Aerodynamic stability and free vibration of FGP-Reinforced nano-fillers annular sector microplates exposed to supersonic flow

Thin-Walled Structures, Год журнала: 2024, Номер 197, С. 111610 - 111610

Опубликована: Янв. 18, 2024

Язык: Английский

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Unified nonlocal surface elastic-based thermal induced asymmetric nonlinear buckling of inhomogeneous nano-arches subjected to dissimilar end conditions

Composite Structures, Год журнала: 2025, Номер unknown, С. 118961 - 118961

Опубликована: Фев. 1, 2025

Язык: Английский

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Natural frequency analysis of imperfect GNPRN conical shell, cylindrical shell, and annular plate structures resting on Winkler-Pasternak Foundations under arbitrary boundary conditions

Engineering Analysis with Boundary Elements, Год журнала: 2022, Номер 144, С. 145 - 164

Опубликована: Авг. 20, 2022

Язык: Английский

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Natural frequency analysis of FG-GOP/ polymer nanocomposite spheroid and ellipsoid doubly curved shells reinforced by transversely-isotropic carbon fibers

Engineering Analysis with Boundary Elements, Год журнала: 2022, Номер 138, С. 369 - 389

Опубликована: Март 11, 2022

Язык: Английский

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On the poroelastic vibrations of lightweight FGSP doubly-curved shells integrated with GNPs-reinforced composite coatings in thermal atmospheres

Applied Mathematical Modelling, Год журнала: 2023, Номер 124, С. 122 - 141

Опубликована: Авг. 1, 2023

Язык: Английский

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Thermo-elastic buckling behaviors of advanced fluid-infiltrated porous shells integrated with GPLs-reinforced nanocomposite patches

Mechanics of Advanced Materials and Structures, Год журнала: 2023, Номер 31(26), С. 7853 - 7869

Опубликована: Авг. 28, 2023

AbstractIn the existing paper, thermo-mechanical buckling performance of three-layered advanced fluid-infiltrated porous shells that are embedded between two GPLs-reinforced composite layers is investigated. The influence fluids in pores investigated using Skempton coefficient. Imperfection types and ratio effects also considered. Moreover, for face layers, Graphene nanoplatelets (GPLs) weight fraction dispersion patterns studied. After deriving governing equations employing virtual displacement method, they solved analytically via Navier's approach. Finally, impact different factors on critical loads (CBLs) temperatures (CBTs) cylindrical, spherical, doubly-curved assessed.Keywords: nanoplateletsfluid-infiltrated materialsthermo-elastic bucklingfirst-order shear deformation theorydoubly-curved shellsandwich structures Disclosure statementThe authors state there no conflict interest them to disclose.

Язык: Английский

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Circumferential vibration analysis of nano-porous-sandwich assembled spherical-cylindrical-conical shells under elastic boundary conditions

Engineering Structures, Год журнала: 2022, Номер 273, С. 115094 - 115094

Опубликована: Окт. 18, 2022

Язык: Английский

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Transient Thermal Stresses in FG Porous Rotating Truncated Cones Reinforced by Graphene Platelets

Applied Sciences, Год журнала: 2022, Номер 12(8), С. 3932 - 3932

Опубликована: Апрель 13, 2022

The present work studies an axisymmetric rotating truncated cone made of functionally graded (FG) porous materials reinforced by graphene platelets (GPLs) under a thermal loading. problem is tackled theoretically based on classical linear thermoelasticity approach. consists layered material with uniform or non-uniform dispersion GPLs in metal matrix open-cell internal pores, whose effective properties are determined according to the extended rule mixture and modified Halpin–Tsai model. A finite element method (FEM) Rayleigh–Ritz energy formulation Crank–Nicolson algorithm here applied solve both time space domain. thermo-mechanical response checked for different porosity distributions (uniform graded), together types GPL patterns across thickness. parametric study performed analyze effect coefficients, weight fractions GPL, semi-vertex angles cone, circular velocity, thermal, kinematic, stress structural member.

Язык: Английский

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On the vibrational analysis of combined paraboloidal-conical air vehicle segment shell-type structures

Aerospace Science and Technology, Год журнала: 2022, Номер 129, С. 107823 - 107823

Опубликована: Авг. 22, 2022

Язык: Английский

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On vibrational-based numerical simulation of a jet engine cowl shell-like structure

Mechanics of Advanced Materials and Structures, Год журнала: 2022, Номер 30(19), С. 4016 - 4027

Опубликована: Июнь 14, 2022

The present research proposes an applicable and impressive analytical model of Aircraft Engine Cowl (AEC) due to auspicate its frequency parameter. For the first time, authors configured structure AEC by joining two well-known shapes shell, including elliptical conical. This procedure is implemented obtaining governing motion organization differential equations affiliated with Joined Elliptical-Conical Shells (JECS) in line first-order shear deformation theory (FSDT) General Shell Formulation (GSF). Moreover, Functionally Graded Materials (FGMs) various spreading forms along structure’s thickness are used enhance dynamic performance AEC. It worth mentioning that recognized Rule Mixture (RM) engaged for achieving equivalent mechanical characteristics FGM. Finally, a semi-analytical Generalized Differential Quadrature (GDQ) hired extract resulting system access free vibration responses diverse Boundary Conditions (BCs). interesting numerical done inspect remnants geometric material features on oscillation demeanor structures. will be verified projected can helpful AEC’s analysis extendable other types studies predict structure's static treatment.

Язык: Английский

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