出版社:International Digital Organization for Scientific Information Publications
摘要:In this paper, for optimization and decreasing of the weight of Military Mobile Bridges (MMB),
numerical simulations of laminated composite plate, which is more applicable in manufacturing of deck of
MMB were done. The maximum deflection and stress are of the major parameters that are taken in to
account in the plates design. Final purpose of this paper is to obtain suitable mechanical property of
composite plates. To reach to this purpose, the behavior of laminated composite plates under pressure
loading is studied by using two numerical simulations. In Primary stage, Sightly plates have been solved by
finite element simulation using the ANSYS software which applies the First order Shear Deformation
Theory (FSDT) and the results have been compared with the results of finite difference method using the
MATLAB software which applies the Classical Laminate Plate Theory (CLPT). The plates have been
evaluated with actual condition of problem such as distributed load, under two clamp boundary conditions
with different layers. The effects of fiber orientation, number of layers and stiffness ratio on the
displacement and stress response of symmetric and anti-symmetric laminated composite plates subjected to
uniformly pressure loads are presented. The deflection of central point of plates becomes minimum for
90/0° fiber orientation with 5 layers. The thickness of individual layers plays an important role in the
response of the plate and stiffness ratio of 20 which it’s for composite material of Carbon Reinforce Fiber
Polymer (CFRP). At result, application the composite material of CARBON/Epoxy is suitable for bridge
deck where it has been extreme of strength apposite minimum density.
关键词:Military Mobile Bridge (MMB) · finite element method · finite difference method · laminate ·
composite materials