Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications
Composite materials have several mechanical qualities that improve their performance in engineering applications and are widely used in many industries. Inclusions and cracks often occur together and are influenced by one another. The crack that forms and spreads to reach the inclusion materia...
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sg-ntu-dr.10356-1816142024-12-14T16:52:46Z Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications Lim, Yu Cong Xiao Zhongmin School of Mechanical and Aerospace Engineering MZXIAO@ntu.edu.sg Engineering Composite materials have several mechanical qualities that improve their performance in engineering applications and are widely used in many industries. Inclusions and cracks often occur together and are influenced by one another. The crack that forms and spreads to reach the inclusion material will either stop or continue to propagate when an inclusion with a comparatively different Young's modulus occurs in a plate. The stress intensity factor (SIF), which aids in crack propagation prediction, can be found by measuring the separation between the inclusion and the crack tip. Ansys software is being used for the project to simulate a two- dimensional model that solely addresses plane strain. Because of this assumption, the complexity and equations of the problems have been made simpler, making the solutions more accurate and manageable. Bachelor's degree 2024-12-11T00:30:26Z 2024-12-11T00:30:26Z 2024 Final Year Project (FYP) Lim, Y. C. (2024). Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications. Final Year Project (FYP), Nanyang Technological University, Singapore. https://hdl.handle.net/10356/181614 https://hdl.handle.net/10356/181614 en application/pdf Nanyang Technological University |
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Engineering Lim, Yu Cong Crack-inclusion interaction in composite materials with aerospace and offshore engineering applications |
description |
Composite materials have several mechanical qualities that improve their performance in
engineering applications and are widely used in many industries. Inclusions and cracks often
occur together and are influenced by one another. The crack that forms and spreads to reach
the inclusion material will either stop or continue to propagate when an inclusion with a
comparatively different Young's modulus occurs in a plate. The stress intensity factor (SIF),
which aids in crack propagation prediction, can be found by measuring the separation between
the inclusion and the crack tip. Ansys software is being used for the project to simulate a two-
dimensional model that solely addresses plane strain. Because of this assumption, the
complexity and equations of the problems have been made simpler, making the solutions more
accurate and manageable. |
author2 |
Xiao Zhongmin |
author_facet |
Xiao Zhongmin Lim, Yu Cong |
format |
Final Year Project |
author |
Lim, Yu Cong |
author_sort |
Lim, Yu Cong |
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 |
2024 |
url |
https://hdl.handle.net/10356/181614 |
_version_ |
1819113043009732608 |