Free vibrations and buckling analyses of sandwich cylindrical shells with auxetic core and shape memory alloy wires reinforced face sheets

Composite Structures, Год журнала: 2025, Номер unknown, С. 118994 - 118994

Опубликована: Фев. 1, 2025

Язык: Английский

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Vibration and response behaviors of composite sandwich cylindrical shells with corrugated-honeycomb blended cores in inhomogeneous thermal environments

Thin-Walled Structures, Год журнала: 2024, Номер unknown, С. 112454 - 112454

Опубликована: Сен. 1, 2024

Язык: Английский

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A review on computational linear and nonlinear dynamic analysis of shell-type composite structures

Computers & Structures, Год журнала: 2024, Номер 306, С. 107596 - 107596

Опубликована: Ноя. 28, 2024

Язык: Английский

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Static deflection prediction of damaged glass fiber‐reinforced metal laminated composite and experimental validation

Polymer Composites, Год журнала: 2025, Номер unknown

Опубликована: Янв. 7, 2025

Abstract This study examines the influence of damage on stiffness characteristics synthetic fiber (Glass)‐reinforced metal laminated composite panels through static deflection analysis. The fiber‐metal laminate (FML) structural panel deflections are obtained computationally via a mathematical model using third‐order kinematics in framework equivalent single‐layer theory. values numerically with help finite element steps. solution consistencies verified by convergence test and extended to perform validation. Additionally, numerical results compared in‐house experimental data FML bending considering properties damage. maximum deviation intact response was −4.27%, while for crack showed −0.57%. Again, is engaged obtaining varying different geometry‐dependent design parameters, including data. spherical geometry pre‐damaged structure demonstrates better deformation resistance under external loading. thickness ratio ( L/h ) angle layup scheme show higher response. Highlights A higher‐order FE delved compute damaged FML. validity values. inference parameters computed numerically. understandings significant discussed detail.

Язык: Английский

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Nonlinear free vibration analysis of sandwich truncated conical shells with auxetic core and functionally graded face sheets

Mechanics Based Design of Structures and Machines, Год журнала: 2025, Номер unknown, С. 1 - 25

Опубликована: Март 23, 2025

Язык: Английский

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Nonlinear vibration of corrugated-honeycomb cylindrical shells in thermal environments

International Journal of Mechanical Sciences, Год журнала: 2025, Номер unknown, С. 110200 - 110200

Опубликована: Март 1, 2025

Язык: Английский

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Frequency multiplication resonances of spatial four-direction braided composite sandwich cylindrical shells with three-dimensional lattice pyramid cores exposed to harmonic loads and thermal environments

Thin-Walled Structures, Год журнала: 2025, Номер unknown, С. 113260 - 113260

Опубликована: Март 1, 2025

Язык: Английский

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Rapid optimization strategy for Chiral Quadrilateral Structures driven by deep learning and computational feedback

Materials Today Communications, Год журнала: 2025, Номер unknown, С. 112368 - 112368

Опубликована: Апрель 1, 2025

Язык: Английский

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Exploring honeycomb structures: A review of their types, general applications, and role in vibration damping and structural stability

Structures, Год журнала: 2025, Номер 76, С. 108837 - 108837

Опубликована: Апрель 15, 2025

Язык: Английский

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Traveling-wave vibration of spinning thick multi-conical shells: New solving system

International Journal of Mechanical Sciences, Год журнала: 2025, Номер 296, С. 110313 - 110313

Опубликована: Апрель 28, 2025

Язык: Английский

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