Engineering
Carbon-Epoxy Laminate
100%
Temperature Dependency
100%
Nanofiber
100%
Toughening
100%
Electrospun
100%
Nanolayers
33%
Cohesive Failure
16%
End-Notched Flexure
16%
Epoxy Composite
16%
Damage Mechanism
16%
Damage Propagation
16%
Fracture Surface
16%
Impact Toughness
16%
Plastic Deformation
16%
High Temperature Adhesive
16%
Critical Role
16%
Adhesive Failure
16%
Increasing Temperature
16%
Loading Condition
16%
Dynamic Mechanical Analysis
16%
Images
16%
Debonding
16%
Fiber
16%
Elevated Temperature
16%
Low-Temperature
16%
INIS
epoxides
100%
carbon
100%
nanofibers
100%
temperature range 0273-0400 k
50%
failures
33%
surfaces
33%
damage
33%
layers
33%
loading
33%
nanolayers
33%
fractures
33%
increasing
16%
dynamics
16%
low temperature
16%
adhesives
16%
scanning electron microscopy
16%
range
16%
glass
16%
transition temperature
16%
images
16%
carbon fibers
16%
fracture toughness
16%
plasticity
16%
cracks
16%
Material Science
Temperature
100%
Surface
16%
Scanning Electron Microscopy
8%
Carbon Fiber
8%
Composite Laminate
8%
Dynamic Mechanical Analysis
8%
Glass Transition Temperature
8%
Fracture Toughness
8%