M
M. Ravandi
Researcher at K.N.Toosi University of Technology
Publications - 14
Citations - 384
M. Ravandi is an academic researcher from K.N.Toosi University of Technology. The author has contributed to research in topics: Epoxy & Fiber. The author has an hindex of 5, co-authored 11 publications receiving 269 citations. Previous affiliations of M. Ravandi include University of Michigan & National University of Singapore.
Papers
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Low velocity impact performance of stitched flax/epoxy composite laminates
TL;DR: In this paper, the effect of yarn stitching on the low-velocity impact response of the woven flax/epoxy composite laminates with the purpose of extending their use to higher performance applications was investigated.
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Effects of hybridization and hybrid fibre dispersion on the mechanical properties of woven flax-carbon epoxy at low carbon fibre volume fractions
TL;DR: In this article, the effects of interlaminar hybrid fiber dispersion on tensile performance of hybrid laminates with single carbon plies interspersed with flax plies were investigated, and the results suggested that morphology of mating hybrid plies might affect stiffness in woven fabrics.
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The effects of through-the-thickness stitching on the Mode I interlaminar fracture toughness of flax/epoxy composite laminates
TL;DR: In this paper, the effects of stitching using natural fibres on the interlaminar fracture toughness and tensile properties of flax fiber/epoxy composite laminates were experimentally studied.
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Effect of interlayer carbon fiber dispersion on the low-velocity impact performance of woven flax-carbon hybrid composites:
TL;DR: In this article, the effects of interlayer hybrid fiber dispersion on the impact response of carbon-flax epoxy hybrid laminates at low carbon volume fractions were investigated.
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Prediction of Mode I interlaminar fracture toughness of stitched flax fiber composites
TL;DR: In this paper, a simulation procedure is proposed to predict the interlaminar fracture toughness of stitched flax fiber composites through a virtual double cantilever beam test, where two-node beam elements are superposed onto the cohesive interface of the parent laminate at a prescribed stitch density and distribution.