Effect of loading rates on behaviour of titanium alloys for aerospace structures

Titanium 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...

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Bibliographic Details
Main Author: Tan, Kenneth Hong Yi.
Other Authors: School of Mechanical and Aerospace Engineering
Format: Final Year Project (FYP)
Language:English
Published: 2013
Subjects:
Online Access:http://hdl.handle.net/10356/53950
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author Tan, Kenneth Hong Yi.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Tan, Kenneth Hong Yi.
author_sort Tan, Kenneth Hong Yi.
collection NTU
description Titanium 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.
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spelling ntu-10356/539502023-03-04T18:37:00Z Effect of loading rates on behaviour of titanium alloys for aerospace structures Tan, Kenneth Hong Yi. School of Mechanical and Aerospace Engineering Li Peifeng DRNTU::Engineering Titanium 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. Bachelor of Engineering (Aerospace Engineering) 2013-06-10T07:12:26Z 2013-06-10T07:12:26Z 2013 2013 Final Year Project (FYP) http://hdl.handle.net/10356/53950 en Nanyang Technological University 53 p. application/pdf
spellingShingle DRNTU::Engineering
Tan, Kenneth Hong Yi.
Effect of loading rates on behaviour of titanium alloys for aerospace structures
title Effect of loading rates on behaviour of titanium alloys for aerospace structures
title_full Effect of loading rates on behaviour of titanium alloys for aerospace structures
title_fullStr Effect of loading rates on behaviour of titanium alloys for aerospace structures
title_full_unstemmed Effect of loading rates on behaviour of titanium alloys for aerospace structures
title_short Effect of loading rates on behaviour of titanium alloys for aerospace structures
title_sort effect of loading rates on behaviour of titanium alloys for aerospace structures
topic DRNTU::Engineering
url http://hdl.handle.net/10356/53950
work_keys_str_mv AT tankennethhongyi effectofloadingratesonbehaviouroftitaniumalloysforaerospacestructures