Nonlinear three-dimensional stability characteristics of geometrically imperfect nanoshells under axial compression and surface residual stress

dc.contributor.authorShahzad, Muhammad Atif
dc.contributor.authorSafaei, Babak
dc.contributor.authorSahmani, Saeid
dc.contributor.authorBasingab, Mohammed Salem
dc.contributor.authorHameed, Abdul Zubar
dc.date.accessioned2026-02-06T18:26:29Z
dc.date.issued2023
dc.departmentDoğu Akdeniz Üniversitesi
dc.description.abstractThrough reduction of thickness value in nanostructures, the features of surface elasticity become more prominent due to having a high surface-to-volume ratio. The main aim of this research work was to examine the surface residual stress effect on the three-dimensional nonlinear stability characteristics of geometrically perfect and imperfect cylindrical shells at nanoscale under axial compression. To do so, an unconventional threedimensional shell model was established via combination of the three-dimensional shell formulations and the GurtinMurdoch theory of elasticity. The silicon material is selected as a case study, which is the most utilized material in the design of micro-electromechanically systems. Then, the moving Kriging meshfree approach was applied to take numerically into account the surface free energy effects and the initial geometrical imperfection in the threedimensional nonlinear stability curves. Accordingly, the considered cylindrical shell domain was discretized via a set of nodes together using the quadratic polynomial type of basis shape functions and an appropriate correlation function. It was found that the surface stress effects lead to an increase the critical axial buckling load of a perfect silicon nanoshell about 82.4% for the shell thickness of 2 nm, about 32.4% for the shell thickness of 5 nm, about 15.8% for the shell thickness of 10 nm, and about 7.5% for the shell thickness of 20 nm. These enhancements in the value of the critical axial buckling load for a geometrically imperfect silicon nanoshell become about 92.9% for the shell thickness of 2 nm, about 36.5% for the shell thickness of 5 nm, about 17.7% for the shell thickness of 10 nm, and about 8.8% for the shell thickness of 20 nm.
dc.description.sponsorshipMinistry of Education in Saudi Arabia [IFPRC-047-135-2020]; King Abdulaziz University,DSR, Jeddah, Saudi Arabia
dc.description.sponsorshipThis research work was funded by the Deanship for Research and Innovation, Ministry of Education in Saudi Arabia, through the project numberIFPRC-047-135-2020and King Abdulaziz University,DSR, Jeddah, Saudi Arabia.
dc.identifier.doi10.1515/ntrev-2022-0551
dc.identifier.issn2191-9089
dc.identifier.issn2191-9097
dc.identifier.issue1
dc.identifier.orcid0000-0002-1675-4902
dc.identifier.scopus2-s2.0-85162119882
dc.identifier.scopusqualityQ1
dc.identifier.urihttps://doi.org/10.1515/ntrev-2022-0551
dc.identifier.urihttps://hdl.handle.net/11129/10498
dc.identifier.volume12
dc.identifier.wosWOS:001005421900001
dc.identifier.wosqualityQ1
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherDe Gruyter Poland Sp Z O O
dc.relation.ispartofNanotechnology Reviews
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/openAccess
dc.snmzKA_WoS_20260204
dc.subjectnanostructures
dc.subject3D elasticity
dc.subjectnonlinear buckling
dc.subjectsurface residual stress
dc.subjectmeshfree numerical technique
dc.titleNonlinear three-dimensional stability characteristics of geometrically imperfect nanoshells under axial compression and surface residual stress
dc.typeArticle

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