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Fatigue simulation for Ti/GFRP laminates using cohesive elements
T. Yamaguchi,
T. Okabe
, T. Kosaka
ENG - Aerospace Engineering
Research output
:
Contribution to journal
›
Article
›
peer-review
8
Citations (Scopus)
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Dive into the research topics of 'Fatigue simulation for Ti/GFRP laminates using cohesive elements'. Together they form a unique fingerprint.
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Engineering
Cohesive Element
100%
Crack Growth Rate
16%
Cyclic Loading
16%
Degradation Process
16%
Experiments
16%
Fatigue Damage Process
33%
Fibre Metal Laminate
66%
Glass Fibre-Reinforced Plastic
33%
Hybrid
16%
Lamination
16%
Models
50%
Nodes
33%
Numerical Approach
16%
Sheet Metal
16%
Simulated Result
16%
Simulation
33%
Transverse Cracking
100%
Physics
Crack Growth
50%
Damage Mechanics
50%
Fatigue Damage
100%
Glass Fiber Reinforced Plastics
33%
Independent Variables
16%
Model
50%
Simulation
33%
Splitting
33%
Titanium
33%
Material Science
Delamination
66%
Finite Element Methods
33%
Glass Fiber Reinforced Plastics
33%
Plastic Laminate
33%
Sheet Metal
16%