Fatigue crack growth analysis of aircraft structural material

• المؤلف الرئيسي: Vikneswaran Narayanan
• مؤلفون آخرون: Pang Hock Lye, John
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2009
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Materials of construction
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/16507
• المؤسسة: Nanyang Technological University

An experimental fatigue life analysis was performed using the Air Force Growth(AFGROW) crack life prediction software for predicting the life of aircraft structural components. The research was twofold. Firstly was to gain exposure into a commercially available software AFGROW and the second was...