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Jaap Wijker
Mechanical Vibrations in Spacecraft Design
EngineeringONLINE LIBRARY
http://www.springer.de/engine/
Springer-Verlag Berlin Heidelberg GmbH
Jaap Wijker
Mechanical Vibrationsin Spacecraft Design
With120Figuresand 29Tables
• Springer
Jaap Wijker
DutchSpaceBYP.O. Box320702303 DBLeidenThe Netherlands
E-mail: [email protected]
Cataloging-in-Publication Data applied for.Bibliographic information published by Die Deutsche Bibliothek. Die Deutsche Bibliothek liststhis publication in the Deutsche Nationalbibliografie; detailed bibliographic data is available inthe Internet at <http ://dnb.ddb.de>.
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© Springer-Verlag Berlin Heidelberg 2004Originally published by Springer-VerlagBerlin Heidelberg New York in 2004
Softcover reprint ofthe hardcover 1st edition 2004
The use of general descriptive names, registered names, trademarks, etc. in this publication doesnot imply, even in the absence of a specific statement, that such names are exempt from therelevant protective laws and regulations and therefore free for general use.
Typesetting: Dataconversion by authorCover-design: medio, BerlinPrinted on acid-free paper 62 13020 hu - 5 4 3 2 I 0
ISBN 978-3-642-07354-0 ISBN 978-3-662-08587-5 (eBook)DOI 10.1007/978-3-662-08587-5
Dedicated to my mother
Maartje Wijker-Gravemaker
and to the memory of my father
Job Wijker
Preface
This book about mechanical vibrations focuses on spacecraft structuresdesign and reflects my experiences gained at Dutch Space B.Y., formerlyFokker Space B.Y., Fokker Space & Systems B.Y. and the Space Divisionof Fokker Aircraft B.Y., over a period of about 30 years.
Many books about mechanical vibrations have been published, however,in spacecraft structures design, many vibration topics are applied but can beread in different books. I have collected in this book most of the topicsabout mechanical vibrations techniques usually applied in spacecraftstructures design .
I work as a part-time associate professor at the Chair AerospaceStructures & Computational Mechanics, Faculty of Aerospace Engineering,Delft University of Technology, and lecture "Spacecraft Structures" in theMaster's program. The scientific environment at the university, incombination with my work in the aerospace industry, has amplified thewish to write a book about mechanical vibrations with focus on spacecraftstructures design. To bring together most of the techniques of modal anddynamic response analysis is my greatest motivation to write this book.
I would like to express my admiration for the patient attitude of my wifeWil during the time I was preparing this book.
I would also like to acknowledge my colleagues at Dutch Space and theDelft University of Technology in general, but in particular I would like tothank my collegue John Tyrrell at Dutch Space, for all the discussions wehad about vibration problems within the framework of spacecraft structuresprojects, and Gillian Saunders-Smits at the Delft University of Technologyfor reading the English text. Also, I would like to thank Bas Franssen forreading the sections on the Mode Acceleration Technique and LoadTransformation Matrices.
Jaap WijkerVelserbroek 2003
Table ofContents
Introduct ion 1
1.1 Why Another Book about Mechanical Vibrations ? 1
1.2 A Short Overview of Theory 5
1.2.1 Single Degree of Freedom (sdot) Systems 5
1.2.2 Damped Vibrations 6
1.2.3 Multi-Degrees of Freedom (mdot) Dynamic Systems 7
1.2.4 Modal Analysis 8
1.2.5 Modal Effective Mass 9
1.2.6 Response Analysis 9
1.2.7 Transient Response Analysis 10
1.2.8 Random Vibrations 11
1.2.9 Shock-Response Spectrum 12
1.2.10 Acoustic Loads, Structural Responses 13
1.2.11 Statistical Energy Analysis 13
1.2.12 Inertia-Relief 14
1.2.13 Mode Acceleration Method 141.2.14 Residual Vectors 14
1.2.15 Dynamic Model Reduction 151.2.16 Component Model Synthesis 16
1.2.17 Load Transformation Matrice s 17
1.3 Problems 17
1.3.1 Problem 1 17
2 Single Degree of Freedom System 19
2.1 Introduction 19
2.2 Undamped Sdof System 20
2.2.1 Solution of an Sdof System with Initial Conditions 23
x Table of Contents
2.2.2 Solution of an Sdof System with Applied Forces 24
2.3 Damped Vibration and the Damping Ratio 27
2.3.1 Solut ion of the Sdof System in the Time Domain 29
2.3.2 Solution of the Damped Sdof System with Applied Forces 32
2.3.3 Solut ion in the Frequency Domain 34
2.3.4 State Space Representation of the Sdof System .42
2.4 Problems 45
2.4.1 Problem I 45
2.4.2 Problem 2 46
2.4.3 Problem 3 46
2.4.4 Problem 4 46
2.4.5 Problem 5 47
2.4.6 Problem 6 47
2.4.7 Problem 7 47
2.4.8 Problem 8 48
3 Damping Models 49
3.1 Introduction 49
3.2 Damped Vibration 50
3.2.1 Linear Damping 50
3.2.2 Viscous Damping 51
3.2.3 Structural Damping 51
3.2.4 Loss Factor 52
3.3 Amplification Factor 53
3.3.1 Modal Viscous Damping 53
3.3.2 Modal Structural Damping 54
3.3.3 Discussion of Modal Damping 55
3.4 Method of Determining Damping from Measurements 56
3.4.1 The Half-Power Point Method 56
3.5 Problems 57
3.5.1 Problem 1 57
3.5.2 Problem 2 58
4 Multi-Degrees of Freedom Linear Dynamic Systems 59
4.1 Introduction 59
4.2 Derivation of the Equations of Motion 60
4.2.1 Undamped Equations of Motion with Newton's Law 60
4.2.2 Undamped Equations of Motion using Energies 62
4.2.3 Undamped Equations of Motion using Lagrange's Equations 63
Table of Contents
4.2.4 Damped Equations of Motion using Lagrange's Equations 65
4.3 Finite Element Method 70
4.4 Problems 70
4.4.1 Problem I 70
4.4.2 Problem 2 71
5 Modal Analysis 73
5.1 Introduction 73
5.2 Undamped Linear Dynamic Systems 735.2.1 Natural Frequencies and Mode Shapes 74
5.2.2 Orthogonality Relations of Modes 77
5.2.3 Rigid-Body Modes 80
5.2.4 Left Eigenvectors 84
5.3 Damped Linear Dynamic Systems 86
5.3.1 The State Vector 86
5.3.2 Eigenvalue Problem 88
5.3.3 Eigenvectors 89
5.4 Problems 92
5.4.1 Problem I 92
5.4.2 Problem 2 93
6 Natural Frequencies , an Approximation 95
6.1 Introduction 95
6.2 Static Displacement Method 95
6.3 Rayleigh's Quotient 98
6.4 Dunkerley 's Method 101
6.5 Problems 107
6.5.1 Problem I 107
6.5.2 Problem 2 107
6.5.3 Problem 3 107
6.5.4 Problem 4 108
6.5.5 Problem 5 109
7 Modal Effective Mass III
7.1 Introduction III
7.2 Enforced Acceleration III
7.3 Modal Effective Masses of an Mdof System 114
7.4 Problems 122
xi
xli Tableof Contents
7.4.1 Problem I 122
7.4.2 Problem 2 123
8 Response Analysis 125
8.1 Introduction 125
8.2 Forces and Enforced Acceleration 125
8.2.1 Relative Motions 126
8.2.2 Absolute Motions 138
8.2.3 Large-Mass Approach 140
8.3 Problems 146
8.3.1 Problem 1 146
8.3.2 Problem 2 147
8.3.3 Problem 3 148
9 Transient-Response Analysis 149
9.1 Introduction 149
9.2 Numerical Time Integration 151
9.2.1 Discrete Solution Convolution Integral... 151
9.2.2 Explicit Time-Integration Method 153
9.2.3 Implicit Time-Integration Methods 153
9.2.4 Stability 153
9.3 Explicit Time-Integration 154
9.3.1 Central Difference Method 154
9.3.2 Runge-Kutta Formulae for First-Order Differential Equations 156
9.3.3 Runge-Kutta-Nystrom Method for S-O Differential Equations 159
9.4 Implicit Time Integration 159
9.4.1 HouboItMethod 160
9.4.2 Wilson-theta Method 162
9.4.3 Newmark-beta Method 164
9.4.4 The Hughes, Hilber and Taylor (HHT) alpha-Method 166
9.4.5 The Wood, Bossak and Zienkiewicz (WBZ) alpha-Method 167
9.4.6 The Generalised-alpha Algorithm 168
9.5 Piecewise Linear Method 169
9.6 Problems 170
9.6.1 Problem 1 170
9.6.2 Problem 2 172
9.6.3 Problem 3 172
Table of Contents xiii
10 Shock-Response Spectrum 173
10.1 Introduction 173
10.2 Enforced Acceleration174
10.3 Numerical Calculation of the SRS, the Piecewise Exact Method 176
10.4 Response Analysis in Combination with Shock-Response Spectra 181
10.5 Matching Shock Spectra with Synthesised Time Histories 190
10.6 Problems 199
10.6.1 Problem 1 199
10.6.2 Problem2 200
11 Random Vibration of Linear Dynamic Systems 201
11.1 Introduction 201
11.2 Random Process 201
11 .3 Power-Spectral Density 207
11.4 Deterministic Linear Dynamic System 212
11.4.1 Force-Loaded Sdof System 214
11.4.2 Enforced Acceleration 216
11.4.3 Multi-Inputs and SingleOutput(MISO) 223
11.5 Deterministic Mdof Linear Dynamic System 224
11.5.1 RandomForces 224
11.5.2 RandomBase Excitation 227
11.5.3 RandomStresses and Forces 229
11.6 Analysis of Narrow-Band Processes 234
11 .6.1 Crossings 23411.6.2 Fatigue Damagedue to Random Excitation 238
11.7 Some Practical Aspects 241
11.8 Problems 24411 .8.1 Problem 1 24411 .8.2 Problem 2 24411 .8.3 Problem 3 245
11 .8.4 Problem 4 245
11 .8.5 Problem 5 246
12 Low-Frequency Acoustic Loads, Structural Responses 247
12.1 Introduction 247
12.2 Acoustic Loads 247
12.3 Equations of Motion 249
12.4 Problems 260
xiv Table of Contents
12.4.1 Problem 1 26012.4.2 Problem 2 261
13 Statistical Energy Analysis 263
13.1 Introduction 263
13.2 Some Basics about Averaged Quantities 264
13.3 Two Coupled Oscillators 270
13.4 Multimode Subsystems 277
13.5 SEA Parameters 28313.5.1 Subsystem Modal Densities 28313.5.2 Source Power Input 28813.5.3 Subsystem Energies 28913.5.4 Damping Loss Factor 29413.5.5 Coupling Loss Factor 295
13.6 Stresses and Strains 298
13.7 Problems 29913.7.1 Problem 1 29913.7.2 Problem 2 29913.7.3 Problem 3 30013.7.4 Problem 4 30013.7.5 Problem 5 30013.7.6 Problem 6 30 1
13.7.7 Problem 7 30113.7.8 Problem 8 302
14 Free-free Dynamic Systems, Inertia Relief 303
14.1 Introduction 303
14.2 Relative Motion 303
14.3 Relative Forces 304
14.4 Flexibility Matrix 307
14.5 Problems 31014.5.1 Problem 1 310
15 Mode Acceleration Method 313
15.1 Introduction 313
15.2 Decomposition of Flexibility and Mass Matrix 31315.2.1 Decomposition of the Flexibility Matrix 31315.2.2 Decomposition of the Mass Matrix 315
Table of Contents xv
15.2.3 ConvergenceProperties of ReconstructedMatrices 316
15.3 Mode Acceleration Method 318
15.4 Problems 325
15.4.1 Problem 1 32515.4.2 Problem2 325
15.4.3 Problem3 326
15.4.4 Problem 4 326
15.4.5 Problem5 327
16 Residual Vectors 331
16.1 Introduction 331
16.2 Residual Vectors 33116.2.1 Dickens Method 331
16.2.2 Rose Method 334
16.3 Problems 34016.3.1 Problem 1 340
17 Dynamic Model Reduction Methods 343
17.1 Introduction 343
17.2 Static Condensation Method 344
17.2.1 Improved Calculation of Eliminated Dofs 350
17.3 Dynamic Reduction 351
17.4 Improved Reduced System (IRS) 352
17.5 Craig-Bampton Reduced Models 355
17.6 Generalised Dynamic Reduction 358
17.7 System Equivalent Reduction Expansion Process (SEREP) 362
17.8 Ritz Vectors 365
17.9 Conclusion 367
18 Component Mode Synthesis 369
18.1 Introduction 369
18.2 The Unified CMS Method 370
18.2.1 Modal Truncation 371
18.2.2 General Synthesis of TwoComponents 372
18.2.3 General Example 374
18.3 Special CMS Methods 379
18.3.1 Craig-Bampton Fixed-InterfaceMethod 379
18.3.2 Free-Interface Method 384
xvi Table of Contents
18.3.3 General-Purpose eMS Method 391
18.4 Problems 39618.4.1 Problem 1 396
18.4.2 Problem 2 397
19 Load Transformation Matrices 399
19.1 Introduction 399
19.2 Reduced Model with Boundary Conditions 400
19.3 Reduced Free-Free Dynamic Model 404
19.4 Continuous Dynamic Systems .409
19.5 Problems 41319.5.1 Problem I 41319.5.2 Problem 2 414
19.5.3 Problem 3 41519.5.4 Problem 4 415
References 417
Author Index 427
Subject Index 431