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Johannes Reiner

Researcher at Deakin University

Publications -  43
Citations -  492

Johannes Reiner is an academic researcher from Deakin University. The author has contributed to research in topics: Composite laminates & Finite element method. The author has an hindex of 8, co-authored 27 publications receiving 205 citations. Previous affiliations of Johannes Reiner include University of Queensland & University of British Columbia.

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Theory-guided machine learning for damage characterization of composites

TL;DR: A novel approach for damage characterization through machine learning is presented where theoretical knowledge of failure and strain-softening is linked to the macroscopic response of quasi-isotropic composite laminates in over-height compact tension tests, demonstrating the effectiveness of machine learning to reduce experimental efforts forDamage characterization in composites.
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A study of energy dissipating mechanisms in orthogonal cutting of UD-CFRP composites

TL;DR: In this article, a three-dimensional thermo-mechanical finite element (FE) model is presented for the orthogonal cutting simulation of unidirectional carbon fiber reinforced polymer (UD-CFRP) materials.
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Progressive damage analysis of composite structures using higher-order layer-wise elements

TL;DR: In this article, the authors developed a numerical framework for the simulation of damage in composite structures using explicit time integration, where Lagrange polynomials are used to represent the displacement field through the thickness of each ply, resulting in a layer-wise element model.
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Experimental and numerical analysis of drop-weight low-velocity impact tests on hybrid titanium composite laminates

TL;DR: In this paper, an experimental and numerical study on low-velocity impact responses on [Ti/0/90]s hybrid titanium composite laminates (HTCLs) is presented.
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Comparison of two progressive damage models for studying the notched behavior of composite laminates under tension

TL;DR: In this article, two continuum damage models with different underlying assumptions are investigated to assess their predictive capabilities and limitations with respect to progressive intra-laminar damage in notched IM7/8552 CFRP composite laminates under tension.