Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/16507
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dc.contributor.authorVikneswaran Narayanan
dc.date.accessioned2009-05-26T08:54:10Z
dc.date.available2009-05-26T08:54:10Z
dc.date.copyright2009en_US
dc.date.issued2009
dc.identifier.urihttp://hdl.handle.net/10356/16507
dc.description.abstractAn 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 to predict the services life‟s and crack propagation characteristics of the aircraft component parts. It was shown during the course of the experiments that the fatigue life‟s can be performed with reasonable accuracy and efficiency. This was demonstrated by investigations firstly on flat plate aluminum alloys with surface cracks and then validated by comparing it with experimental test date. This research was also done on typical aircraft lugs to predict the service life of aircraft component parts and simulate the crack propagation lines in a practical manner.en_US
dc.format.extent58 p.en_US
dc.language.isoenen_US
dc.rightsNanyang Technological University
dc.subjectDRNTU::Engineering::Aeronautical engineering::Materials of constructionen_US
dc.titleFatigue crack growth analysis of aircraft structural materialen_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.supervisorPang Hock Lye, Johnen_US
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen_US
dc.description.degreeBachelor of Engineering (Aerospace Engineering)en_US
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Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)
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