Measurement, Journal Year: 2024, Volume and Issue: unknown, P. 116565 - 116565
Published: Dec. 1, 2024
Language: Английский
Measurement, Journal Year: 2024, Volume and Issue: unknown, P. 116565 - 116565
Published: Dec. 1, 2024
Language: Английский
Acta Mechanica, Journal Year: 2025, Volume and Issue: unknown
Published: Jan. 15, 2025
Language: Английский
Citations
2Physica B Condensed Matter, Journal Year: 2025, Volume and Issue: 700, P. 416903 - 416903
Published: Jan. 8, 2025
Language: Английский
Citations
1Acta Mechanica, Journal Year: 2025, Volume and Issue: unknown
Published: Feb. 7, 2025
Language: Английский
Citations
1Mechanics of Advanced Materials and Structures, Journal Year: 2025, Volume and Issue: unknown, P. 1 - 18
Published: Feb. 24, 2025
Language: Английский
Citations
1Aerospace Science and Technology, Journal Year: 2024, Volume and Issue: unknown, P. 109672 - 109672
Published: Oct. 1, 2024
Language: Английский
Citations
7Microsystem Technologies, Journal Year: 2024, Volume and Issue: unknown
Published: Sept. 24, 2024
Language: Английский
Citations
5Archive of Applied Mechanics, Journal Year: 2024, Volume and Issue: 95(1)
Published: Nov. 21, 2024
Language: Английский
Citations
5Mechanics 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
4Mechanics of Advanced Materials and Structures, Journal Year: 2025, Volume and Issue: unknown, P. 1 - 13
Published: Jan. 14, 2025
The present study investigates the oscillation characteristics of a sport ball that is modeled as doubly curved shell made nanocomposite material consisting functionally graded graphene platelets and metal foams. immersed on Kerr basis, which an elastic foundation with three parameters. organization pores dispersion throughout thickness model are considered based stated functionality. Halpin-Tsai expanded rule mixture micromechanical models employed to determine effective mechanical property values. Once motion equations established, frequencies derived using analytical method, especially efficient for shells simply supported edges. investigation takes into account deals effects different influences natural frequencies. results could serve benchmark future research. Given absence comparable research in existing literature, findings this can standard investigations.
Language: Английский
Citations
0International Journal of Mechanical Sciences, Journal Year: 2025, Volume and Issue: unknown, P. 110128 - 110128
Published: March 1, 2025
Language: Английский
Citations
0