Finite element model analysis of composite materials reinforced with different shape nanopaper

2019 ◽  
Author(s):  
Aying Zhang ◽  
Zhenghong Li
2017 ◽  
Vol 62 (2/3/4) ◽  
pp. 155
Author(s):  
Albert Oliver ◽  
Raúl Arasa ◽  
Agustí Pérez Foguet ◽  
Mª Ángeles González

2016 ◽  
Vol 115 ◽  
pp. 1-8 ◽  
Author(s):  
Cynthia J. Mitchell ◽  
Lisa M. Dangora ◽  
James A. Sherwood

Author(s):  
Mozammil Hussain ◽  
Ralph E. Gay ◽  
Kai-Nan An ◽  
Rodger Tepe

Many neck pain complaints are associated with degenerated discs in cervical spine. Disc degeneration (DD) consists of cascading stages of events with complex changes in disc tissue properties. This results in deterioration of the ability of the disc to perform its function normally. Several biomechanical and biochemical changes occur in the disc with degeneration. Increase in motion segment stiffness and peak stresses in the posterior annulus are some of the gross changes that occur in the disc with degeneration.


2018 ◽  
Vol 2 (3) ◽  
pp. 53
Author(s):  
Josh Kelly ◽  
Edward Cyr ◽  
Mohsen Mohammadi

Composite materials have recently been of particular interest to the automotive industry due to their high strength-to-weight ratio and versatility. Among the different composite materials used in mass-produced vehicles are sheet moulded compound (SMC) composites, which consist of random fibres, making them inexpensive candidates for non-structural applications in future vehicles. In this work, SMC composite materials were prepared with varying fibre orientations and volume fractions (25% and 45%) and subjected to a series of uniaxial tensile and flexural bending tests at a strain rate of 3 × 10−3 s−1. Tensile strength as well as failure strain increased with the increasing fibre volume fraction for the uniaxial tests. Flexural strength was found to also increase with increasing fibre percentage; however, failure displacement was found to decrease. The two material directions studied—longitudinal and transverse—showed superior strength and failure strain/displacement in the transverse direction. The experimental results were then used to create a finite element model to describe the deformation behaviour of SMC composites. Tensile results were first used to create and calibrate the model; then, the model was validated with flexural experimental results. The finite element model closely predicted both SMC volume fraction samples, predicting the failure force and displacement with less than 3.5% error in the lower volume fraction tests, and 6.6% error in the higher volume fraction tests.


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