Static tensile and fatigue and testing of aluminium plate with holes and cracks

• المؤلف الرئيسي: Yeap, Shi Hong
• مؤلفون آخرون: Chai Gin Boay
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2011
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Materials of construction; DRNTU::Engineering::Materials::Mechanical strength of materials
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/46165
• المؤسسة: Nanyang Technological University

In an aircraft structure, fatigue failures usually started from the initiation and propagation of cracks from notches or defects. For example, an aircraft usually has a lot of rivet holes. High stress concentrations are usually found on these holes and these are the likely places for the development...