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B. N. Fedulov

Researcher at Moscow State University

Publications -  37
Citations -  256

B. N. Fedulov is an academic researcher from Moscow State University. The author has contributed to research in topics: Residual stress & Epoxy. The author has an hindex of 8, co-authored 34 publications receiving 175 citations. Previous affiliations of B. N. Fedulov include Skolkovo Institute of Science and Technology & Moscow Aviation Institute.

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Influence of fibre misalignment and voids on composite laminate strength

TL;DR: In this paper, the effects of manufacturing defects of laminate composite materials on the first-ply failure load and ultimate strength of the laminate, which are calculated using finite element modelling with Zinoviev's damage model, were investigated.
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Nonlinear anisotropic elasticity for laminate composites

TL;DR: In this article, the dependence of nonlinear elastic response of composite materials on loading conditions is studied and several approaches to model elastic nonlinearity such as different stiffness for particular type of loadings and nonlinear shear stress-strain relations are considered.
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Failure analysis of laminated composites based on degradation parameters

TL;DR: A number of assumptions to build up a theory for failure prediction in laminated composites are presented, which are generalized enough to serve as the basis for explanation of current models and for further development of modelling theory.
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Optimization of parts manufactured using continuous fiber three-dimensional printing technology

TL;DR: In this article, a topology optimization framework for continuous composite fiber 3D printing is presented, which allows optimization of parts within complex computer-aided design models and considers different types of nonlinearities in the finite-element model.
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Nonlinear shear behavior and failure of composite materials under plane stress conditions

TL;DR: In this paper, an analysis of the nonlinear response of the composite material with stress concentrator and its influence on stress distribution and damage evaluation during specimen loading is performed. But the results are limited to the case of an open hole composite plate under compression loading.