Evgeny V. Morozov
Other affiliations: Australian Defence Force Academy, University of KwaZulu-Natal, Russian State Hydrometeorological University ...read more
Bio: Evgeny V. Morozov is an academic researcher from University of New South Wales. The author has contributed to research in topics: Orthotropic material & Galerkin method. The author has an hindex of 25, co-authored 147 publications receiving 2445 citations. Previous affiliations of Evgeny V. Morozov include Australian Defence Force Academy & University of KwaZulu-Natal.
Papers published on a yearly basis
01 Jan 2001
TL;DR: In this paper, the authors discuss failure criteria and strength of laminates and optimal composite structures for failure detection and failure detection in unidirectional and non-unidirectionally-pilated solids.
Abstract: Preface. Introduction. Fundamentals of Mechanics of Solids. Mechanics of a Unidirectional Ply. Mechanics of a Composite Layer. Mechanics of Laminates. Failure Criteria and Strength of Laminates. Environmental, Special Loading, and Manufacturing Effects. Optimal Composite Structures. Name Index. Subject Index.
19 Jun 2013
TL;DR: Advanced Mechanics of Composite Materials and Structural Elements as discussed by the authors analyzes contemporary theoretical models at the micro-and macro levels of material structure and provides a comprehensive coverage of practical methods and approaches, experimental results, and optimization of composite material properties and structural component performance.
Abstract: Advanced Mechanics of Composite Materials and Structural Elements analyzes contemporary theoretical models at the micro- and macro levels of material structure. Its coverage of practical methods and approaches, experimental results, and optimization of composite material properties and structural component performance can be put to practical use by researchers and engineers. The third edition of the book consists of twelve chapters progressively covering all structural levels of composite materials from their constituents through elementary plies and layers to laminates and laminated composite structural elements. All-new coverage of beams, plates and shells adds significant currency to researchers. Composite materials have been the basis of many significant breakthroughs in industrial applications, particularly in aerospace structures, over the past forty years. Their high strength-to-weight and stiffness-to-weight ratios are the main material characteristics that attract the attention of the structural and design engineers. Advanced Mechanics of Composite Materials and Structural Elements helps ensure that researchers and engineers can continue to innovate in this vital field. It includes detailed physical and mathematical coverage of complex mechanics and analysis that required in actual applications - not just standard homogeneous isotropic materials. It covers environmental and manufacturing discussions that enable practical implementation within manufacturing technology, experimental results, and design specifications. It discusses material behavior impacts in-depth such as nonlinear elasticity, plasticity, creep, structural nonlinearity enabling research and application of the special problems of material micro- and macro-mechanics.
01 Jan 2007
TL;DR: In this article, the authors present the results of more than 30 years practical experience in the field of design and analysis of composite materials and structures and present a detailed and comprehensive coverage of the contemporary theoretical models at the micro-and macro-level of material structure, practical methods and approaches, experimental results, and optimisation of composite material properties and component performance.
Abstract: Composite materials have been representing most significant breakthroughs in various industrial applications, particularly in aerospace structures, during the past thirty five years. The primary goal of "Advanced Mechanics of Composite Materials" is the combined presentation of advanced mechanics, manufacturing technology, and analysis of composite materials. This approach lets the engineer take into account the essential mechanical properties of the material itself and special features of practical implementation, including manufacturing technology, experimental results, and design characteristics.This title gives complete coverage of the topic: from basics and fundamentals to the advanced analysis including practical design and engineering applications. At the same time, it includes a detailed and comprehensive coverage of the contemporary theoretical models at the micro- and macro- levels of material structure, practical methods and approaches, experimental results, and optimisation of composite material properties and component performance. The authors present the results of more than 30 year practical experience in the field of design and analysis of composite materials and structures. It also includes: eight chapters progressively covering all structural levels of composite materials from their components through elementary plies and layers to laminates; detailed presentation of advanced mechanics of composite materials; and, emphasis on nonlinear material models (elasticity, plasticity, creep) and structural nonlinearity.
TL;DR: In this paper, the buckling behavior of anisogrid composite lattice cylindrical shells under axial compression, transverse bending, pure bending, and torsion was investigated.
Abstract: The paper investigates the buckling behaviour of anisogrid composite lattice cylindrical shells under axial compression, transverse bending, pure bending, and torsion. The lattice shells are modelled as three-dimensional frame structures composed of curvilinear ribs subjected to the tension/compression, bending in two planes and torsion. The specialised finite-element model generation procedure (model generator/design modeller) is developed to control the orientation of the beam elements allowing the original twisted geometry of the curvilinear ribs to be closely approximated. The effects of varying the length of the shells, the number of helical ribs and the angles of their orientation on the buckling behaviour of lattice structures are examined using parametric analyses. Buckling of the lattice shells with cutouts is also analysed. The results of these studies indicate that the modelling approach presented in this work can be successfully applied to the solution of design problems.
TL;DR: In this paper, a finite element (FE) model is developed for the progressive failure analysis of composite laminates, which includes in-ply and delamination damage effects, and a combined elastoplastic damage model is used to represent the mechanical response of composite layers and is implemented in the FE code Abaqus using user-defined material subroutine UMAT.
Abstract: A finite element (FE) model, which includes in-ply and delamination damage effects, is developed for the progressive failure analysis of composite laminates. A combined elastoplastic damage model which accounts for both plasticity and damage effects is used to represent the mechanical response of composite layers and is implemented in the FE code Abaqus using user-defined material subroutine UMAT. A cohesive zone model based on cohesive elements available in Abaqus is employed to simulate delamination behaviour in the adhesive interfaces. Continuum shell elements and cohesive elements are stacked together to simulate composite and adhesive layers, respectively. The model is applied to the progressive failure analysis of AS4/PEEK composite laminates subjected to in-plane tensile and out-of-plane transverse low-velocity impact loadings. It is shown that the model can be successfully applied to the simulations of composite laminates susceptible to delamination failure.
TL;DR: This book by a teacher of statistics (as well as a consultant for "experimenters") is a comprehensive study of the philosophical background for the statistical design of experiment.
Abstract: THE DESIGN AND ANALYSIS OF EXPERIMENTS. By Oscar Kempthorne. New York, John Wiley and Sons, Inc., 1952. 631 pp. $8.50. This book by a teacher of statistics (as well as a consultant for \"experimenters\") is a comprehensive study of the philosophical background for the statistical design of experiment. It is necessary to have some facility with algebraic notation and manipulation to be able to use the volume intelligently. The problems are presented from the theoretical point of view, without such practical examples as would be helpful for those not acquainted with mathematics. The mathematical justification for the techniques is given. As a somewhat advanced treatment of the design and analysis of experiments, this volume will be interesting and helpful for many who approach statistics theoretically as well as practically. With emphasis on the \"why,\" and with description given broadly, the author relates the subject matter to the general theory of statistics and to the general problem of experimental inference. MARGARET J. ROBERTSON
24 May 2005
TL;DR: Linear Elastic Stress-Strain Relations Elastic Constants Based on Micromechanics, Plane Stress, Global Coordinate System, Elastic Constant Based on Global Coordinated System, Laminate Analysis - Part I- Laminate analysis - Part II- Effective Elastic Constant of a Laminate- Failure Theories of a Laminating System, Homogenization of Composite Materials, to Damage Mechanics of composite Materials as discussed by the authors.
Abstract: Linear Elastic Stress-Strain Relations- Elastic Constants Based on Micromechanics- Plane Stress- Global Coordinate System- Elastic Constants Based on Global Coordinate System- Laminate Analysis - Part I- Laminate Analysis - Part II- Effective Elastic Constants of a Laminate- Failure Theories of a Lamina- to Homogenization of Composite Materials- to Damage Mechanics of Composite Materials
02 Nov 2005
TL;DR: In this article, the authors presented a comprehensive analysis of the four Elastic Moduli coefficients of a Unidirectional Lamina Coefficients of Thermal Expansion and Moisture Expansion.
Abstract: INTRODUCTION TO COMPOSITE MATERIALS Chapter Objectives Introduction Classi?cation Recycling Fiber-Reinforced Composites Mechanics Terminology Summary Key Terms Exercise Set References MACROMECHANICAL ANALYSIS OF A LAMINA Chapter Objectives Introduction Review of De?nitions Hooke's Law for Different Types of Materials Hooke's Law for a Two-Dimensional Unidirectional Lamina Hooke's Law for a Two-Dimensional Angle Lamina Engineering Constants of an Angle Lamina Invariant Form of Stiffness and Compliance Matrices for an Angle Lamina Strength Failure Theories of an Angle Lamina Hygrothermal Stresses and Strains in a Lamina Summary Key Terms Exercise Set References APPENDIX A: MATRIX ALGEBRA Key Terms APPENDIX B: TRANSFORMATION OF STRESSES AND STRAINS Transformation of Stress Transformation of Strains Key Terms MICROMECHANICAL ANALYSIS OF A LAMINA Chapter Objectives Introduction Volume and Mass Fractions, Density, and Void Content Evaluation of the Four Elastic Moduli Ultimate Strengths of a Unidirectional Lamina Coefficients of Thermal Expansion Coefficients of Moisture Expansion Summary Key Terms Exercise Set References MACROMECHANICAL ANALYSIS OF LAMINATES Chapter Objectives Introduction Laminate Code Stress-Strain Relations for a Laminate In-Plane and Flexural Modulus of a Laminate Hygrothermal Effects in a Laminate Summary Key Terms Exercise Set References FAILURE, ANALYSIS, AND DESIGN OF LAMINATES Chapter Objectives Introduction Special Cases of Laminates Failure Criterion for a Laminate Design of a Laminated Composite Other Mechanical Design Issues Summary Key Terms Exercise Set References BENDING OF BEAMS Chapter Objectives Introduction Symmetric Beams Nonsymmetric Beams Summary Key Terms Exercise Set References INDEX
TL;DR: A review of the state-of-the-art in the area of dynamic analysis of composite shells can be found in this article, where the main aim is to provide a broad perspective of the current state of the art in this field.
Abstract: Laminated composite shells are frequently used in various engineering applications in the aerospace, mechanical, marine, and automotive industries. This article follows a previous book and review articles published by the leading author (Qatu, 2004, 2002, 1989, 1992, 1999 [1–5]). It reviews most of the research done in recent years (2000–2009) on the dynamic behavior (including vibration) of composite shells. This review is conducted with emphasis on the type of testing or analysis performed (free vibration, impact, transient, shock, etc.), complicating effects in material (damping, piezoelectric, etc.) and structure (stiffened shells, etc.), and the various shell geometries that are subjected to dynamic research (cylindrical, conical, spherical and others). A general discussion of the various theories (classical, shear deformation, 3D, non-linear etc.) is also given. The main aim of this review article is to collate the research performed in the area of dynamic analyses of composite shells during the last 10 years, thereby giving a broad perspective of the state of art in this field. This review article contains close to 200 references.
01 Jan 2016
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