Results 231 to 240 of about 7,520 (261)
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THERMAL BUCKLING OF CLAMPED CYLINDRICAL PANELS BASED ON FIRST-ORDER SHEAR DEFORMATION THEORY
International Journal of Structural Stability and Dynamics, 2004Based on the first-order shear deformation shell theory, an analytical approach is developed to predict the thermal buckling response of an all-edge clamped cylindrical panel. The analytical approach adopts a double Fourier solution method suitable for cylindrical panels.
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Composite Structures, 2016
Abstract In this article an analytical solution is presented for power output from a piezoelectric shallow shell energy harvester using higher order shear deformation theory (HSDT). The energy harvester is made of an elastic substrate layer coupled with one or two surface bonded piezoelectric layers.
Hassan Sayyaadi +2 more
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Abstract In this article an analytical solution is presented for power output from a piezoelectric shallow shell energy harvester using higher order shear deformation theory (HSDT). The energy harvester is made of an elastic substrate layer coupled with one or two surface bonded piezoelectric layers.
Hassan Sayyaadi +2 more
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International Journal of Mechanical Sciences, 2019
Abstract A general higher-order shear deformation zig-zag theory is proposed for predicting the nonlinear aerothermoelastic characteristics of composite laminated panels subjected to supersonic airflow. The von Karman strains are employed to describe the structural nonlinearity of the panels, and the quasi-steady first-order piston theory is adopted ...
Fangtao Xie +4 more
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Abstract A general higher-order shear deformation zig-zag theory is proposed for predicting the nonlinear aerothermoelastic characteristics of composite laminated panels subjected to supersonic airflow. The von Karman strains are employed to describe the structural nonlinearity of the panels, and the quasi-steady first-order piston theory is adopted ...
Fangtao Xie +4 more
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Composite Structures, 2013
Abstract The main aim of this paper is to provide a general framework for the formulation and the dynamic analysis computations of moderately thick laminated doubly-curved shells and panels. A 2D higher-order shear deformation theory is also proposed and the differential geometry is used to define the arbitrary shape of the middle surface of shells ...
VIOLA, ERASMO +2 more
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Abstract The main aim of this paper is to provide a general framework for the formulation and the dynamic analysis computations of moderately thick laminated doubly-curved shells and panels. A 2D higher-order shear deformation theory is also proposed and the differential geometry is used to define the arbitrary shape of the middle surface of shells ...
VIOLA, ERASMO +2 more
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Composite Structures, 2013
Abstract This paper investigates the static analysis of doubly-curved laminated composite shells and panels. A theoretical formulation of 2D Higher-order Shear Deformation Theory (HSDT) is developed. The middle surface of shells and panels is described by means of the differential geometry tool.
VIOLA, ERASMO +2 more
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Abstract This paper investigates the static analysis of doubly-curved laminated composite shells and panels. A theoretical formulation of 2D Higher-order Shear Deformation Theory (HSDT) is developed. The middle surface of shells and panels is described by means of the differential geometry tool.
VIOLA, ERASMO +2 more
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Composite Structures, 2016
Abstract This paper presents an aeroelastic analysis of carbon nanotube (CNT) reinforced functionally graded composite panels in supersonic airflow using a higher-order shear deformation theory. There are four types of CNT distributions considered in this investigation.
Z.G. Song, L.W. Zhang, K.M. Liew
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Abstract This paper presents an aeroelastic analysis of carbon nanotube (CNT) reinforced functionally graded composite panels in supersonic airflow using a higher-order shear deformation theory. There are four types of CNT distributions considered in this investigation.
Z.G. Song, L.W. Zhang, K.M. Liew
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Composite Structures, 2020
Abstract This work studies large amplitude free vibration of piezoelectric laminated doubly curved panels reinforced with zigzag/armchair graphene sheets under uniform temperature rise. Thermomechanical and kinematic relations are derived using refined Halpin-Tsai approach and Amabili-Reddy (fourth-order shear deformation) theory which remains all ...
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Abstract This work studies large amplitude free vibration of piezoelectric laminated doubly curved panels reinforced with zigzag/armchair graphene sheets under uniform temperature rise. Thermomechanical and kinematic relations are derived using refined Halpin-Tsai approach and Amabili-Reddy (fourth-order shear deformation) theory which remains all ...
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Acta Mechanica
zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Shayan Mannani +2 more
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zbMATH Open Web Interface contents unavailable due to conflicting licenses.
Shayan Mannani +2 more
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Cyclic behaviour of demountable metallic corrugated shear panel dampers
Journal of Building Engineering, 2022Chaochao Quan
exaly