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An Integrated Approach to Creep-Fatigue Life Prediction

An Integrated Approach to Creep-Fatigue Life Prediction
Author: P. Agatonovic
Publisher:
Total Pages: 19
Release: 1988
Genre: Creep
ISBN:

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There has been special interest recently in developing new, reliable analytical design methods for components under higher temperature conditions. However, at present, the use of material properties is still limited to arrays of single characteristics which do not interact with each other. In this work, several creep fatigue experiments on smooth specimens of IN 800 H have been carried out at 830°C. In some tests, these have also been combined with inside hysteresis loops to investigate the different effects on deformation and damage behavior which originate in a creep and fatigue environment. As a result of these tests, it has been found that the material behavior under creep-fatigue conditions can be significantly changed compared to the material behavior under simple load conditions. Therefore there is a need for life analysis methods to be expanded to include possible variations in properties; for greater accuracy, the material properties must be treated as a complex interacting system of parameters. The examination has been extended to a typical component used under high-temperature conditions. The results of the numerical analysis show that the stress-strain history in the critical area of that component is not simply strain controlled, as it is in the typical laboratory creep-fatigue interaction life test containing a tensile or compressive dwell at constant peak strain level. At high temperatures, the conditions in the component are more severe, causing the life to be reduced compared with the typical laboratory test. In this paper, these conditions are successfully simulated with the help of a generalized Neuber law: ? . ?p = constant. Based on this ratio, the engineering method for evaluating component geometry and loading conditions and their effects on material behavior can be established.


Low Cycle Fatigue

Low Cycle Fatigue
Author: Harvey D. Solomon
Publisher: ASTM International
Total Pages: 1289
Release: 1988
Genre: Engineering design
ISBN: 080310944X

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Advances in Fatigue Lifetime Predictive Techniques

Advances in Fatigue Lifetime Predictive Techniques
Author: Michael R. Mitchell
Publisher: ASTM International
Total Pages: 495
Release: 1992
Genre: Fracture mechanics
ISBN: 0803114230

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Twenty-seven papers from fatigue researchers and practitioners review in detail recent progress in the development of methods to predict fatigue performance of materials and structures and to assess the extent to which these new methods are finding their way into practice. The papers, from the ASTM


Evaluation of the Effect of Creep and Mean Stress on Fatigue Life Using a Damage Mechanics Approach

Evaluation of the Effect of Creep and Mean Stress on Fatigue Life Using a Damage Mechanics Approach
Author: NM. Abuelfoutouh
Publisher:
Total Pages: 7
Release: 1992
Genre: Creep-fatigue
ISBN:

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A method for fatigue life prediction of high temperature polycrystalline materials under high rate fully reversed strain cycles (HRSC) was previously derived using a continuum damage mechanics approach. The method is generalized in this paper to predict the fatigue life of balanced cyclic creep rupture (BCCR), tensile cyclic creep rupture (TCCR), and compressive cyclic creep rupture (CCCR). It is assumed that creep deformation mechanisms dominate during the creep portion of the fatigue cycle and that plasticity mechanisms dominate during the plastic portion of the cycle. The interaction of plasticity and creep with the mean applied stress and the effect of this interaction on the fatigue life are investigated. A sample calculation is applied to René 80 at 1255 K (1800°F).


Behavior of Materials Under Conditions of Thermal Stress

Behavior of Materials Under Conditions of Thermal Stress
Author: S. S. Manson
Publisher:
Total Pages: 730
Release: 1953
Genre: Aeronautics
ISBN:

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A review is presented of available information on the behavior of brittle and ductile materials under conditions of thermal stress and thermal shock. For brittle materials, a simple formula relating physical properties to thermal-shock resistance are derived and used to determine the relative significance of two indices currently in use for rating materials. The importance of simulating operating conditions in thermal-shock testing is deduced from the formula and is experimentally illustrated by showing that BeO could be both inferior or superior to Al2O3 in thermal shock depending on the testing conditions. For ductile materials, thermal-shock resistance depends upon the complex interrelation among several metallurgical variables which seriously affect strength and ductility. These variables are briefly discussed and illustrated from literature sources. The importance of simulating operating conditions in tests for rating ductile materials is especially to be emphasized because of the importance of testing conditions in metallurgy. A number of practical methods that have been used to minimize the deleterious effects of thermal stress and thermal shock are outlined.


Fatigue Life Prediction of Composites and Composite Structures

Fatigue Life Prediction of Composites and Composite Structures
Author: Anastasios P. Vassilopoulos
Publisher: Woodhead Publishing
Total Pages: 766
Release: 2019-10-08
Genre: Technology & Engineering
ISBN: 0081025769

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Fatigue Life Prediction of Composites and Composite Structures, Second Edition, is a comprehensive review of fatigue damage and fatigue life modeling and prediction methodologies for composites and their use in practice. In this new edition, existing chapters are fully updated, while new chapters are introduced to cover the most recent developments in the field. The use of composites is growing in structural applications in many industries, including aerospace, marine, wind turbine and civil engineering. However, there are uncertainties about their long-term performance, including performance issues relating to cyclic fatigue loading that hinder the adoption of a commonly accepted credible fatigue design methodology for the life prediction of composite engineering structures. With its distinguished editor and international team of contributors, this book is a standard reference for industry professionals and researchers alike. Examines past, present and future trends associated with the fatigue life prediction of composite materials and structures Assesses novel computational methods for fatigue life modeling and prediction of composite materials under constant amplitude loading Covers a wide range of techniques for predicting fatigue, including their theoretical background and practical applications Addresses new topics and covers contemporary research developments in the field


Mechanical Behaviour of Materials V

Mechanical Behaviour of Materials V
Author: M. G. Yan
Publisher: Elsevier
Total Pages: 1451
Release: 2013-10-22
Genre: Technology & Engineering
ISBN: 1483294129

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Provides a thorough up-to-date account of the latest developments in materials science and engineering research and applications. The contributed papers cover all aspects of this important field, including material aspects of fracture in engineering practice, fatigue criteria and material characterisation, environmental effects on fracture, high temperature deformation and failure and mechanical properties and engineering applications of composite and non-metallic materials. Contains approximately 200 papers from acknowledged experts.


Prediction of the Creep-Fatigue Lifetime of Alloy 617

Prediction of the Creep-Fatigue Lifetime of Alloy 617
Author:
Publisher:
Total Pages:
Release: 2014
Genre:
ISBN:

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A relatively simple method using the nominal constant average stress information and the creep rupture model is developed to predict the creep-fatigue lifetime of Alloy 617, in terms of time to rupture. The nominal constant average stress is computed using the stress relaxation curve. The predicted time to rupture can be converted to number of cycles to failure using the strain range, the strain rate during each cycle, and the hold time information. The predicted creep-fatigue lifetime is validated against the experimental measurements of the creep-fatigue lifetime collected using conventional laboratory creep-fatigue tests. High temperature creep-fatigue tests of Alloy 617 were conducted in air at 950°C with a tensile hold period of up to 1800s in a cycle at total strain ranges of 0.3% and 0.6%. It was observed that the proposed method is conservative in that the predicted lifetime is less than the experimentally determined values. The approach would be relevant to calculate the remaining useful life to a component like a steam generator that might fail by the creep-fatigue mechanism.


Fatigue Damage, Crack Growth and Life Prediction

Fatigue Damage, Crack Growth and Life Prediction
Author: F. Ellyin
Publisher: Springer Science & Business Media
Total Pages: 484
Release: 2012-12-06
Genre: Technology & Engineering
ISBN: 9400915098

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Fatigue failure is a multi-stage process. It begins with the initiation of cracks, and with continued cyclic loading the cracks propagate, finally leading to the rupture of a component or specimen. The demarcation between the above stages is not well-defined. Depending upon the scale of interest, the variation may span three orders of magnitude. For example, to a material scientist an initiated crack may be of the order of a micron, whereas for an engineer it can be of the order of a millimetre. It is not surprising therefore to see that investigation of the fatigue process has followed different paths depending upon the scale of phenomenon under investigation. Interest in the study of fatigue failure increased with the advent of industrial ization. Because of the urgent need to design against fatigue failure, early investiga tors focused on prototype testing and proposed failure criteria similar to design formulae. Thus, a methodology developed whereby the fatigue theories were proposed based on experimental observations, albeit at times with limited scope. This type of phenomenological approach progressed rapidly during the past four decades as closed-loop testing machines became available.