Filament wound composite fatigue mechanisms investigated with full field DIC strain monitoring

Fatigue of filament wound materials was investigated using Digital Image Correlation DIC monitoring every 50th cycle of a high cycle fatigue test of a split disk ring sample. The ring was cut from a filament wound glass fiber reinforced polymer pressure vessel and had a hole. The strain field redist...

Descripción completa

Guardado en:

Detalles Bibliográficos
Autores principales:	Hugaas Eivind, Echtermeyer Andreas T.
Formato:	article
Lenguaje:	EN
Publicado:	De Gruyter 2021
Materias:	composites filament winding fatigue digital image correlation progressive damage strain fields Engineering (General). Civil engineering (General) TA1-2040
Acceso en línea:	https://doaj.org/article/e4af5589d02e417a8abe53a58083a37f
Etiquetas:	Agregar Etiqueta Sin Etiquetas, Sea el primero en etiquetar este registro!

id	oai:doaj.org-article:e4af5589d02e417a8abe53a58083a37f
record_format	dspace
spelling	oai:doaj.org-article:e4af5589d02e417a8abe53a58083a37f2021-12-05T14:10:46ZFilament wound composite fatigue mechanisms investigated with full field DIC strain monitoring2391-543910.1515/eng-2021-0041https://doaj.org/article/e4af5589d02e417a8abe53a58083a37f2021-01-01T00:00:00Zhttps://doi.org/10.1515/eng-2021-0041https://doaj.org/toc/2391-5439Fatigue of filament wound materials was investigated using Digital Image Correlation DIC monitoring every 50th cycle of a high cycle fatigue test of a split disk ring sample. The ring was cut from a filament wound glass fiber reinforced polymer pressure vessel and had a hole. The strain field redistributed over time, lowering and moving strain concentrations. The redistributive behavior was most extensive in areas that later developed local fiber failure, which soon led to catastrophic failure. Microscopy was carried out on partially fatigued material. Damage evolved as matrix cracks and matrix splitting of groups of fibers and complete debonding of single fibers. This occurred at borders of voids and matrix cracks, easing progressive fiber failure. It was concluded that fatigue in filament wound composites has an extensive matrix damage phase before final failure. Fibers could locally withstand strains close to and above the static failure strain for considerable number of cycles if little local strain field redistribution was observed. The used method was able to detect changes in the strain fields that preceded catastrophic failure. It was concluded that DIC combined with the post processing methods presented may serve as a valuable tool for structural integrity monitoring of composite pressure vessels over time.Hugaas EivindEchtermeyer Andreas T.De Gruyterarticlecompositesfilament windingfatiguedigital image correlationprogressive damagestrain fieldsEngineering (General). Civil engineering (General)TA1-2040ENOpen Engineering, Vol 11, Iss 1, Pp 401-413 (2021)
institution	DOAJ
collection	DOAJ
language	EN
topic	composites filament winding fatigue digital image correlation progressive damage strain fields Engineering (General). Civil engineering (General) TA1-2040
spellingShingle	composites filament winding fatigue digital image correlation progressive damage strain fields Engineering (General). Civil engineering (General) TA1-2040 Hugaas Eivind Echtermeyer Andreas T. Filament wound composite fatigue mechanisms investigated with full field DIC strain monitoring
description	Fatigue of filament wound materials was investigated using Digital Image Correlation DIC monitoring every 50th cycle of a high cycle fatigue test of a split disk ring sample. The ring was cut from a filament wound glass fiber reinforced polymer pressure vessel and had a hole. The strain field redistributed over time, lowering and moving strain concentrations. The redistributive behavior was most extensive in areas that later developed local fiber failure, which soon led to catastrophic failure. Microscopy was carried out on partially fatigued material. Damage evolved as matrix cracks and matrix splitting of groups of fibers and complete debonding of single fibers. This occurred at borders of voids and matrix cracks, easing progressive fiber failure. It was concluded that fatigue in filament wound composites has an extensive matrix damage phase before final failure. Fibers could locally withstand strains close to and above the static failure strain for considerable number of cycles if little local strain field redistribution was observed. The used method was able to detect changes in the strain fields that preceded catastrophic failure. It was concluded that DIC combined with the post processing methods presented may serve as a valuable tool for structural integrity monitoring of composite pressure vessels over time.
format	article
author	Hugaas Eivind Echtermeyer Andreas T.
author_facet	Hugaas Eivind Echtermeyer Andreas T.
author_sort	Hugaas Eivind
title	Filament wound composite fatigue mechanisms investigated with full field DIC strain monitoring
title_short	Filament wound composite fatigue mechanisms investigated with full field DIC strain monitoring
title_full	Filament wound composite fatigue mechanisms investigated with full field DIC strain monitoring
title_fullStr	Filament wound composite fatigue mechanisms investigated with full field DIC strain monitoring
title_full_unstemmed	Filament wound composite fatigue mechanisms investigated with full field DIC strain monitoring
title_sort	filament wound composite fatigue mechanisms investigated with full field dic strain monitoring
publisher	De Gruyter
publishDate	2021
url	https://doaj.org/article/e4af5589d02e417a8abe53a58083a37f
work_keys_str_mv	AT hugaaseivind filamentwoundcompositefatiguemechanismsinvestigatedwithfullfielddicstrainmonitoring AT echtermeyerandreast filamentwoundcompositefatiguemechanismsinvestigatedwithfullfielddicstrainmonitoring
_version_	1718371750803144704

Filament wound composite fatigue mechanisms investigated with full field DIC strain monitoring

Ejemplares similares