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A. Soleiman Fallah
Researcher at Imperial College London
Publications - 6
Citations - 178
A. Soleiman Fallah is an academic researcher from Imperial College London. The author has contributed to research in topics: Finite element method & Ultimate tensile strength. The author has an hindex of 5, co-authored 6 publications receiving 150 citations.
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Journal ArticleDOI
Pressure–impulse diagrams for elastic-plastic-hardening and softening single-degree-of-freedom models subjected to blast loading
A. Soleiman Fallah,Luke A. Louca +1 more
TL;DR: In this paper, a dimensionless parameter has been used to categorize the response into elastic, elastic-plastic-hardening, elasticplastic softening, rigid-PLS, rigidplastic hardening, and rigid-polysilicon softening.
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Analytical–numerical study of interfacial stresses in plated beams subjected to pulse loading
TL;DR: In this article, the spatial and temporal distributions of shear and normal interfacial stresses in a plated beam subjected to pulse loading were investigated and the results for three pulse loading cases have been compared to finite element analyses and reasonable correlation is observed.
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Inelastic deformation and failure of partially strengthened profiled blast walls
TL;DR: In this article, a rapid assessment tool is presented to evaluate the effect of a composite patch on the deformation response of profiled blast walls, which is based on a previous analytical formulation for unstrengthened walls with realistic connection systems.
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An investigation of interfacial stresses in adhesively-bonded single lap joints subject to transverse pulse loading
TL;DR: In this article, an analytical model is developed to estimate the peel and shear stresses in an isotropic elastic adhesive in a single lap joint subjected to transverse pulse loads.
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Characterization of the Mechanical Behavior of a Polymer-Based Laminate and Constituent Fibers at Various Quasi-Static Strain Rates
TL;DR: The mechanical characterization of Dyneema HB26 is described, which shows the in-plane tensile, compressive, and shear stress-strain behavior and strength of the laminate at low rates has been determined experimentally.