3 edition of Fatigue life and crack growth prediction methodology found in the catalog.
Fatigue life and crack growth prediction methodology
by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor in Hampton, Va, [Springfield, Va
Written in English
|Statement||J.C. Newman, Jr., E.P. Phillips, and R.A. Everett, Jr.|
|Series||NASA technical memorandum -- 109044., NASA technical memorandum -- 109044.|
|Contributions||Phillips, E. P., Everett, R. A., Langley Research Center.|
|The Physical Object|
New methods for aircraft movables introduce oblique- and out-of-plane loads on lug joints. With the introduction of these loads on lugs the need arises for a more detailed fatigue life prediction method. Therefore, the thesis research focused on creating a methodology for predicting the fatigue life for lug joints subjected to combined in- and out-of-plane loading in co-operation . Concerning the determination of mechanical fields close to a crack tip, the first part of the book presents most of the traditional methods in order to classify them into two major categories. The first is based on the stress field, such as the Airy function, and the second resolves the problem from functions related to displacement fields.
The advantage of the developed EIFS concept is that an accurate fatigue life prediction can be obtained without complicated micro-mechanics analysis of small crack growth. The developed EIFS methodology is combined with probabilistic crack growth analysis to predict the fatigue life distribution of smooth : Yongming Liu. Fatigue life and crack growth prediction methodology. By Jr. J. C. Newman, Jr. Richard A. Everett and E. P. Phillips. Abstract. This paper reviews the capabilities of a plasticity-induced crack-closure model and life-prediction code to predict fatigue crack growth and fatigue lives of metallic materials. Crack-tip constraint factors, to.
This then leads to design optimization using fatigue life as a design constraint or possibly even as a design objective. Life Prediction Methods. There are three main life prediction methods as already mentioned earlier. These are Total Life, Crack Initiation, and Crack Growth (Propagation). Linkage between Safe‐Life and Crack Growth Approaches for Fatigue Life Prediction. D. Gary Harlow. Search for more papers by this author Robert P. Wei. Search for more papers by this author. Book Editor(s): P.K. Liaw. Search for more papers by this author. R.A. Buchanan. Search for more papers by this author A Model for Fatigue Crack Author: D. Gary Harlow, Robert P. Wei.
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Fatigue Damage, Crack Growth and Life Prediction th Edition by Fernand Ellyin (Author)Format: Paperback. 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.
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. This paper reviews the capabilities of a plasticity-induced crack-closure model and life-prediction code to predict fatigue crack growth and fatigue lives of metallic materials.
Crack-tip constraint factors, to account for three-dimensional effects, were selected to correlate large-crack growth rate data as a function of the effective-stress-intensity. Fatigue lives were calculated using the crack-growth relations and microstructural features like those that initiated cracks for the aluminum alloys and steel for edge-notched specimens.
An equivalent- initial-flaw-size concept was used to calculate fatigue lives in other cases. Results from the tests and analyses agreed Size: 1MB. Prediction methods for fatigue lives and fatigue crack growth are discussed as well as verification by experiments.
Load spectra analysis and statistical aspects are also addressed. The first edition of this book was well received and has been used extensively in various courses taught to staff members and students of universities and other Brand: Springer Netherlands.
In order to accurately predict the total fatigue life, quantitative simulation of the crack growth behavior is needed. When a crack reaches a sufficient length, the crack growth behavior is not sensitive to the microstructure and is described by linear elastic fracture by: 8.
The fatigue life of bogie beam 1 was predicted with four different methods: the S-N-method, the fracture mechanics method, and the modification of the HdM-method with different values on the crack closure stress level. The predictions made with the two first methods were made by ABB Corporate Research and is reported in detail by: 3.
fatigue crack growth rate equation for the remaining life. The two lives are added together to obtain the total fatigue life. All four of these fatigue life models are covered in this course/book File Size: KB. Fatigue life and crack growth prediction methodology Geshelin, V.G., Polunin, V.I.
and Akhant'ev, V.P. Met. Sci. Heat Treat. (Russia) (July ) 36 (), In order to provide high strength to cyclic loads for structural steels; methods of surface hardening by thermochemical treatment are widely applied. This chapter describes a computational methodology for fatigue crack growth analysis and damage prognosis in structures.
This methodology is applicable to a variety structural components and systems with complicated geometry and subjected to Author: Shankar Sankararaman, You Ling, Sankaran Mahadevan. fatigue tests and stress-life (s-n) approach fatigue testing loading test machines specimens standards stress-life apperoach s-n curves mean stress effects on s-n behavior factors influencing s-nbehavior fatigue crack growth testing is covered in section Get this from a library.
Fatigue life and crack growth prediction methodology. [J C Newman; Edward P Phillips; R A Everett; Langley Research Center.]. Fatigue Life Enhancement, XV. Fatigue Life Prediction and Test, XVI. Fatigue Modelling and Simulation, XVII.
Fatigue of Coatings, XVIII. Fracture Processes and Fatigue in Rocks, XIX. Fretting and Contact Fatigue, XX. Growth of Short and Long Cracks, XXI. Laser Shock Peening, XXII. Life Prediction Methodology and Software Development, XXIII. In this paper, a probabilistic methodology is developed for predicting the corrosion fatigue crack growth life of gas turbine engine disks made from a powder-metallurgy Ni-based superalloy (ME3).Cited by: Strain‐life data, from fatigue tests on smooth specimens, are used to propose a convenient fatigue damage model.
Predicted crack growth rates are compared with experimental crack propagation data obtained by authors using fatigue tests on compact tension by: Pang et al. proposed a multi-crack life prediction method combined with fatigue crack closure effect and generated good results by using the threshold stress intensity factor approach in predicting the fatigue life of four-point bending fatigue tests.
The fatigue life prediction based on methods mentioned above takes only edge cracks into : Keji Pang, Huang Yuan. A crack growth-based multiaxial fatigue life prediction model is proposed in this paper, which uses a characteristic plane-based methodology for multiaxial fatigue damage analysis and the Equivalent Initial Flaw Size (EIFS) concept for life : Zizi Lu, Yongming Liu.
Fatigue life and crack growth prediction methodology. By Jr. Everett, E. Phillips and Jr. Newman. Abstract. The capabilities of a plasticity-induced crack-closure model and life-prediction code to predict fatigue crack growth and fatigue lives of metallic materials are reviewed.
Crack-tip constraint factors, to account for three. The damage-tolerant methodology focus on predictions of the fatigue crack growth rate and the remaining fatigue life whereas the safe-life design methodology focuses on estimating the total life.
The crack dimension has been identified as a crucial factor by a number of authors, because short fatigue cracks (having a small length compared to the scale of local plasticity, or to the key microstructural dimension, or simply smaller than mm) in metals grow at faster rate and lower nominal stress compared to large cracks [72, 73]Cited by: Effect of Simulation Methodology on Solder Joint Crack Growth Correlation and Fatigue Life Prediction Robert Darveaux.
Robert Darveaux. South Price Road, Chandler, AZ Search for other works by this author on: This Site. by: This book gathers papers presented at the 36 th conference and 30 th Symposium of the International Committee on Aeronautical Fatigue and Structural integrity. Focusing on the main theme of “Structural Integrity in the Age of Additive Manufacturing”, the chapters cover different aspects concerning research, developments and challenges in this field, offering a timely .