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Speaker : Prof. Seung-Jo Kim (Dept. of Aerospace Engineering, Seoul National University)
Subject : Numerical Simulation of Mechanical Behavior of Composite Structures by Parallel Supercomputing Technology
Date : Jun 5, 2006 2:00pm-3:30pm (Lecture room 72, Faculty of Engineering bldg.7, Hongo campus)
Outline : This paper will examine the possibilities of the virtual tests of composite structures by simulating mechanical (macro and/or micro) behaviors by using supercomputing technologies which now become easily available and powerful but relatively inexpensive. In this paper, we will describe mainly the applications of large scale finite element analysis for the direct numerical simulation(DNS) of the composite structures using parallel supercomputing technology. DNS utilizes the numerical simulation techniques by describing composite material properties from individual constituent properties, and develop the modeling tools for micromechanical material simulations. The numerical modeling examples using a direct numerical simulation (DNS) in this paper are various composite materials such as metal matrix composite(MMC), Active Fiber Composites(AFC), Boron/Epoxy Cross-ply Laminates and 3D orthogonal woven composites to predict the mechanical properties and structural behaviors of various composite structures. The DNS is an approach based on the full microscopic concepts, which can provide detailed information about the local interaction between the constituents and micro-failure mechanisms by separate modeling of each constituent. Such a 3D full micro-mechanical modeling is sometimes helpful to various analyses related to the material characterization and various structural behaviors from unidirectional laminate composites to 3D woven composites.
In this paper, the effective elastic moduli of the composites such as fiber reinforced laminates, active fiber composites and 3D orthogonal woven composites are determined using the DNS models by large scale finite element analysis. This DNS models can also give the global and local information about deformations and influences of high local in-plane and interlaminar stresses induced by transverse impact loading at a microscopic level inside the materials. Furthermore, the multiscale models based on DNS concepts considering microscopic and macroscopic structures simultaneously are also developed and a numerical low velocity impact simulation is performed using these multiscale DNS models. Through these various applications of DNS models, it can be shown that DNS approach can provide insights of various structural behaviors of composite structures.

Contact address
Department of Aeronautics and Astronautics (Graduate School of Frontier Sciences)
Nobuo Takeda
takeda@smart.k.u-tokyo.ac.jp
Tel: +81-3-5841-6642

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