Self healing of metal composite interface

Studies on self-healing material have gained an importance in many applications which reduce the maintenance cost and reusability of the product. The application extends to all fields from automotive to aerospace. Fibre metal laminate is a hybrid material used nowadays due to its structural integ...

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Main Author: Shanmugam Logesh
Other Authors: Yang Jinglei
Format: Theses and Dissertations
Language:English
Published: 2016
Subjects:
Online Access:http://hdl.handle.net/10356/68797
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-687972023-03-11T16:53:01Z Self healing of metal composite interface Shanmugam Logesh Yang Jinglei School of Mechanical and Aerospace Engineering DRNTU::Engineering::Aeronautical engineering Studies on self-healing material have gained an importance in many applications which reduce the maintenance cost and reusability of the product. The application extends to all fields from automotive to aerospace. Fibre metal laminate is a hybrid material used nowadays due to its structural integrity which is a combination of metal and composite. Often, there is a delamination between metal and composite interface if the bonding behaviour is weak. However, introducing a polymer interleaf will increase the bonding strength between metal and composite interface. This thesis presents an investigation of selfhealing and toughening performance of co-polymer (EMAA-polyethylene-co-meth acrylic acid) between composite adherend and metal composite interface (MCI). Furthermore, redux335k, which is a structural adhesive, used as a benchmark for both composite and metal composite specimens in this study. Carbon fibre composites were fabricated from unidirectional pre-preg with thin film of adhesive placed between composite plies and metal composite interface. Results from the double-cantilever-beam test showed that the incorporation of mendable thin film polymers improves interlaminar fracture toughness. This toughness gradually decreases upon further healing of material for three different cycles with the same procedures being followed. Recovery of self-healing material is about 72% for the first heal, 40 % for the second heal and 30% for the third heal. Moreover, the fracture toughness of the self-healing material is higher than redux335k for both monolithic composite specimen and hybrid specimen. Several methods are detailed to discuss the degradation of self-healing between MCI. Comparison of redux335k and self-healing copolymer EMAA is also shown in this thesis. Master of Science (Aerospace Engineering) 2016-06-01T04:28:47Z 2016-06-01T04:28:47Z 2016 Thesis http://hdl.handle.net/10356/68797 en 99 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Aeronautical engineering
spellingShingle DRNTU::Engineering::Aeronautical engineering
Shanmugam Logesh
Self healing of metal composite interface
description Studies on self-healing material have gained an importance in many applications which reduce the maintenance cost and reusability of the product. The application extends to all fields from automotive to aerospace. Fibre metal laminate is a hybrid material used nowadays due to its structural integrity which is a combination of metal and composite. Often, there is a delamination between metal and composite interface if the bonding behaviour is weak. However, introducing a polymer interleaf will increase the bonding strength between metal and composite interface. This thesis presents an investigation of selfhealing and toughening performance of co-polymer (EMAA-polyethylene-co-meth acrylic acid) between composite adherend and metal composite interface (MCI). Furthermore, redux335k, which is a structural adhesive, used as a benchmark for both composite and metal composite specimens in this study. Carbon fibre composites were fabricated from unidirectional pre-preg with thin film of adhesive placed between composite plies and metal composite interface. Results from the double-cantilever-beam test showed that the incorporation of mendable thin film polymers improves interlaminar fracture toughness. This toughness gradually decreases upon further healing of material for three different cycles with the same procedures being followed. Recovery of self-healing material is about 72% for the first heal, 40 % for the second heal and 30% for the third heal. Moreover, the fracture toughness of the self-healing material is higher than redux335k for both monolithic composite specimen and hybrid specimen. Several methods are detailed to discuss the degradation of self-healing between MCI. Comparison of redux335k and self-healing copolymer EMAA is also shown in this thesis.
author2 Yang Jinglei
author_facet Yang Jinglei
Shanmugam Logesh
format Theses and Dissertations
author Shanmugam Logesh
author_sort Shanmugam Logesh
title Self healing of metal composite interface
title_short Self healing of metal composite interface
title_full Self healing of metal composite interface
title_fullStr Self healing of metal composite interface
title_full_unstemmed Self healing of metal composite interface
title_sort self healing of metal composite interface
publishDate 2016
url http://hdl.handle.net/10356/68797
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