Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/53950
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dc.contributor.authorTan, Kenneth Hong Yi.
dc.date.accessioned2013-06-10T07:12:26Z
dc.date.available2013-06-10T07:12:26Z
dc.date.copyright2013en_US
dc.date.issued2013
dc.identifier.urihttp://hdl.handle.net/10356/53950
dc.description.abstractTitanium and its alloys are highly desirable materials to be used in the aerospace industry due to its high strength and light weight. It is commonly used as airframe components on the airplane and could be subjected to different impact velocity. In this project, development of the microstructure of two types of titanium –CP-Ti and Ti-6Al-4V compressed at quasi-static and dynamic rates were investigated. The experiment was conducted using the INSTRON tester for quasi-static compression and SHPB for the dynamic compression testing. The microstructures of both materials at different strains were analysed and the microstructure of the Ti-6Al-4V specimens showed different deformation characteristic when subjected to quasi-static and dynamic compression.en_US
dc.format.extent53 p.en_US
dc.language.isoenen_US
dc.rightsNanyang Technological University
dc.subjectDRNTU::Engineeringen_US
dc.titleEffect of loading rates on behaviour of titanium alloys for aerospace structuresen_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen_US
dc.description.degreeBachelor of Engineering (Aerospace Engineering)en_US
dc.contributor.supervisor2Li Peifengen_US
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Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)
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