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Michel Geradin

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Beschreibung

Mechanical Vibrations: Theory and Application to Structural Dynamics, Third Edition is a comprehensively updated new edition of the popular textbook. It presents the theory of vibrations in the context of structural analysis and covers applications in mechanical and aerospace engineering.

Key features include:

  • A systematic approach to dynamic reduction and substructuring, based on duality between mechanical and admittance concepts
  • An introduction to experimental modal analysis and identification methods
  • An improved, more physical presentation of wave propagation phenomena
  • A comprehensive presentation of current practice for solving large eigenproblems, focusing on the efficient linear solution of large, sparse and possibly singular systems
  • A deeply revised description of time integration schemes, providing framework for the rigorous accuracy/stability analysis of now widely used algorithms such as HHT and Generalized-α
  • Solved exercises and end of chapter homework problems
  • A companion website hosting supplementary material

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Veröffentlichungsjahr: 2014

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Table of Contents

Title Page

Copyright

Foreword

Preface

Introduction

Suggested bibliography

List of main symbols and definitions

Chapter 1: Analytical Dynamics of Discrete Systems

Definitions

1.1 Principle of virtual work for a particle

1.2 Extension to a system of particles

1.3 Hamilton's principle for conservative systems and Lagrange equations

1.4 Lagrange equations in the general case

1.5 Lagrange equations for impulsive loading

1.6 Dynamics of constrained systems

1.7 Exercises

References

Chapter 2: Undamped Vibrations of n-Degree-of-Freedom Systems

Definitions

2.1 Linear vibrations about an equilibrium configuration

2.2 Normal modes of vibration

2.3 Orthogonality of vibration eigenmodes

2.4 Vector and matrix spectral expansions using eigenmodes

2.5 Free vibrations induced by nonzero initial conditions

2.6 Response to applied forces: forced harmonic response

2.7 Response to applied forces: response in the time domain

2.8 Modal approximations of dynamic responses

2.9 Response to support motion

2.10 Variational methods for eigenvalue characterization

2.11 Conservative rotating systems

Exercises

References

Chapter 3: Damped Vibrations of n-Degree-of-Freedom Systems

Definitions

3.1 Damped oscillations in terms of normal eigensolutions of the undamped system

3.2 Forced harmonic response

3.3 State-space formulation of damped systems

3.4 Experimental methods of modal identification

3.5 Exercises

3.6 Proposed exercises

References

Chapter 4: Continuous Systems

Definitions

4.1 Kinematic description of the dynamic behaviour of continuous systems: Hamilton's principle

4.2 Free vibrations of linear continuous systems and response to external excitation

4.3 One-dimensional continuous systems

4.4 Bending vibrations of thin plates

4.5 Wave propagation in a homogeneous elastic medium

4.6 Solved exercises

4.7 Proposed exercises

References

Chapter 5: Approximation of Continuous Systems by Displacement Methods

Definitions

5.1 The Rayleigh–Ritz method

5.2 Applications of the Rayleigh–Ritz method to continuous systems

5.3 The finite element method

5.4 Exercises

References

Chapter 6: Solution Methods for the Eigenvalue Problem

Definitions

6.1 General considerations

6.2 Dynamical and symmetric iteration matrices

6.3 Computing the determinant: Sturm sequences

6.4 Matrix transformation methods

6.5 Iteration on eigenvectors: the power algorithm

6.6 Solution methods for a linear set of equations

6.7 Practical aspects of inverse iteration methods

6.8 Subspace construction methods

6.9 Dynamic reduction and substructuring

6.10 Error bounds to eigenvalues

6.11 Sensitivity of eigensolutions, model updating and dynamic optimization

6.12 Exercises

References

Chapter 7: Direct Time-Integration Methods

Definitions

7.1 Linear multistep integration methods

7.2 One-step formulas for second-order systems: Newmark's family

7.3 Equilibrium averaging methods

7.4 Energy conservation

7.5 Explicit time integration using the central difference algorithm

7.6 The nonlinear case

7.7 Exercises

References

Author Index

Subject Index

End User License Agreement

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Guide

Cover

Table of Contents

Foreword

Preface

Introduction

Begin Reading

List of Illustrations

Figure 1

Figure 1.1

Figure 1.2

Figure 1.3

Figure 1.4

Figure 1.5

Figure 1.6

Figure 1.7

Figure 1.8

Figure 1.9

Figure 1.10

Figure 1.11

Figure 1.12

Figure 1.13

Figure 1.14

Figure 1.15

Figure 2.1

Figure 2.2

Figure 2.3

Figure 2.4

Figure 2.5

Figure 2.6

Figure 2.7

Figure 2.8

Figure 2.9

Figure 2.10

Figure 2.11

Figure 2.12

Figure 2.13

Figure 2.14

Figure 2.15

Figure 2.16

Figure 2.17

Figure 2.18

Figure 3.1

Figure 3.2

Figure 3.3

Figure 3.4

Figure 3.5

Figure 3.6

Figure 3.7

Figure 3.8

Figure 3.9

Figure 3.10

Figure 3.11

Figure 3.12

Figure 3.13

Figure 3.14

Figure 3.15

Figure 3.16

Figure 3.17

Figure 3.18

Figure 3.19

Figure 3.20

Figure 4.1

Figure 4.2

Figure 4.3

Figure 4.4

Figure 4.5

Figure 4.6

Figure 4.7

Figure 4.8

Figure 4.9

Figure 4.10

Figure 4.12

Figure 4.13

Figure 4.14

Figure 4.15

Figure 4.16

Figure 4.17

Figure 4.18

Figure 4.19

Figure 4.20

Figure 4.21

Figure 4.22

Figure 4.23

Figure 4.24

Figure 4.25

Figure 4.27

Figure 4.28

Figure 4.29

Figure 4.30

Figure 4.31

Figure 4.32

Figure 4.33

Figure 4.34

Figure 4.35

Figure 4.36

Figure 4.37

Figure 4.38

Figure 4.39

Figure 4.40

Figure 4.41

Figure 4.42

Figure 4.43

Figure 4.44

Figure 4.45

Figure 4.46

Figure 4.47

Figure 4.48

Figure 4.49

Figure 4.50

Figure 4.51

Figure 4.52

Figure 4.53

Figure 4.54

Figure 4.55

Figure 4.56

Figure 4.57

Figure 4.58

Figure 5.1

Figure 5.2

Figure 5.3

Figure 5.4

Figure 5.5

Figure 5.6

Figure 5.7

Figure 5.8

Figure 5.9

Figure 5.10

Figure 5.11

Figure 5.12

Figure 5.13

Figure 5.14

Figure 5.16

Figure 5.15

Figure 5.20

Figure 5.21

Figure 5.22

Figure 5.23

Figure 5.24

Figure 5.25

Figure 5.26

Figure 5.27

Figure 5.28

Figure 5.29

Figure 5.30

Figure 5.31

Figure 6.1

Figure 6.2

Figure 6.3

Figure 6.4

Figure 6.5

Figure 6.6

Figure 6.7

Figure 6.8

Figure 6.9

Figure 6.10

Figure 6.11

Figure 6.12

Figure 6.15

Figure 7.1

Figure 7.2

Figure 7.3

Figure 7.4

Figure 7.5

Figure 7.6

Figure 7.7

Figure 7.8

Figure 7.10

Figure 7.11

Figure 7.13

Figure 7.14

Figure 7.15

Figure 7.16

Figure 7.17

Figure 7.18

Figure 7.19

Figure 7.20

Figure 7.21

Figure 7.22

Figure 7.23

Figure 7.26

List of Tables

Table 2.1

Table 2.2

Table 3.1

Table 4.1

Table 4.3

Table 5.2

Table 5.3

Table 5.4

Table 5.6

Table 6.1

Table 6.3

Table 7.1

Mechanical Vibrations

Theory and Application to Structural Dynamics

Third Edition

Michel Geradin

University of Liège, Belgium

Daniel J. Rixen

Technische Universität München, Germany

This edition first published 2015

© 2015 John Wiley & Sons, Ltd

Second Edition published in 1997

© 1997 John Wiley & Sons, Ltd

Registered office

John Wiley & Sons Ltd, The Atrium, Southern Gate, Chichester, West Sussex, PO19 8SQ, United Kingdom

For details of our global editorial offices, for customer services and for information about how to apply for permission to reuse the copyright material in this book please see our website at www.wiley.com.

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All rights reserved. No part of this publication may be reproduced, stored in a retrieval system, or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording or otherwise, except as permitted by the UK Copyright, Designs and Patents Act 1988, without the prior permission of the publisher.

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Limit of Liability/Disclaimer of Warranty: While the publisher and author have used their best efforts in preparing this book, they make no representations or warranties with respect to the accuracy or completeness of the contents of this book and specifically disclaim any implied warranties of merchantability or fitness for a particular purpose. It is sold on the understanding that the publisher is not engaged in rendering professional services and neither the publisher nor the author shall be liable for damages arising herefrom. If professional advice or other expert assistance is required, the services of a competent professional should be sought.

Library of Congress Cataloging-in-Publication Data

Géradin, Michel, 1945—

Mechanical vibrations : theory and application to structural dynamics / Michel Géradin, Daniel J. Rixen.— Third edition.

pages cm

Includes bibliographical references and index.

ISBN 978-1-118-90020-8 (hardback)

1. Structural dynamics. I. Rixen, Daniel. II. Title.

TA654.G45 2014

624.1'76—dc23

2014014588

A catalogue record for this book is available from the British Library.

ISBN: 978-1-118-90020-8

Foreword

The first two editions of this book had seven skillfully written chapters, organized in my mind in three parts. Collectively, they aimed at giving the reader a coherent presentation of the theory of vibrations and associated computational methods, in the context of structural analysis. The first part covered the analytical dynamics of discrete systems, and both undamped and damped vibrations of multiple-degree-of-freedom systems. It also served as a good introduction to the second part, which consisted of two chapters. The first one focused on the dynamics of continuous systems and covered the subject of wave propagation in elastic media. It was followed by a chapter which bridged this topic with the first part of the book, by introducing the novice to the concept of displacement methods for semi-discretizing continuous systems. It also culminated with a brief and yet well-executed initiation to the finite element method. All this led to the third part of the book, which indulged into a concise and effective treatment of classical numerical methods for the solution of vibration problems in both frequency and time domains. Covering all of these topics in a unified approach, making them interesting to both students and practitioners, including occasional references to experimental settings wherever appropriate, and delivering all this in less than 400 pages, was a daunting challenge that the authors had brilliantly met. For this reason, the previous editions of this book have been my favourite educational publication on this subject matter. I have used them to teach this topic at the MS level, first at the University of Colorado at Boulder, then at Stanford University.

So what can one expect from a third edition of this book?

In its third edition, the overall organization of this book and that of its chapters has remained mostly unchanged. However, several enhancements have been made to its technical content. The notion of the response of a system to a given input has been refined throughout the text, and its connections to the concepts of dynamic reduction and substructuring (which remain timely) have been made easier to observe, follow, and understand. Chapter 3 has gained a new section on experimental methods for modal analysis and some associated essentials in signal processing and system identification. The mathematical content of Chapter 6 has been somehow refreshed, and its scope has been enhanced by two welcome enrichments. The first one is a new section on linear equation solvers with particular emphasis on singular systems. Such systems arise not only in many mechanical and aerospace engineering problems where the structure of interest is only partially restrained or even unrestrained, but also as artifacts of many modern computational methods for structural analysis and structural dynamics. The second enrichment brought to Chapter 6 is an updated section on the analysis of the sensitivity of frequencies and mode shapes to parameters of interest, and its association with model updating. Most importantly, the third edition comes now with carefully designed problem sets (and occasionally some solutions) that will certainly enhance both processes of teaching and learning. Overall, the third edition has added about 150 pages of technical content that make it a better textbook for students and teachers, a useful reference for practitioners, and a source of inspiration for researchers.

Charbel FarhatStanford University1 January 2014

Preface

This monograph results from a complete recasting of a book on Mechanical Vibrations, initially written in French and published by Masson Éditions in 1992 under the title Théorie des vibrations, Application à la dynamique des structures. The first edition in English was issued shortly after, thanks to the support of DIST (French Ministry of Scientific Research and Space) and published by John Wiley & Sons in 1994. The book was indubitably felt to fill a gap since both editions were a success in France as well as internationally, so that both versions were almost immediately followed by a second edition by the same publishers: in French in 1996, and in 1997 for the English version. Due to the short delay between editions, only minor changes—essentially corrections—took place between the first and second versions of the manuscript.

The numerous constructive comments received from readers —university colleagues, students and practising engineers— during the following decade convinced both of us that a deep revision of the original manuscript was definitely needed to meet their expectations. Of course there were still remaining errors to be corrected—and the very last one will never be discovered, error-making being a common trait of human beings— and more rigor and accuracy had to be brought here and there in the presentation and discussion of the concepts. But the subject of mechanical vibration has also rapidly evolved, rendering the necessity of the addition of some new important topics. Proposed exercises to help, on the one hand, teachers explain the quintessence of dynamics and, on the other hand, students to assimilate the concepts through examples were also missing.

We were already planning to produce this third edition in French in the early 2000s, but the project could never be achieved due to overwhelming professional duties for both of us. The necessary time could finally be secured from 2010 (partly due to the retirement of the first author). However, priority has now been given to the English language for the writing of this third, entirely new edition since our perception was that the demand for a new, enhanced version comes essentially from the international market. We are indebted to Éditions Dunod for having agreed to release the rights accordingly.

We are thus pleased to present to our former readers a new edition which we hope will meet most of their expectations, and to offer our new readers a book that allows them to discover or improve their knowledge of the fascinating world of mechanical vibration and structural dynamics.

Without naming them explicitly, we express our gratitude to all those who have helped us to make this book a reality. Indeed, we received from many colleagues, friends and relatives much support, which could take various forms, such as a careful and critical reading of some parts, the provision of some examples and figures, appropriate advice whenever needed, personal support and, not the least, the understanding of our loved ones when stealing from them precious time to lead such a project to its very end.

Michel Géradin and Daniel J. RixenMünchen24 January 2014

Introduction

We owe to Lord Rayleigh the formulation of the principles relative to the theory of vibration such as they are applied and taught nowadays. In his remarkable treatise entitled Theory of Sound and published in 1877 he introduced the fundamental concept of oscillation of a linear system about an equilibrium configuration and showed the existence of vibration eigenmodes and eigenfrequencies for discrete as well as for continuous systems. His work remains valuable in many ways, even though he was concerned with acoustics rather than with structural mechanics.

Because of their constant aim to minimize the weight of flying structures, the pioneers of aeronautics were the first structural designers who needed to get vibration and structural dynamic problems under control. From the twenties onwards, aeronautical engineers had to admit the importance of the mechanics of vibration for predicting the aeroelastic behaviour of aircraft. Since then, the theory of vibration has become a significant subject in aeronautical studies. During the next forty years, they had to limit the scope of their analysis and apply methods that could be handled by the available computational means: the structural models used were either analytical or resulted from a description of the structure in terms of a small number of degrees of freedom by application of transfer or Rayleigh-Ritz techniques.

The appearance and the progressive popularization of computing hardware since 1960 have led to a reconsideration of the entire field of analysis methods for structural dynamics: the traditional methods have been replaced by matrix ones arising from the discretization of variational expressions. In particular, the tremendous advances in the finite element method for setting up structural models gave rise to the development of new computational methods to allow design engineers to cope with always increasing problem sizes.

Today, the elaboration of efficient computational models for the analysis of the dynamic behaviour of structures has become a routine task. To give an example, Figure 1 illustrates the computational prediction of the vibration modes of a stator section of an aircraft engine. The fineness of the finite element model has been adapted in this case for the needs of the associated stress analysis, the latter requiring a level of detail that is not really needed for a modal analysis. The eigenmode represented is a 3-diameter mode exhibiting a global deformation of the structure. What makes the modal analysis of such a structure very difficult is the high level of cyclic symmetry (resulting from the number of stator blades) which is responsible for the appearance of a high number of nearly equal eigenvalues.

Figure 1 Finite element model of a stator section of aircraft engine. Source: Reproduced with permission from Techspace Aero—SAFRAN Group.

Development of computing, acquisition and sensing hardware has led to a similar revolution in the field of experimental techniques for identification of vibrational characteristics of structures. For more than thirty years, experimental modal analysis techniques have been developed which are based either on force appropriation or on arbitrary excitation.

The methods for dynamic analysis, whether they are numerical or experimental, have now taken an important place everywhere in engineering. If they were rapidly accepted in disciplines such as civil engineering, mechanical design, nuclear engineering and automotive production where they are obviously needed, they have now become equally important in the design of any manufactured good, from the micro-electromechanical device to the large wind turbine.

From its origin in the early sixties, the aerospace department of the University of Liège (Belgium) has specialized mainly in structural mechanics in its education programme. This book results from more than twenty years of lecturing on the theory of vibration to the students of this branch. It is also based on experience gathered within the University of Liège's Laboratory for Aerospace Techniques in the development of computational algorithms designed for the dynamic analysis of structures by the finite element method and implemented in the structural analysis code the team of the laboratory has developed since 1965, the SAMCEF™ software.1

The content of the book is based on the lecture notes developed over the years by the first author and later formatted and augmented by one of his former students (the second author). This work reflects the teaching and research experience of both authors. In addition to his academic activity at the University of Liège, the first author has also spent several years as head of the European Laboratory for Safety Assessment at the Joint Research Centre in Ispra (Italy). The second author has accumulated until 2012 lecturing and research experience at the Delft Technical University (The Netherlands) and is currently pursuing his career at the Technische Universität München (Germany). The book has been adopted internationally as course reference in several universities.

Due to its very objective, the book has a slightly hybrid character: the concepts of vibration theory are presented mainly with the intention of applying them to dynamic analysis of structures and significant attention is paid to the corresponding methods. Even though the foundations of analytical mechanics are reviewed, a preliminary acquaintance with this subject is necessary. A good knowledge of matrix algebra and theory of complex numbers, calculus, structural mechanics and numerical analysis for linear systems is required. It is also assumed that the reader is familiar with the theory of the single-degree-of-freedom oscillator. However, the presentation of the finite element method is deliberately made simple since its study requires a course of its own. Finally, the very important fields of nonlinear vibration and random vibration have been intentionally omitted in the present text since they are highly specialized subjects.

What is new in this third edition?

Although the overall structure of the book, its organization into individual chapters and the main topics addressed, remain unchanged, this new version is the result of important revision work to achieve major improvements.

Regarding the theoretical content itself, the main changes with respect to the previous edition are the following:

The response of an either discrete or continuous system has been the object of deep rethinking and turned out to be a thread towards the important concepts of dynamic reduction and substructuring. The latter are explained and developed, starting from the observation that the response of a part from the overall system is the result either from an excitation of its support, or from the application of a set of loads at selected points of the structure. Such duality can be exploited in at least two ways. On the one hand, it allows a system description in terms of the classical concepts of mechanical impedance or admittance. On the other hand, it naturally leads to the concept of dynamic substructuring based on an expansion of the response in terms of the spectral content of the impedance and admittance relationships.

Experimental modal analysis is an essential ingredient in structural dynamics since it allows to confirm by experiment the structural properties predicted through numerical modelling. Therefore it was felt necessary to include in this new version of the book the essentials of signal processing and identification techniques that allow us to extract the spectral properties of a linear structure from measured dynamic responses.

In the same spirit, the concept of eigensolution sensitivity to physical parameters has been further detailed since it is the basis for the development of appropriate numerical tools for improving the numerical model of a real dynamic system.

The considerable evolution of the size of the structural systems to be considered for eigenvalue extraction and transient dynamic analysis in the context of large engineering projects had to be reflected and addressed properly. Models reaching the size of several millions of degrees of freedom (such as the one displayed on

Figure 1

) are now common practice. The efficiency of the eigenvalue solvers (such as the Lanczos method) and implicit time integrators (based on the Newmark family) depends for one part on the tuning of the algorithms themselves, but perhaps even more on the performance of the linear solvers that are used at each solution step. Therefore it was felt necessary to cover in a deeper manner the topic of linear solvers, introducing not only the principle of the algorithms but also their implementation taking into accountthe sparse character of the large sets of equations generated by finite element discretization. Much attention is also brought to the case of singular systems since they frequently occur in the context of structural dynamics.

The link that was made in the previous edition between vibration and wave propagation did not allow the reader to easily grasp the physical nature of the wave propagation phenomena that can occur in a continuous medium. The discussion of the fundamental cases of wave propagation in solids (both in one-dimensional and three-dimensional media) has thus been reviewed and better illustrated in order to improve the didactics of the presentation.

The presentation of the finite element method has still been limited to one-dimensional structures (bars, beams) since the main objective of the book is not to go deeply into finite element technology. The chapter devoted to it has, however, been complemented with the development of a beam element including the shear deformation. The motivation behind the presentation was to show that, as is often the case, remaining within the strict context of the variational principle of displacements leads to shortcomings which can easily be removed through the use of mixed variational formulations.

The stability and accuracy properties of the Newmark family of time integration algorithms have been revisited, their rigorous discussion being achieved in terms of the invariants of the amplification matrix. Also, it is shown that dissociating displacement interpolation and expression of equilibrium allows us to imbed most integration schemes of the Newmark family in the same formalism.

As a result, the original manuscript has been almost completely rewritten. The opportunity has been taken to improve or clarify the presentation whenever necessary, including the quality of the figures.

A great effort has been achieved to adopt throughout the manuscript notations that are as coherent and uniform as possible. Therefore a general list of notations and symbols is provided after this introduction. However it was still necessary in many cases to depart locally from these general conventions, and therefore to introduce in each chapter an additional list of local definitions that complements the general one.

Among the many constructive comments received regarding the previous editions, a major deficiency felt and reported by the users was the absence of exercises proposed to the reader. A few solved exercises are now detailed at the end of each chapter, and both teachers and students will certainly appreciate the fact that a number of selected problems are also suggested. The numerical solution of some of them requires the use of a numerical toolbox, in which case softwares such as MATLAB® or the Open Source ones OCTAVE® and SCILAB® are appropriate. Some others involve cumbersome analytical developments that are greatly facilitated by symbolic computation using software tools such as MAPLE® or MATHEMATICA®.

The content

The content of the book is organized as follows:

Chapter 1 is dedicated to analytical dynamics of discrete systems. Hamilton's principle is taken as a starting point: first the equations of motion are found for one particle and then those for a system of particles under kinematic constraints are derived. Considering the equations of motion in the Lagrangian form, the structure of the inertia terms and the classification of the forces are established. In the last two sections of the chapter, the less common case of impulsive loading of systems is dealt with and the method of Lagrange multipliers is introduced.

Chapter 2 discusses the undamped vibrations of -degree-of-freedom systems and begins by introducing the concepts of equilibrium position and of equilibrium configuration corresponding to steady motion. After a review of the classical concepts of eigenmodes and eigenfrequencies, some more specific aspects are considered: the forced harmonic response is developed and is shown to lead to the concepts of dynamic influence coefficient and mechanical impedance. The modal expansion technique is applied for calculating the dynamic response to transient external loading. It is shown that limiting the points of load application leads to the concept of reduced mechanical admittance. The case of systems excited through support motion is discussed in depth and also examined from the point of view of dynamic substructuring. Variational methods for characterizing the eigenvalues of a vibrating system are then discussed. The solution of the motion equations of rotating systems is considered in a specific section at the end of the chapter, with the main objective to show the existence of instability zones linked to the existence of gyroscopic forces.

Chapter 3 deals with the damped oscillations of -degree-of-freedom systems. First, the concept of lightly-damped systems and its equivalence to the modal damping assumption are discussed. Then the principles of modal identification through appropriate excitation and the characteristic phase-lag theory are outlined. The formulation of damped system equations in state-space form is developed in order to provide a suitable mathematical model for describing systems with arbitrarily large damping. In the last section, a basic presentation is made of the signal processing and identification techniques that are commonly used to best fit the parameters of the mathematical model from experimental measurements.

In Chapter 4, the theory of vibration is extended to the analysis of continuous systems, taking as a starting point the variational principle operating on displacements. The chapter begins by considering the case of three-dimensional continuous media: strain measure, stress–strain relationships, variational formulation and equations of motion. The effects of the second-order terms arising from the presence of an initial stress field are investigated in detail. Then the concepts of eigenmodes, eigenfrequencies and modal expansion are generalized to the continuous case. It is also shown that the principle of reciprocitycommonly described for structures under steady loading can be generalized to dynamics. In a major part of the chapter, a quite extensive study is made of some one-dimensional or two-dimensional continuous systems: the bar in extension, the vibrating string, the bending of a beam without and with shear deflection and finally the bending vibration of thin plates. Numerous examples of closed-form solutions are given and particular attention is devoted to the effects resulting from the rotation of beams and, for systems in bending, from initial extension. Their respective properties as one-dimensional wave guides are discussed. The last section provides an elementary presentation of wave propagation phenomena in an elastic medium, with a derivation of the fundamental solutions and a discussion of their physical meaning.

In Chapter 5, the approximation problem for continuous systems is investigated by means of displacement methods. First, the Rayleigh–Ritz method is reviewed and then applied to some classical problems such as the bar in extension, and the bending of a beam and of a thin plate. The case of prestressed structures is once more considered. The second part of the chapter is dedicated to an introduction to the finite element method, the principles of which are illustrated by several simple examples. The chapter ends with the more complex but instructive case of finite element modelling of the beam with shear deformation.

Chapter 6 deals with solution methods for the eigenvalue problem. After an introduction where a classification of the existing methods is suggested, a successive survey of the most classical methods is made and their related numerical aspects are discussed. The methods efficiently implemented in structural computation codes are pointed out, namely the subspace method and the Lanczos algorithm. A significant part of the chapter is devoted to the efficient solution of large, sparse linear systems since they form in fact the kernel of eigenvolvers based on inverse iteration such as Lanczos and subspace iteration. The particular case of singular structures is discussed in depth since frequently occurring in the context of structural dynamics. The methods of dynamic reduction and substructuring already introduced in Chapter 2 are discussed again, with three objectives in mind: to review the principle of dynamic reduction in a more general manner, to show that dual points of view can be adopted, depending upon the physical nature (displacement or force) of the primary variables and to propose dynamic reduction and substructuring as a practical approach for the solution of large problems of structural dynamics. A section is also devoted to the computation of error bounds to eigenvalues. The last section deals with the concept of eigensolution sensitivity to structural modifications.

Chapter 7 outlines some aspects of direct methods for integrating the transient dynamic response. After having introduced the concepts of stability and accuracy for an integration operator, it discusses the one-step formulas of Newmark's family. Their properties are analyzed as well as those of variants commonly used in structural analysis: the Hilber-Hugues-Taylor -method and the Generalized- variant which provides a neat way to introduce numerical damping in the model and the central difference integration scheme especially well adapted to impact problems. Eventually, there is a short discussion of the time integration of nonlinear systems.

The scope

The book has been devised to be used by senior undergraduate and graduate students. Therefore, the associated concepts are revealed by numerous simple examples. Nevertheless, although the text is primarily aimed at students, it is also dedicated to research and design engineers who wish to improve their understanding and knowledge of the dynamic analysis of structures. Solved exercises are also proposed to readers at the end of each chapter, and a number of selected problems are provided to allow them to practice the concepts and assess their assimilation. In order to simplify the presentation, most examples and solved exercises are presented in a nondimensional manner.

Finally, the authors do not claim to cover within the following text the field of vibration theory and dynamic analysis in an exhaustive way. Neither have they made explicit reference to all the bibliographic work they have consulted throughout their writing. Therefore the following list of references is suggested for further details on the various aspects of structural dynamics.

Suggested bibliography

Reference works on linear and nonlinear vibration theory (phenomenological aspects and analytical methods):

Biezeno CB and Grammel R 1939

Technische Dynamik

. Springer Berlin.

Crede CE and Harris CM 1977

Shock and Vibration Handbook

(2nd edition). McGraw-Hill, New York.

Del Pedro M and Pahud P 1997

Mécanique vibratoire: systèmes discrets linéaires

. Presses Polytechniques Romandes, Lausanne.

Den Hartog J 1947

Mechanical Vibrations

. McGraw-Hill, New York.

Genta G 2009

Vibration Dynamics and Control

. Springer.

Géradin M 1990

Dynamique des constructions mécaniques

. Course lecture notes, University of Liège.

Hagedorn P 1981

Non-linear Oscillations

. Clarendon Press, Oxford.

Hussey M 1983

Fundamentals of Mechanical Vibrations

. Macmillan.

Lalanne M, Berthier P and Der Hagopian J 1980

Mécanique des vibrations linéaires

. Masson, Paris.

Lord Rayleigh BJWS 1894

Theory of Sound (2 volumes)

2nd edn. Macmillan and Co., London and New York (first edition in 1877).

Magnus K 1961

Schwingungen; eine Einfuhrung in die theoretische Behandlung von Schwingungsproblemen

. Teubner, Stuttgart.

Mazet R 1966

Mécanique vibratoire

. Dunod, Paris.

Meirovitch L 1967

Analytical Methods in Vibrations

. The Macmillan Company, New York.

Meirovitch L 1975

Elements of vibration analysis

. McGraw-Hill.

Müller PC and Schiehlen WO 1985

Linear Vibrations: A Theoretical Treatment of Multi-Degree-of-Freedom Vibrating Systems

. Martinus Nijhoff Publishers, Dordrecht.

Nayfeh AH and Mook DT 1979

Nonlinear Oscillations

. John Wiley & Sons, Inc., New York.

Rao S 1986

Mechanical Vibrations

. Addison-Wesley, Reading, MA.

Rocard Y 1960

Dynamique générale des vibrations

. Masson, Paris.

Roseau M 1984

Vibrations des systèmes mécaniques: méthodes analytiques et applications

. Masson, Paris.

Timoshenko S 1937

Vibration Problems in Engineering

2nd. edn. D. Van Norstrand.

Tong KN 1960

Theory of Mechanical Vibration

. John Wiley & Sons, Inc., New York.

Reference works on random vibration:

Crandall SH and Mark WD 1963

Random Vibration in Mechanical Systems

. Academic Press, New York.

Preumont A 1994

Random Vibrations and Spectral Analysis

. Kluwer Academic.

Reference works on structural dynamics:

Argyris J and Mlejnek H 1991

Dynamics of Structures

. Elsevier, Amsterdam.

Clough RW and Penzien J 1975

Dynamics of Structures

. McGraw-Hill, New York.

Craig R and Kurdila A 2006

Fundamentals of Structural Dynamics

. John Wiley & Sons, Inc., New York.

Fraeijs de Veubeke B, Géradin M and Huck A 1972

Structural Dynamics

. number 126 in

CISM Lecture Notes (Udine, Italy)

. Springer.

Hurty WC and Rubinstein MF n.d.

Dynamics of Structures

. Prentice-Hall New Jersey.

Meirovitch L 1980

Computational Methods in Structural Dynamics

. Sijthoff & Noordhoff.

Preumont A 2013

Twelve Lectures on Structural Dynamics

. Springer.

Reference works dedicated to the finite element method:

Bathe K 1996

Finite Element Procedures in Engineering Analysis

. Prentice Hall, Englewood Cliffs NJ.

Batoz JL and Dhatt G 1990

Modélisation des structures par éléments finis

vol. 1, 2 and 3. Presses Université Laval.

Craveur JC 1996

Modélisation des structures, calcul par éléments finis

. Masson, Paris.

Dhatt G and Touzot G 1984

Une présentation de la méthode des éléments finis

. Collection de l'Université de Compiègne, edited by Maloine.

Hughes T 1987

The Finite Element Method—Linear Static and Dynamic Finite Element Analysis

. Prentice Hall Inc., New Jersey.

Imbert J n.d.

Analyse des structures par éléments finis

. Cepadues Editions, Toulouse.

Kardestuncer H and Norrie DH 1987

Finite Element Handbook

. McGraw-Hill, Inc.

Zienkiewicz O and Taylor R 1989

The Finite Element Method

4th edn. McGraw-Hill. 2 volumes.

Reference works on aeroelasticity:

Bisplinghoff RL and Ashley H 1975

Principles of Aeroelasticity

. Dover Publications, New York.

Bisplinghoff RL, Ashley H and Halfman R 1955

Aeroelasticity

. Addison-Wesley, Cambridge, Mass.

Dowell E, Clark R, Cox D, Curtiss H, Edwards J, Hall K, Peters D, Scanlan R, Simiu E and Sisto F 2004

A Modern Course in Aeroelasticity (Fourth Revised and Enlarged Edition)

. Kluwer Academic Publishers.

Försching HW 1974

Grundlagen der Aeroelastik

. Springer-Verlag, Berlin.

Fung Y 1955

An Introduction to the Theory of Aeroelasticity

. John Wiley & Sons, Ltd, Chichester.

Reference works on fluid-structure interaction and acoustics:

Morand-Fahy FJ and Gardonio P 2007

Sound and structural vibration:radiation, transmission and response

. Academic press.

Morand HJP and Ohayon R 1992

Interactions fluides-structures

. Masson, Paris.

Ohayon R and Soize C 1997

Structural Acoustics and Vibration: Mechanical Models, Variational Formulations and Discretization

. Elsevier.

Reference works on classical mechanics:

Goldstein H 1986

Classical Mechanics

. Addison-Wesley, Reading, MA.

Komzsik L 2014

Applied Calculus of Variations for Engineers

. 2nd edn. CRC Press.

Lanczos C 1949

The Variational Principles of Mechanics

Mathematical Expositions, No. 4. University of Toronto Press, Toronto, Canada.

Meirovitch L 1970

Methods of Analytical Dynamics

. McGraw Hill, New York.

Whittaker ET 1952

Analytical Dynamics of Particles and Rigid Bodies

. Cambridge University Press, New York.

Reference works on solid mechanics:

Fraeijs de Veubeke B 1979 A Course in Elasticity vol. 29 of

Applied Mathematical Sciences

Springer.

Fung Y 1965

Foundations of Solid Mechanics

. Prentice Hall, New Jersey.

Reference works on dynamics of mechanical systems:

Bauchau OA 2011

Flexible Multibody Dynamics

. vol. 176. Springer Science.

Géradin M and Cardona A 2001

Flexible Mutibody Dynamics: The Finite Element Method Approach

. John Wiley & Sons, Ltd, Chichester.

Pfeiffer F 2005

Mechanical System Dynamics

vol. 40. Springer.

Shabana AA 2005

Dynamics of Multibody Systems

. Cambridge University Press.

Reference works on experimental methods in vibration:

Brandt A 2011

Noise and Vibration Analysis: Signal Analysis and Experimental Procedures

. John Wiley & Sons, Ltd, Chichester.

Brincker R 2013

Introduction to Operational Modal Analysis

. John Wiley & Sons, Ltd, Chichester.

Ewins DJ 2000

Modal Testing: Theory, Practice and Application

. Research Studies Press, Baldock.

Heylen W, Lammens S and Sas P 1997

Modal Analysis Theory and Testing

. Katholieke Universiteit Leuven, Department Werktuigkunde, Heverlee.

McConnell KG and Varoto PS 2008

Vibration Testing: Theory and Practice

second edn. John Wiley & Sons, Ltd, Chichester.

Silva JM and Maia NM 1999

Modal analysis and testing NATO Science Series E

vol. 363 Springer.

Zaveri K 1984

Modal Analysis of Large Structures—Multiple Exciter Systems

. Brüel & Kjær, BT 0001-11.

Reference works on vibration control:

Preumont A 2006

Mechatronics: Dynamics of Electromechanical and Piezoelectric Systems

vol. 136. Springer.

Preumont A 2011

Vibration Control of Active Structures: An Introduction

vol. 179. Springer.

Reference works on rotor dynamics:

Friswell MI, Penny JE, Garvey SD and Lees AWi 2010

Dynamics of Rotating Machines

. Cambridge University Press.

Genta G 2005

Dynamics of Rotating Systems

. Springer, New York.

Lalanne M, Ferraris G and Der Hagopian J 1998

Rotordynamics Prediction in Engineering

(2nd edition). John Wiley & Sons, Inc., New York.

Reference works on numerical methods for linear and eigenvalue solutions:

Golub GH and Van Loan CF 1989

Matrix Computations

. John Hopkins University Press.

Householder AS 1964

The Theory of Matrices in Numerical Analysis

. Blaisdell.

Komzsik L 2003

The Lanczos Method: Evolution and Application

. SIAM.

Wilkinson J 1965

The Algebraic Eigenvalue Problem

. Clarendon Press, Oxford.

Reference works on numerical methods for time integration:

Belytschko T and Hughes T 1983

Computational Methods for Transient Analysis

. North-Holland.

Gear C 1971

Numerical Initial Value Problems in Ordinary Differential Equations

. Prentice Hall, Englewood Cliffs, NJ.

List of main symbols and definitions

The list below provides the definitions of variables and quantities that are common to all book chapters. A separate list is provided at the beginning of each chapter with definitions that remain local to the chapter.2

In the text, we will use bold characters to denote matrices. Lower case bold symbols will represent uni-column matrices whereas upper case ones denote multi-column matrices. For instance,

and

Nonbold symbols represent scalars. A subscript like typically denotes the coefficient of a matrix .

Subscripts in parentheses (e.g. ) indicate that the quantity is associated to mode .

-dimensional space.

subspace of first

eigenmodes.

dof

degree-of-freedom.

rigid mobility matrix.

damping matrix.

strain differential operator.

flexibility matrix.

gyroscopic matrix.

admittance (dynamic flexibility) matrix of undamped system.

identity matrix.

stiffness matrix.

geometric stiffness matrix.

modified stiffness matrix (rotating system).

mass matrix.

modal reduction matrix.

matrix of rigid body modes.

matrix of elastic eigenmodes.

imposed load per unit of volume.

impedance (dynamic stiffness) matrix of undamped system.

-th unit vector.

vector of external loads.

vector of generalized coordinates.

generalized coordinates at

.

vector of generalized velocities.

generalized velocities at

.

vector of generalized accelerations.

vector of surface tractions.

vector of imposed surface tractions.

-th rigid body mode.

eigenvector of conservative system associated to

.

dissipation function.

bar extensional stiffness.

beam bending stiffness.

total energy.

Fourier transform.

imaginary part of a complex number.

beam shear stiffness.

Laplace transform.

generalized force conjugated to

.

real part of a complex number.

external surface of continuous body.

part of external surface with imposed surface tractions.

part of external surface with imposed displacements.

kinetic energy.

transport kinetic energy.

relative kinetic energy.

complementary kinetic energy.

volume of continuous body.

potential energy.

volume of reference configuration.

external potential energy.

complementary external potential energy.

geometric part of internal potential energy.

internal potential energy.

complementary internal potential energy.

modified potential.

gravity constant.

step response function.

impulse response function.

imaginary number.

length.

number of generalized coordinates.

number of degrees of freedom.

generalized coordinate.

time.

diagonal matrix of eigenvalues

.

vector of Lagrange multipliers.

strain matrix, collecting the strain components

.

vector of normal coordinates of elastic modes

.

diagonal matrix of generalized masses

.

stress matrix, collecting the strain components

.

vector of normal coordinates of rigid body modes

.

Laplacian operator.

rotation velocity.

variation symbol.

Kronecker symbol.

Dirac function.

strain tensor.

linear part of strain tensor.

quadratic part of strain tensor.

normal coordinate of elastic mode

.

generalized stiffness of mode

.

generalized mass of mode

.

frequency (in Hz).

circular frequency (in rad/s).

th eigenvalue of second order system.

circular frequency of mode

(in rad/s).

load participation factor of mode

.

volumic mass.

volumic mass in reference configuration.

stress tensor.

tensor of initial stresses.

 

 

1

 From 1986, SAMCEF™ has been industrialized, maintained and distributed by SAMTECH SA, a spin-off company of the University of Liège.

2

 Multiple use of same symbol has been avoided as much as possible, but may still occur locally.

Chapter 1Analytical Dynamics of Discrete Systems

The variational approach to mechanics is based on the concepts of energy and work and therefore provides a better understanding of mechanical phenomena. In some sense one can say that variational principles consider the system in a global sense, disregarding the specifities of the forces associated to kinematic constraints imposed on the system. It provides at the same time a very powerful tool for two main reasons:

It considerably simplifies the analytical formulation of the motion equations for a complex mechanical system.

It gives rise to approximate numerical methods for the solution of both discrete and continuous systems in the most natural manner, as will be later explained in Chapters 5 and 6.

The objective of this chapter is to recall to the reader, how the fundamental Newton's equations for dynamics can be effectively applied to general systems on which kinematic constraints are imposed. First we recall the concept of virtual displacements and the principle of virtual work for a single mass point (Section 1.1), then for a system of particles (Section 1.2), explaining how it leads to a global dynamic description of a system where unknown reaction forces associated to kinematic constraints do not appear. The intimately related concepts of kinematic constraints and generalized coordinates (or degrees of freedom) are also discussed in those sections. Note that in this book we will not discuss the dynamics of rigid bodies. Although a rigid body can be seen as a collection of constrained point masses and therefore a special case of the systems treated here, analyzing the dynamics of a rigid body and building models of multiple rigid components is a topic in itself that will not be handled here since the main scope of the book is vibrational behaviour of flexible systems.1

In Section 1.3 the dynamics of systems is described in an even more abstract way, using the energy concepts to show that the virtual work principle can be written as a variational principle, namely Hamilton's principle. It is then shown that the equations of motion can be derived from the energy description of the system: the Lagrange equations. Those equations are outlined for the general case of nonconservative systems in Section 1.4.2

Section 1.5 deals with the generalization of the Lagrange equations to systems undergoing impulsive loading (i.e. shocks, impact). Finally, Section 1.6 provides an introduction to the dynamics of constrained systems. It is shown that the method of Lagrange multipliers provides an efficient way to extend Lagrange's equations to systems described by coordinates for which constraints need to be explicitly accounted for.

Definitions

The list below complements the general definitions given in the book introduction, but remains local to Chapter 1.

gyroscopic forces.

number of particles.

generalized impulse.

number of constraints.

displacement component of

particle in terms of generalized coordinates.

dislocation potential.

,

component of force on (

) particle.

,

mass of (

) particle.

,

displacement component of (

) particle.

reference configuration of

particle.

Lagrange multiplier.

instantaneous configuration of

particle.

1.1 Principle of virtual work for a particle

1.1.1 Nonconstrained particle

Let us consider a particle of mass , submitted to a force field of components . The dynamic equilibrium of the particle can be expressed in d'Alembert's form:

1.1

where represents the displacement of the particle.

Let us next imagine that the particle follows during the time interval a motion trajectory distinct from the real one . This allows us to define the virtual displacement of the particle by the relationship (Figure 1.1):

1.2

Figure 1.1 Virtual displacement of a particle.

By its very definition, the virtual displacement is arbitrary for . However, let us suppose that the varied trajectory and the real one both pass through the same points at the ends of the time interval. The end conditions then take the form:

1.3

An immediate consequence of definition (1.2) is that the variation operator commutes with the time-derivative operator since

1.4

Let us next multiply the dynamic equilibrium equations (1.1) by the associated virtual displacement and sum over the components. The virtual work expression results:

1.5

which shows that

The virtual work produced by the forces acting on the particle during a virtual displacementis equal to zero.

1.1.2 Constrained particle

Equation (1.5) represents the scalar product between the forces acting on the particle and the virtual displacement . It thus represents the projection of the equilibrium along the direction. If (1.5) is satisfied for all variations , then the trajectory satisfies the dynamic equilibrium in all directions.

If no kinematical constraint is imposed onto the particle, namely if no restriction is imposed on its displacement, the trajectory of the material point is determined by the equilibrium in all directions. But when kinematic constraints are specified for the particle, there exist reaction forces in addition to the applied forces. These reaction forces are inherent to the constraining mechanism and ensure that the imposed kinematical constraints are satisfied. Those reaction forces are not known in advance since they depend on the motion itself.

Figure 1.2 describes a particle constrained to move along a curve and a spherical pendulum where a particle is constrained to have a constant distance with respect to a fixed point. On one hand, the presence of reaction forces acting in the direction of the constraint generally renders the equilibrium description more complex since those unknown forces must be determined along the entire trajectory such that kinematical constraints are satisfied. On the other hand, solving the equilibrium equations in the direction constrained by the kinematical conditions is not useful since, in that direction, the trajectory is prescribed by the constraint and thus known.

Figure 1.2 Kinematically admissible virtual displacements.

In the system described in Figure 1.2.a only the motion along the direction tangent to the curve needs to be determined. In doing so, the reaction forces, which act in the direction normal to the curve, do not participate to the motion and thus need not be determined: the position of the particle in the direction normal to the curve is obviously imposed by the constraint and does not require solving the equilibrium equation in that direction. In the same way, if the equilibrium of the particle of the spherical pendulum is expressed in the plane tangent to the sphere (Figure 1.2.b), only the forces actually applied participate in the determination of the trajectory.

Let us therefore decide that, in the presence of kinematical constraints, we consider only virtual displacements compatible with the constraints or, in other words, kinematically admissible. Equation (1.5) then describes the projection of the dynamic equilibrium in the space compatible with the constraints, namely in directions orthogonal to unknown reaction forces. The form (1.5) thus involves only effectively applied forces and stipulates that

The virtual work produced by the effective forces acting on the particle during a virtual displacementcompatible with the constraints is equal to zero.