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Maryam Shokravi, Speaker at Materials Science Conferences
Energy Institute of Higher Education, Iran (Islamic Republic of)
Title : Dynamic buckling of smart sandwich beam subjected to electric field based on hyperbolic piezoelasticity theory

Abstract:

CNTs have superior properties such as high tensile strengths, high aspect ratio, high stiffness and low density and however, can be used as the reinforce phase for the composite materials. In this paper, dynamic buckling of the smart subjected to blast load subjected to electric field is studied. The effect of CNTs on the forced vibration of micro cylindrical shell is presented. In nano and micro scales, considering size effect is essential. The sandwich structure is rested on Pasternak foundation with springs and shear elements. Applying piezoelasticity theory and hyperbolic shear deformation beam theory (HSDBT), the motion equations are derived by energy method. For calculating the dynamic instability region (DIR) of the sandwich structure, differential quadrature method (DQM) along with Bolotin method is used. The effect of different parameters including CNTs volume percent and distribution type, boundary conditions, size effect and length to thickness ratio on the frequency response of the of the system was studied. It can be concluded that the FGX pattern was the best choice compared to other cases. It was observed that increasing the CNT volume fraction increases the frequency and decreases the deflection of the structure. As can be seen the deflection of the strain gradient theory was lower than couple stress and the deflection of the couple stress was lower than classical one. In addition, by increasing the material length scale parameter, the amplitude of the system will be reduced. Furthermore, by considering CC boundary condition, the maximum amplitude decreases and the frequency is increased. Beam the geometry of the embedded micro cylindrical shell with radius, R, length, L, and thickness h. The structure is reinforced by FG-CNTs and is subjected to harmonic load. The structure is made from Poly methyl methacrylate (PMMA) with the constant Poisson’s ratios of vm = 0.34, temperature-dependent thermal coefficient of αm = (1 + 0.0005ΔT)×
10?6/K, and temperature-dependent Young moduli of Em =(3.52?0.0034T)GPa in which T=T0 +ΔT and T0 = 300 K (room temperature) (Madani et al. 2016). The effect of distribution type of CNT on the frequency response of the structure is shown.

Audience take Away Notes: 

  • Sandwich structures can be used in different industries such as aerospace, aircraft, automobile and etc due to high strength and low weight with respect to traditional materials
  • One of the important ways for control of the sandwich structures, is using piezoelectric materials since in these materials, the structure subjected to mechanical forces can produces the electric field and vice versa.
  • The mathematical modeling of nanocomposite structures and the pursuit of numerical solutions represent a pivotal frontier in materials science and engineering
  • Nanocomposites, characterized by the incorporation of nanoscale reinforcements into a matrix material, exhibit unique mechanical, thermal, and electrical properties, offering a broad spectrum of applications in various industries
  • The intricate interplay of nanoscale phenomena demands advanced mathematical models to accurately capture the behavior of these structures under different conditions. The development of robust numerical solutions is essential for predicting and understanding the complex responses of nanocomposite materials
  • This field not only explores the fundamental principles governing nanocomposite behavior but also addresses practical engineering challenges. As researchers delve into this subject, they contribute to the advancement of innovative materials with tailored properties, influencing the design and optimization of nanocomposite-based technologies across diverse domains, including aerospace, electronics, and healthcare
  • The importance of this research lies in its potential to unlock new frontiers in material science, enabling the creation of advanced materials with enhanced performance characteristics and expanded applications

Biography:

Maryam Shokravi  received his PhD.degrees from University of Kashan in the field of mechanical engineering. She spent her sabbatical period at Northeastern University in Boston, USA. She has an extensive teaching experience, having served as a faculty member at Buein Zahra Technical University. Her courses taught include Strength of Material, Statics, Vibration, and dynamic analyses of various structures. Maryam has received several honors and awards. Maryam has an impressive list of  publications in reputable  journals and conferences, covering topics such as vibrations, buckling, and dynamic analyses of various structures, including nanocomposites, sandwich plates, and cylindrical shells. 

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