Characteristic damage state of symmetric laminates subject to uniaxial monotonic-fatigue loading

•Experiments show sequential occurrence of matrix cracks and induced delaminations in laminates.•Matrix crack density at saturation is shown to change with cracked ply thickness and orientation.•Crack density at saturation is identical under static and fatigue loading with different stresses.•Crack...

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Published inEngineering fracture mechanics Vol. 199; pp. 86 - 100
Main Authors Pakdel, Hamed, Mohammadi, Bijan
Format Journal Article
LanguageEnglish
Published New York Elsevier Ltd 01.08.2018
Elsevier BV
Subjects
Online AccessGet full text
ISSN0013-7944
1873-7315
DOI10.1016/j.engfracmech.2018.05.007

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Abstract •Experiments show sequential occurrence of matrix cracks and induced delaminations in laminates.•Matrix crack density at saturation is shown to change with cracked ply thickness and orientation.•Crack density at saturation is identical under static and fatigue loading with different stresses.•Crack density at saturation is a characteristic damage state (CDS) independent of loading.•CDS can be predicted with an energy based criterion based on energy release rate. Experimental and variational investigation of the onset of matrix crack saturation and induced delamination initiation are performed in laminates containing mid-ply matrix cracks. An evolution criterion is developed based on energy release rate to predict the crack density at saturation which is argued to be a characteristic damage state (CDS) independent of loading. A unit cell based analysis is established upon variational principles to derive the stress state and strain energy of [θm(o)/θn(i)]s laminates containing mid-ply cracks with or without induced delaminations. Tensile static and fatigue experiments are performed on CFRP specimens with different layups under several maximum stress and stress ratios and optical microscopy is used to detect matrix crack density during experiments. The saturation crack densities of laminates subject to static and fatigue loading with different maximum stress and stress ratios confirm the characteristic damage state (CDS) to be independent of loading as argued in the proposed criterion. Analytical predictions of CDS of different layups are shown to be in accordance with experimental observations.
AbstractList Experimental and variational investigation of the onset of matrix crack saturation and induced delamination initiation are performed in laminates containing mid-ply matrix cracks. An evolution criterion is developed based on energy release rate to predict the crack density at saturation which is argued to be a characteristic damage state (CDS) independent of loading. A unit cell based analysis is established upon variational principles to derive the stress state and strain energy of ... laminates containing mid-ply cracks with or without induced delaminations. Tensile static and fatigue experiments are performed on CFRP specimens with different layups under several maximum stress and stress ratios and optical microscopy is used to detect matrix crack density during experiments. The saturation crack densities of laminates subject to static and fatigue loading with different maximum stress and stress ratios confirm the characteristic damage state (CDS) to be independent of loading as argued in the proposed criterion. Analytical predictions of CDS of different layups are shown to be in accordance with experimental observations. (Proquest: ... denotes non-USASCII text omitted.)
•Experiments show sequential occurrence of matrix cracks and induced delaminations in laminates.•Matrix crack density at saturation is shown to change with cracked ply thickness and orientation.•Crack density at saturation is identical under static and fatigue loading with different stresses.•Crack density at saturation is a characteristic damage state (CDS) independent of loading.•CDS can be predicted with an energy based criterion based on energy release rate. Experimental and variational investigation of the onset of matrix crack saturation and induced delamination initiation are performed in laminates containing mid-ply matrix cracks. An evolution criterion is developed based on energy release rate to predict the crack density at saturation which is argued to be a characteristic damage state (CDS) independent of loading. A unit cell based analysis is established upon variational principles to derive the stress state and strain energy of [θm(o)/θn(i)]s laminates containing mid-ply cracks with or without induced delaminations. Tensile static and fatigue experiments are performed on CFRP specimens with different layups under several maximum stress and stress ratios and optical microscopy is used to detect matrix crack density during experiments. The saturation crack densities of laminates subject to static and fatigue loading with different maximum stress and stress ratios confirm the characteristic damage state (CDS) to be independent of loading as argued in the proposed criterion. Analytical predictions of CDS of different layups are shown to be in accordance with experimental observations.
Author Mohammadi, Bijan
Pakdel, Hamed
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Keywords Variational analysis
Fatigue
Characteristic damage state
Induced delamination
Off-axis layup
Matrix cracking
Language English
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Snippet •Experiments show sequential occurrence of matrix cracks and induced delaminations in laminates.•Matrix crack density at saturation is shown to change with...
Experimental and variational investigation of the onset of matrix crack saturation and induced delamination initiation are performed in laminates containing...
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SubjectTerms Carbon fiber reinforced plastics
Characteristic damage state
Crack initiation
Crack propagation
Cracks
Criteria
Damage
Density
Energy release rate
Fatigue
Fatigue cracks
Fatigue failure
Fatigue life
Fracture mechanics
Induced delamination
Laminates
Matrix cracking
Matrix cracks
Off-axis layup
Optical microscopy
Saturation
Stress-strain curves
Stresses
Unit cell
Variational analysis
Variational principles
Title Characteristic damage state of symmetric laminates subject to uniaxial monotonic-fatigue loading
URI https://dx.doi.org/10.1016/j.engfracmech.2018.05.007
https://www.proquest.com/docview/2114215586
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