 110128

Published: March 1, 2025

Language: Английский

Citations

0