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A material sensitive modified wheeler model for predicting the retardation in fatigue response of AM60B due to an overload
Affiliation:1. Key Laboratory for Power Machinery and Engineering of Ministry of Education, Shanghai Jiao Tong University, Shanghai, China;2. Collaborative Innovation Center for Advanced Ship and Deep-Sea Exploration, Shanghai, China;3. China North Engine Research Institute, Tianjin 300400, China;1. Department of Civil and Materials Engineering, University of Malaga, C/Dr Ortiz Ramos, s/n, 29071 Malaga, Spain;2. MAX IV Laboratory, Lund University, Box 118, SE-221 00 Lund, Sweden;3. NMMU, Gardham Avenue, 6031 Port Elizabeth, South Africa;4. ESRF, 6 rue J Horowitz, 38000 Grenoble, France;5. Rolls-Royce plc, PO Box 31, Derby DE24 8BJ, UK;6. Department of Materials Science and Metallurgy Engineering, University of Jaen, Campus Las Lagunillas, 23071 Jaen, Spain;7. Simuline Ltd., Derbyshire S18 1QD, UK;8. School of Materials, University of Manchester, Grosvenor St., Manchester M13 PL, UK;1. Department of Materials Science and Engineering, Center for Electrochemical Science and Engineering, University of Virginia, 395 McCormick Road, P.O. Box 400745, Charlottesville, VA 22904-4745, USA;2. Department of Materials Science and Engineering, University of California, Davis, 1 Shields Ave, Davis, CA 95616, USA;3. Department of Mechanical and Aerospace Engineering, University of California, Davis, 1 Shields Ave, Davis, CA 95616, USA;1. College of Engineering, Ocean University of China, Qingdao 266100, China;2. Shandong Provincial Key Laboratory of Ocean Engineering, Ocean University of China, Qingdao 266100, China;3. School of Mechanical and Marine Engineering, Beibu Gulf University, Qinzhou, Guangxi 535011, China;1. RMIT University, 124 La Trobe Street, Melbourne, Victoria 3000, Australia;2. Defence Science and Technology, 506 Lorimer Street, Fishermans Bend, Victoria 3207, Australia
Abstract:Application of an overload within an otherwise constant-amplitude loading scenario causes retardation in crack propagation. Several models have been proposed for predicting retardation in crack propagation due to an overload cycle. Among them, the widely used Wheeler model, assumes the “affected zone dimension” to be a function of the current and overloaded plastic zone radii. When one considers the actual shape of the plastic zone, however, one realizes that the affected zone dimension does not agree with that assumed by Wheeler.In this paper, the influence of a single overload (but by considering three different overload ratios) on the fatigue crack growth retardation of center-cracked AM60B magnesium alloy plates is experimentally investigated. The retardation effect on crack growth due to an applied overload within a random-amplitude loading scenario, using various “clipping levels”, is also investigated. The sensitivity of this material to overload is compared with the response of some other materials.The actual radius of the plastic zone is evaluated for various stress intensity factors, using the finite element method. The results indicate that depending on the material, the affected zone would be sometimes larger or smaller than that produced by Wheeler’s model. Subsequently, a new parameter, hereafter referred to as the “sensitivity parameter” (β), is introduced that enables one to evaluate the affected zone dimension more accurately. It is shown that the proposed modified model is more effective than the original one in predicting the retardation response of the alloy. The integrity of the modified model is also investigated by evaluating the retardation in some other materials.
Keywords:Overload  Sensitivity parameter  Retardation  Wheeler model  Clipping level
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