Results 31 to 40 of about 9,711 (260)
Buckling And Postbuckling Of An Imperfect Plate Subjected To The Shear Load
The stability analysis of an imperfect plate subjected to the shear load is presented. To solve this problem, a specialized computer program based on FEM has been created.
Psotný Martin
doaj +1 more source
Postbuckling analysis of variable angle tow (VAT) composite plates [PDF]
Variable angle tow (VAT) placement techniques provide the designer with the ability to tailor the point-wise stiffness properties of composite laminates according to structural design requirements.
Raju, Gangadharan +2 more
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Simulating Postbuckling Behaviour and Collapse of Stiffened CFRP Panels [PDF]
Advanced composite materials are well known for their outstanding potential in weight-related stiffness and strength leading to an ever increasing share in aerospace structural components out of Carbon Fibre Reinforced Plastics (CFRP).
Degenhardt, Richard, Rohwer, Klaus
core
Approximate Stability Analysis of Omega‐Stringer Stiffened Composite Panels
ABSTRACT Thin‐walled composite structures are widely used in weight‐critical applications such as aircraft and spacecraft. However, ensuring the stability of such structures under various load cases remains a key challenge in their design and optimization.
Cherine El Yaakoubi‐Mesbah +1 more
wiley +1 more source
Postbuckling behaviour of graphene-reinforced plate with interfacial effect
The present study is aimed to study the postbuckling response of the graphene sheet (GS)-reinforced plate including the effect of van-der-Waals (vdW) bonding between GS and matrix.
A. Kumar Srivastava, D. Kumar
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For the first time, simultaneous influences of porosities, tangential constraints of boundary edges, surrounding elastic media and elevated temperature on the buckling and postbuckling behaviors of a functionally graded toroidal shell segment are ...
L.T. Nhu Trang, H. Van Tung
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Postbuckling behavior of graphite-epoxy panels [PDF]
Structurally efficient fuselage panels are often designed to allow buckling to occur at applied loads below ultimate. Interest in applying graphite-epoxy materials to fuselage primary structure led to several studies of the post-buckling behavior of ...
Dickson, J. N. +2 more
core +1 more source
ABSTRACT The structural design optimization aims for robust structures with minimal use of material resources, leading to slender and thin‐walled structures, which entail a higher risk of stability problems. This issue is further influenced by geometrical imperfections, which are subjected to uncertainties.
Maximilian Schweizer +3 more
wiley +1 more source
Recently, graphene sheets have shown significant potential for environmental engineering applications such as wastewater treatment. In the present work, the posbuckling response of orthotropic single-layered graphene sheet (SLGS) is investigated in a ...
S.R. Asemi, M. Mohammadi, A. Farajpour
doaj +1 more source
The use of damage as a design parameter for postbuckling composite aerospace structures [PDF]
Advanced fibre-reinforced polymer composites have seen a rapid increase in use in aircraft structures in recent years due their high specific strength and stiffness, amongst other properties.
Degenhardt, Richard +2 more
core

