نتایج جستجو برای: composite laminate

تعداد نتایج: 123142  

2016
Ender Akan Bora Bagis

Progress in adhesive technologies has made possible to perform more conservative restoration techniques. Bonded porcelain veneers have been widely used to address aesthetic dental problems for more than 3 decades1,2. Aesthetic parameter plays an important role when deciding the treatment choice of a patient with diastema. Development of the adhesive materials allows the dentist to construct mor...

2017
M Karray C Poilane M Gargouri P Picart

A method for real time 3D measurements based on three-color digital holographic interferometry is presented and applied to the investigation of fracture mechanisms in laminate composite submitted to a three point flexural loading. A convolution algorithm allows the three monochrome images to be superposed to provide simultaneous full-field 3D measurements. Experimental results are presented and...

Journal: :Journal of the Royal Society, Interface 2012
Elham Hamed Iwona Jasiuk Andrew Yoo Yikhan Lee Tadeusz Liszka

We model trabecular bone as a nanocomposite material with hierarchical structure and predict its elastic properties at different structural scales. The analysis involves a bottom-up multi-scale approach, starting with nanoscale (mineralized collagen fibril) and moving up the scales to sub-microscale (single lamella), microscale (single trabecula) and mesoscale (trabecular bone) levels. Continuu...

Journal: :علوم و تکنولوژی پلیمر 0
احمدرضا قاسمی رسول باقرصاد محمدرضا وزیری سرشک

the residual stresses in composite laminates depend on several factors including the conditions of fabricating process, property of materials, direction and lay-ups of the layers. however the thermo-elastic behavior of composite is one of the most important parameters affecting the magnitude of residual stresses. the elastic properties and residual stresses do not remain constant under cyclic t...

2001
S Durvasula

In this paper, a method of solution and some numerical resu~s of free vibration and buckling of composite laminates are presented. All the edges of the laminates are assumed as simply supported. Ritz's method of solution is used with deflection surface expressed in terms of double series in Chebyshev polynomials satisfying the simply supported laminate boundary conditions. The numerical results...

Journal: :Aeronautics and Aerospace Open Access Journal 2018

Journal: :Composites Part A: Applied Science and Manufacturing 2016

Journal: :Journal of The Korean Society for Composite Materials 2012

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