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Showing papers by "J. N. Reddy published in 1999"


Journal ArticleDOI
TL;DR: In this article, a study on the vibration of cylindrical shells made of a functionally gradient material (FGM) composed of stainless steel and nickel is presented, the objective is to study the natural frequencies, the influence of constituent volume fractions and the effects of configurations of the constituent materials on the frequencies.

726 citations


01 Jan 1999
TL;DR: The theory and analysis of Euler-Bernoulli Beams and Timoshenko Beams is discussed in this article. But the analysis of the classical plate theory is not considered.
Abstract: Preface 1.General Introduction and Preliminaries 2.Virtual Work Principles and Solution Methods 3.Theory and Analysis of Euler-Bernoulli Beams 4.Theory and Analysis of Timoshenko Beams 5.The Classical Plate Theory 6.The First Order Shear Deformation Theory 7.Variational Solutions of Plates 8.Finite Element Analysis of Beams and Plates 9.Refined Theories of Plates 10.Nonlinear Analysis of Beams and Plates Subject Index

460 citations


Journal ArticleDOI
J. N. Reddy1
TL;DR: In this article, a simple negative velocity feed back control algorithm coupling the direct and converse piezoelectric effects is used to actively control the dynamic response of an integrated structure through closed loop control.

353 citations


Journal ArticleDOI
TL;DR: In this article, the authors studied axisymmetric bending and stretching of annular circular plates using the first-order shear deformation Mindlin plate theory and provided the solutions for deflections, force and moment resultants in terms of the corresponding quantities of isotropic plates based on the classical Kirchhoff plate theory.
Abstract: Axisymmetric bending and stretching of functionally graded solid and annular circular plates is studied using the first-order shear deformation Mindlin plate theory. The solutions for deflections, force and moment resultants of the first-order theory are presented in terms of the corresponding quantities of isotropic plates based on the classical Kirchhoff plate theory. This gives the Mindlin solution of functionally graded circular plates whenever the Kirchhoff solution to the problem is known. Numerical results for displacements and stresses are presented for various percentages of ceramic-metal volume fractions.

339 citations


Journal ArticleDOI
TL;DR: In this paper, the pseudodynamic thermoelastic response of functionally graded ceramic-metal cylinders is studied and a finite-element formulation of the 1D, axisymmetric heat transfer equation and the thermo-elastic radial boundary value problem is presented.
Abstract: The pseudodynamic thermoelastic response of functionally graded ceramic-metal cylinders is studied. This paper presents the finite-element formulation of the 1D, axisymmetric heat transfer equation and the thermoelastic radial boundary value problem. A two-step solution of the governing equations of thermoelasticity is presented. Thermoelastic coupling is considered by taking into effect the temperature dependence of the constitutive equations. Nonlinearity due to the temperature dependence of the material properties of the constituent ceramic and metal is considered. A parametric study with respect to varying volume fraction of the metal is conducted. Temperature and radial/hoop stress distributions arising due to rapid heating of the inner surface of the functionally graded cylinder are presented.

127 citations


Journal ArticleDOI
TL;DR: In this article, a complete set of linear equations of the second-order theory of laminated composite plates are obtained, and a generalized Levy type solution in conjunction with the state space concept is used to analyze the free vibration behavior of cross-ply and antisymmetric angle-ply laminated plates.

121 citations


Journal ArticleDOI
TL;DR: In this paper, the impact response of functionally graded (FG) cylindrical shells with one layer or multi-layers is presented, which includes both contact deformation and transverse shear deformation.

111 citations


Journal ArticleDOI
TL;DR: In this paper, the dynamic stability of simply-supported, isotropic cylindrical panels under combined static and periodic axial forces is investigated, and the effects of the thickness-to-radius ratio on the instability regions are examined in detail.

56 citations


Journal ArticleDOI
J. N. Reddy1
TL;DR: In this paper, various finite element models of the Timoshenko beam theory for static analysis are reviewed, and a novel derivation of the 4 × 4 stiffness matrix (for the pure bending case) of the superconvergent finite element model for static problems is presented using two alternative approaches: (1) an assumed-strain finite-element model of the conventional Timoshenkobeam theory, and (2) assumed-displacement finite elements model of a modified Timoshenko-beam theory.
Abstract: First, various finite element models of the Timoshenko beam theory for static analysis are reviewed, and a novel derivation of the 4 × 4 stiffness matrix (for the pure bending case) of the superconvergent finite element model for static problems is presented using two alternative approaches: (1) assumed-strain finite element model of the conventional Timoshenko beam theory, and (2) assumed-displacement finite element model of a modified Timoshenko beam theory. Next, dynamic versions of various finite element models are discussed. Numerical results for natural frequencies of simply supported beams are presented to evaluate various Timoshenko beam finite elements. It is found that the reduced integration element predicts the natural frequencies accurately, provided a sufficient number of elements is used.

41 citations


Journal ArticleDOI
TL;DR: In this article, a layerwise displacement finite element with enhanced strains is used to determine deflections and interface model using the penalty function method is developed to determine interlaminar stresses and strain energy release rates to study delaminations.

39 citations


Book ChapterDOI
J. N. Reddy1
01 Jan 1999
TL;DR: In fiber-reinforced composites, fibers are the principal loadcarrying members, and the matrix material keeps the fibers together, acts as a load-transfer medium between fibers, and protects fibers from being exposed to the environment as mentioned in this paper.
Abstract: Composite materials consist of two or more materials which together produce desirable properties that may not be achieved with any of the constituents alone. Fiber-reinforced composite materials, for example, consist of high strength and high modulus fibers in a matrix material. Reinforced steel bars embedded in concrete provide an example of fiber-reinforced composites. In these composites, fibers are the principal loadcarrying members, and the matrix material keeps the fibers together, acts as a load-transfer medium between fibers, and protects fibers from being exposed to the environment (e.g., moisture, humidity, etc.).

Journal ArticleDOI
TL;DR: In this paper, the state-space approach in conjunction with the Jordan canonical form is presented to obtain exact solutions for the thermoelastic response of cross-ply composite beams for arbitrary boundary conditions and subjected to general temperature fields.
Abstract: Thermal deformations in symmetric and antisymmetric cross-ply beams are investigated. The state-space approach in conjunction with the Jordan canonical form is presented to obtain exact solutions for the thermoelastic response of cross-ply composite beams for arbitrary boundary conditions and subjected to general temperature fields. The classical, first-, second-, and third-order beam theories are used in the analysis. As a demonstrative example, deflections are computed for beams with various lamination schemes and boundary conditions undergoing linearly varying temperature through the thickness.

Journal ArticleDOI
TL;DR: In this article, a four-noded quadrilateral CO strain plate element for the analysis of thick laminated composite plates is presented, which is based on the third-order shear deformation theory and the assumed strain element formulation.
Abstract: This paper presents a four-noded quadrilateral CO strain plate element for the analysis of thick laminated composite plates. The element formulation is based on: 1) the third-order shear deformation theory; 2) assumed strain element formulation; and 3) interrelated edge displacements and rotations along element boundaries. Unlike the existing displacement-type composite plate elements based on the third-order theory, which rely on the C-1-continuity formulation, the present plate element is of C-0-continuity, and its element stiffness matrix is evaluated explicitly. Because of the third-order expansion of the in-plane displacements through the thickness, the resulting theory and hence elements do not need shear correction factors. The explicit element stiffness matrix makes the present element more computationally efficient than the composite plate elements using numerical integration for the analysis of thick layered composite plates.