On the Buckling and Initial Postbuckling Behavior of Shallow Spherical and Conical Sandwich Shells
, 1972 The boundary-value problems associated with the axisymmetrical, asymmetrical, and initial postbuckling behavior of the clamped shallow conical sandwich shell under a uniform pressure are developed for face sheets of the same material and equal ...
N. Akkas
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Stability Analysis of Shear Deformable Inhomogeneous Nanocomposite Cylindrical Shells under Hydrostatic Pressure in Thermal Environment. [PDF]
Materials (Basel), 2023 Sofiyev AH, Fantuzzi N.
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Buckling and Postbuckling of Composite Plates Under Shear Load [PDF]
, 1990 A theoretical and experimental investigation of the buckling and postbuckling response of laminated composite plates under uniform, inplane shear load is ...
Kosteletos, Stefanos
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Nonlinear Thermal/Mechanical Buckling of Orthotropic Annular/Circular Nanoplate with the Nonlocal Strain Gradient Model. [PDF]
Micromachines (Basel), 2023 Sadeghian M, Palevicius A, Janusas G.
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Delamination buckling, postbuckling, and growth in axially loaded beam-plates
, 1987 The purpose of this study is to develop a simple one-dimensional model to analyze axially loaded beam-plates containing cracks which extend through the thickness of the beam-plates.
Wolfe, David R.
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MODELING OF NONLINEAR DEFORMATION AND BUCKLING OF ELASTIC INHOMOGENEITIES SHELLS
Structural Mechanics of Engineering Constructions and Buildings, 2014 He paper outlines the fundamentals of the method of solving static problems of geomet- rically nonlinear deformation, buckling, and postbuckling behavior of thin thermoelastic in- homogeneous shells with complex-shaped mid-surface, geometrical features ...
V A Bazhenov +3 more
doaj
Free Vibration Analysis of Functionally Graded Porous Cylindrical Panels Reinforced with Graphene Platelets. [PDF]
Nanomaterials (Basel), 2023 Cho JR.
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Progresses and Challenges of Composite Laminates in Thin-Walled Structures: A Systematic Review. [PDF]
ACS Omega, 2023 Ahmed OS +4 more
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New design tools for lightweight aerospace structures
, 2004 This paper presents two new design tools for lightweight aerospace structures. The first tool is the Tailored Fibre Placement (TFP) design tool TACO. It is used to optimize the fibre orientations of structures made of Carbon Fibre Reinforcement Plastics (
Temmen, Hubert +5 more
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Dynamic analysis of thick plates reinforced with agglomerated GNPs. [PDF]
Heliyon, 2023 Alnujaie A +9 more
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