A comparison of three Algorithms for Tracing Nonlinear Equilibrium Paths of Structural Systems [PDF]
The relative efficiencies of the Riks/Wempner, Crisfield, and normal flow solution algorithms for tracking nonlinear equilibrium paths of structural systems are compared.
Gürdal, Z., Ragon, S.A., Watson, L.T.
core +1 more source
Stability Analysis of Thin-Walled Perforated Composite Columns Using Finite Element Method. [PDF]
Falkowicz K.
europepmc +1 more source
Load-shortening behavior of an initially curved eccentrically loaded column [PDF]
To explore the feasibility of using buckled columns to provide a soft support system for simulating a free-free boundary condition in dynamic testing, the nonlinear load-shortening behavior of initially imperfect, eccentrically loaded slender columns is ...
Fichter, W. B., Pinson, Mark W.
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Analysis and design for the moderately deep postbuckling behavior of composite plates [PDF]
It is widely acknowledged that tracking the postbuckling response of structures made from thin plates can be problematical. Such difficulty is associated with highly nonlinear effects, including mode jumping, imperfection sensitivity, and their combined ...
Raju, Gangadharan +2 more
core +3 more sources
This study investigates the nonlinear behavior of functionally graded graphene platelet-reinforced composite (FG-GPLRC) thin cylindrical shells stiffened by orthogonal or spiral FG-GPLRC stiffeners under axial compression.
Kieu Quang Thai +4 more
doaj +1 more source
Analysis of webs of partial-tension-field beams subjected to lateral pressure loadings [PDF]
Webs of partial-tension-field beams subjected to lateral pressure ...
Furuike, T. +3 more
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DNA fluctuations reveal the size and dynamics of topological domains. [PDF]
Vanderlinden W +5 more
europepmc +1 more source
Developments in impact damage modeling for laminated composite structures [PDF]
Damage tolerance is the most critical technical issue for composite fuselage structures studied in the Advanced Technology Composite Aircraft Structures (ATCAS) program.
Avery, William B. +3 more
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Local Buckling of Thin-Walled Column of Square Cross-Section Made of In-Plane Coupled Laminate. [PDF]
The non–symmetric, general laminate exhibits different types of coupling between the extension, shearing, bending and twisting. For practical reasons, the in–plane coupled laminate is a particularly interesting.
Kołakowski, Zbigniew +2 more
core
Numerical Investigations of Perforated CFRP Z-Cross-Section Profiles, under Axial Compression. [PDF]
Falkowicz K.
europepmc +1 more source

