scispace - formally typeset
T

Tomohiro Yokozeki

Researcher at University of Tokyo

Publications -  220
Citations -  4422

Tomohiro Yokozeki is an academic researcher from University of Tokyo. The author has contributed to research in topics: Composite laminates & Epoxy. The author has an hindex of 30, co-authored 193 publications receiving 3273 citations. Previous affiliations of Tomohiro Yokozeki include Japan Aerospace Exploration Agency.

Papers
More filters
Journal ArticleDOI

Improved mechanical properties of carbon fiber/graphene oxide-epoxy hybrid composites

TL;DR: In this article, a carbon fiber/graphene oxide-epoxy hybrid composites were used to improve the mechanical properties of polymer composites, and graphene oxide was used as one of the filler for the development of carbon fiber composite.
Journal ArticleDOI

Mechanical properties of corrugated composites for candidate materials of flexible wing structures

TL;DR: In this paper, a simple analytical model for the initial stiffness of the corrugated composites is developed, and the predictions are compared with the experimental results, and some improvements, installing of stiff rod and flexible rubber, are attempted for the creation of smooth aerodynamic surface and the improvement of stiffness.
Journal ArticleDOI

Mechanical properties of CFRP laminates manufactured from unidirectional prepregs using CSCNT-dispersed epoxy

TL;DR: In this article, the experimental results of the mechanical properties of three-phase CFRP laminates consisting of traditional carbon fibers and epoxy matrix modified using cup-stacked carbon nanotubes (CSCNTs) in comparison to those of CFRP without CSCNT are presented.
Journal ArticleDOI

Experimental characterization of strength and damage resistance properties of thin-ply carbon fiber/toughened epoxy laminates

TL;DR: In this article, the authors investigated several strength properties as well as the damage resistance properties of carbon fiber/toughened epoxy composite laminates for the applicability of thin-ply prepregs to aircraft structures.
Journal ArticleDOI

Matrix cracking behaviors in carbon fiber/epoxy laminates filled with cup-stacked carbon nanotubes (CSCNTs)

TL;DR: In this paper, the authors investigated the damage accumulation behaviors in carbon fiber reinforced nanocomposite laminates under tensile loading and found that the dispersion of CSCNT resulted in fracture toughness improvement and residual thermal strain decrease, which is considered to cause the retardation of matrix crack formation.