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Journal ArticleDOI

Maximization of fundamental frequency of axially compressed laminated curved panels with cutouts

TLDR
In this article, a free vibration analysis of laminated curved panels with central circular cutouts and subjected to axial compressive forces is carried out by employing the Abaqus finite element program.
Abstract
Free vibration analyses of laminated curved panels with central circular cutouts and subjected to axial compressive forces are carried out by employing the Abaqus finite element program. The fundamental frequencies of these composite laminated curved panels with a given material system are then maximized with respect to fiber orientations by using the golden section method. Through parametric studies, the significant influences of the panel aspect ratio, the panel curvature, the cutout size and the compressive force on the maximum fundamental frequencies, the optimal fiber orientations and the associated fundamental vibration modes of these panels are demonstrated and discussed.

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Citations
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Journal ArticleDOI

A critical assessment of Kriging model variants for high-fidelity uncertainty quantification in dynamics of composite shells

TL;DR: In this paper, a critical comparative assessment of Kriging model variants for surrogate based uncertainty propagation considering stochastic natural frequencies of composite doubly curved shells is presented, where the effect of noise in uncertainty propagation is addressed by using the Stochastic kriging.
Journal ArticleDOI

Stochastic free vibration analyses of composite shallow doubly curved shells – A Kriging model approach

TL;DR: In this paper, the Kriging model approach for stochastic free vibration analysis of composite shallow doubly curved shells is presented. And the convergence studies and error analysis are carried out to ensure the accuracy of present approach.
Journal ArticleDOI

Effect of cutout on stochastic natural frequency of composite curved panels

TL;DR: In this article, support vector regression (SVR) based uncertainty quantification (UQ) algorithm in conjunction with Latin hypercube sampling is developed to achieve computational efficiency for laminated composite curved panels with cutout.
Journal ArticleDOI

Aerothermoelastic analysis of nonlinear composite laminated panel with aerodynamic heating in hypersonic flow

TL;DR: In this paper, the effects of the shock wave on the aerodynamic properties of a nonlinear laminated panel were investigated using Hamilton's principle to establish the aero-thermal-elastic model of the panel.
Journal ArticleDOI

Maximum fundamental frequency of thick laminated composite plates by a hybrid optimization method

TL;DR: In this article, a combined method is introduced to obtain maximum fundamental frequency of thick laminated composite plates via finding optimum fibers orientation, the governing equations are obtained based on the higher order shear deformation theory (HSDT).
References
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Book

Concepts and Applications of Finite Element Analysis

TL;DR: In this article, the authors present a formal notation for one-dimensional elements in structural dynamics and vibrational properties of a structural system, including the following: 1. Isoparametric Elements.
Book

Elements of Structural Optimization

TL;DR: In this article, the authors present an approach for the optimization of structural components of a ten-bar truss and a twenty-five-bar trestle in the context of structural optimization.
Book

Numerical Optimization Techniques for Engineering Design: With Applications

TL;DR: This book contains the edited version of lectures and selected papers presented at the NATO ADVANCED STUDY INSTITUTE on computer aided optimal design: Structural and Mechanical Systems, held in Tr6ia, Portugal, 29th June to 11th July 1986.
Journal ArticleDOI

Structural synthesis - Its genesis and development

TL;DR: An historical account is given of the development, from its conception in 1960, of the structural synthesis method, and such elementary applications of synthesis methods as the three-bar truss, an integrally stiffened waffle plate, a stiffened cylindrical shell, and an idealized delta wing are given.
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