Keyphrases
Carbon-epoxy Laminate
100%
Fracture Energy
100%
Toughening Mechanism
100%
In-situ SEM
100%
Fracture Characterization
100%
Thermoplastic Veils
100%
Polyphenylene Sulfide
75%
Delamination
50%
Double Cantilever Beam Specimen
50%
Polyetherimide
50%
Mode I Fracture Energy
50%
Scanning Electron Microscopy
25%
Loading Conditions
25%
Resin
25%
Crack Propagation
25%
Carbon Fiber
25%
Fiber Dispersion
25%
Nonwoven
25%
Fiber Diameter
25%
Epoxy Resin
25%
Fiber Pull-out
25%
Fracture Surface
25%
Lamin
25%
Aerospace
25%
Specific Surface Area
25%
Specimen Geometry
25%
Microdamage
25%
Carbon Fiber Epoxy
25%
Araldite
25%
Fracture Toughening
25%
Damage Evolution
25%
Miniature Specimen
25%
Fiber Bridging
25%
Fiber-matrix Debonding
25%
Interlaminar Fracture
25%
Non-crimp Fabric Composites
25%
Vacuum Assisted Resin Infusion
25%
Areal Weight
25%
Non-crimp Fabric
25%
Fibre Discontinuity
25%
Energy Mechanism
25%
Non-woven Veil
25%
Out-of-autoclave
25%
Embedded Fibres
25%
Epoxy Resin Systems
25%
Engineering
Toughening
100%
Fracture Energy
100%
Carbon-Epoxy Laminate
100%
Poly-Phenylene Sulphide
50%
Double-Cantilever Beam
33%
Beam Specimen
33%
Mode I Fracture
33%
Polyetherimide
33%
Non-Crimp Fabric
33%
Delamination
33%
Epoxy Laminate
16%
Micrograph
16%
Loading Condition
16%
Embedded Fiber
16%
Fiber Dispersion
16%
Bridging
16%
Fiber Diameter
16%
Fracture Surface
16%
Specimen Geometry
16%
Debonding
16%
Microdamage
16%
Crack Propagation
16%
Specific Surface Area
16%
Damage Evolution
16%
Material Science
Scanning Electron Microscopy
100%
Thermoplastics
100%
Carbon Fiber
75%
Polyphenylene
75%
Delamination
50%
Crack Propagation
25%
Epoxy
25%
Debonding
25%
Composite Fabrics
25%
Damage Evolution
25%