Experimental analysis and investigation of the phenomenon of fatigue in the connections of ship

Majid askary sayar1 Amir reza bahri2

Abstract :
In materials science, fatigue is the initiation and propagation of cracks in a material due to cyclic loading. Once a fatigue crack has initiated, it grows a small amount with each loading cycle, typically producing striations on some parts of the fracture surface. The crack will continue to grow until it reaches a critical size, which occurs when the stress intensity factor of the crack exceeds the fracture toughness of the material, producing rapid propagation and typically complete fracture of the structure. Fatigue cracking is one of the primary damage mechanisms of structural components. Fatigue cracking results from cyclic stresses that are below the ultimate tensile stress, or even the yield stress of the material. The name “fatigue” is based on the concept that a material becomes “tired” and fails at a stress level below the nominal strength of the material. The fact that the original bulk design strengths are not exceeded and the only warning sign of an impending fracture is often just a tiny crack, makes fatigue damage especially dangerous. Fatigue has traditionally been associated with the failure of metal components which led to the term metal fatigue. In the nineteenth century, the sudden failing of metal railway axles was thought to be caused by the metal crystallizing because of the brittle appearance of the fracture surface, but this has since been disproved. Most materials, such as composites, plastics and ceramics, seem to experience some sort of fatigue-related failure. To aid in predicting the fatigue life of a component, fatigue tests are carried out using coupons to measure the rate of crack growth by applying constant amplitude cyclic loading and averaging the measured growth of a crack over thousands of cycles. However, there are also a number of special cases that need to be considered where the rate of crack growth is significantly different compared to that obtained from constant amplitude testing. Such as the reduced rate of growth that occurs for small loads near the threshold or after the application of an overload; and the increased rate of crack growth associated with short cracks or after the application of an underload.

Keywords : structural survivability experimental method crack growth fracture strain energy


زبان مقاله : انگلیسی
محور مقاله : مهندسی مکانیک
محل انتشار : هفتمین کنفرانس بین المللی پژوهش های کاربردی در علوم و مهندسی
آدرس وب سایت کنفرانس : 7carse.com
کد IOI مقاله : XGZK-HHGKE
لینک مستقیم مقاله : https://isnac.ir/XGZK-HHGKE

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