Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications
Composite materials have been widely used in many industries as its multiple mechanical properties that provide a better performance in engineering applications. Cracks and inclusion are often occurred together and are influence by each of them. When an inclusion has a relatively different you...
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2023
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sg-ntu-dr.10356-1677282023-06-03T16:52:06Z Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications Soon, Jun Hong Xiao Zhongmin School of Mechanical and Aerospace Engineering MZXIAO@ntu.edu.sg Engineering::Mechanical engineering Composite materials have been widely used in many industries as its multiple mechanical properties that provide a better performance in engineering applications. Cracks and inclusion are often occurred together and are influence by each of them. When an inclusion has a relatively different young’s modulus is occurred in a plate, the crack which occurs and propagates to reach the inclusion material would either stop or continue propagating. The distance between the crack tip and inclusion can determine the stress intensity factor (SIF) which help to predict propagation of crack. The project is using Ansys software to simulate a two-dimensional model, which only focus on plane strain. This assumption has been simplified the equations and complexity of problems leading to a more manageable and accurate solutions. Bachelor of Engineering (Mechanical Engineering) 2023-06-03T13:20:21Z 2023-06-03T13:20:21Z 2023 Final Year Project (FYP) Soon, J. H. (2023). Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications. Final Year Project (FYP), Nanyang Technological University, Singapore. https://hdl.handle.net/10356/167728 https://hdl.handle.net/10356/167728 en P-B035 application/pdf Nanyang Technological University |
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Engineering::Mechanical engineering Soon, Jun Hong Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications |
description |
Composite materials have been widely used in many industries as its multiple
mechanical properties that provide a better performance in engineering applications.
Cracks and inclusion are often occurred together and are influence by each of them.
When an inclusion has a relatively different young’s modulus is occurred in a plate, the
crack which occurs and propagates to reach the inclusion material would either stop or
continue propagating. The distance between the crack tip and inclusion can determine
the stress intensity factor (SIF) which help to predict propagation of crack. The project
is using Ansys software to simulate a two-dimensional model, which only focus on
plane strain. This assumption has been simplified the equations and complexity of
problems leading to a more manageable and accurate solutions. |
author2 |
Xiao Zhongmin |
author_facet |
Xiao Zhongmin Soon, Jun Hong |
format |
Final Year Project |
author |
Soon, Jun Hong |
author_sort |
Soon, Jun Hong |
title |
Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications |
title_short |
Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications |
title_full |
Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications |
title_fullStr |
Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications |
title_full_unstemmed |
Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications |
title_sort |
crack-inclusion interaction in composite materials with aerospace and offshore engineering applications |
publisher |
Nanyang Technological University |
publishDate |
2023 |
url |
https://hdl.handle.net/10356/167728 |
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1772827346921848832 |