Fatigue Crack Growth Under Spectrum Loads
Author | : Ralph Ivan Stephens |
Publisher | : ASTM International |
Total Pages | : 345 |
Release | : 1976 |
Genre | : Alloys |
ISBN | : |
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Author | : Ralph Ivan Stephens |
Publisher | : ASTM International |
Total Pages | : 345 |
Release | : 1976 |
Genre | : Alloys |
ISBN | : |
Author | : J. Petit |
Publisher | : Springer |
Total Pages | : 422 |
Release | : 1988-12-31 |
Genre | : Technology & Engineering |
ISBN | : |
Author | : J. Schijve |
Publisher | : Springer Science & Business Media |
Total Pages | : 627 |
Release | : 2008-12-16 |
Genre | : Science |
ISBN | : 1402068085 |
Fatigue of structures and materials covers a wide scope of different topics. The purpose of the present book is to explain these topics, to indicate how they can be analyzed, and how this can contribute to the designing of fatigue resistant structures and to prevent structural fatigue problems in service. Chapter 1 gives a general survey of the topic with brief comments on the signi?cance of the aspects involved. This serves as a kind of a program for the following chapters. The central issues in this book are predictions of fatigue properties and designing against fatigue. These objectives cannot be realized without a physical and mechanical understanding of all relevant conditions. In Chapter 2 the book starts with basic concepts of what happens in the material of a structure under cyclic loads. It illustrates the large number of variables which can affect fatigue properties and it provides the essential background knowledge for subsequent chapters. Different subjects are presented in the following main parts: • Basic chapters on fatigue properties and predictions (Chapters 2–8) • Load spectra and fatigue under variable-amplitude loading (Chapters 9–11) • Fatigue tests and scatter (Chapters 12 and 13) • Special fatigue conditions (Chapters 14–17) • Fatigue of joints and structures (Chapters 18–20) • Fiber-metal laminates (Chapter 21) Each chapter presents a discussion of a speci?c subject.
Author | : J. B. Chang |
Publisher | : ASTM International |
Total Pages | : 150 |
Release | : 1981 |
Genre | : Technology & Engineering |
ISBN | : 9780803107151 |
Author | : Hans Albert Richard |
Publisher | : Springer |
Total Pages | : 305 |
Release | : 2016-06-13 |
Genre | : Technology & Engineering |
ISBN | : 3319325345 |
This book offers a concise introduction to fatigue crack growth, based on practical examples. It discusses the essential concepts of fracture mechanics, fatigue crack growth under constant and variable amplitude loading and the determination of the fracture-mechanical material parameters. The book also introduces the analytical and numerical simulation of fatigue crack growth as well as crack initiation. It concludes with a detailed description of several practical case studies and some exercises. The target group includes graduate students, researchers at universities and practicing engineers.
Author | : Wolf Elber |
Publisher | : ASTM International |
Total Pages | : 671 |
Release | : 1988 |
Genre | : Fracture mechanics |
ISBN | : 0803109962 |
Author | : Margery A. Dean |
Publisher | : |
Total Pages | : 38 |
Release | : 1983 |
Genre | : Airframes |
ISBN | : |
The life prediction of aerospace structures subjected to service loading conditions can be complex and expensive. Fortunately, many flight-by- flight loadings can be analyzed as constant amplitude loading if the variability in crack growth rate is low. A test program was designed such that the stress intensity factor (Kmax) was held constant by uniformly reducing the load as the fatigue crack grew. With a constant Kmax, the crack growth rate remains constant throughout the life of the test. The baseline fatigue crack growth rate variability was established for the 7075-T6 center-cracked panels under a flight-by-flight load history. The effect of introducing overloads to the baseline flight history on the crack growth rate variability was reported. The results indicate that the delay region for the applied 114% overloads was predicted by Irwin's plastic zone model and was equal to 0.0382 inches which was equal to 225 flights. The delay behavior was consistent for the several overload conditions that were studied. When the occurrence of overload increased, the fatigue crack growth decreased. The standard error of estimate remained relatively constant, suggesting that a block approach to life prediction is feasible for flight-by-flight load history.
Author | : Jeffrey T. Fong |
Publisher | : ASTM International |
Total Pages | : 389 |
Release | : 1988 |
Genre | : Materials |
ISBN | : 0803109253 |
Author | : M. A. Meyers |
Publisher | : Elsevier |
Total Pages | : 317 |
Release | : 2003-12-05 |
Genre | : Technology & Engineering |
ISBN | : 0080537235 |
The importance of the nanoscale effects has been recognized in materials research for over fifty years, but it is only recently that advanced characterization and fabrication methods are enabling scientists to build structures atom-by-atom or molecule-by molecule. The understanding and control of the nanostructure has been, to a large extent, made possible by new atomistic analysis and characterization methods pioneered by transmission electron microscopy. Nano and Microstructural Design of Advanced Materials focuses on the effective use of such advanced analysis and characterization techniques in the design of materials. - Teaches effective use of advanced analysis and characterization methods at an atomistic level - Contains many supporting examples of materials in which such design concepts have been successfully applied