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Novel adherend laminate designs for composite bonded joints
J.A. Kupski
Structural Integrity & Composites
Research output
:
Thesis
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Dissertation (TU Delft)
83
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Dive into the research topics of 'Novel adherend laminate designs for composite bonded joints'. Together they form a unique fingerprint.
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INIS
design
100%
damage
100%
failures
87%
thickness
75%
topology
68%
fingers
62%
adhesives
37%
peaks
31%
interfaces
25%
stiffness
25%
geometry
18%
polymers
18%
bending
18%
comparative evaluations
18%
acoustics
18%
carbon fibers
18%
performance
18%
strains
18%
shear
18%
emission
12%
bonding
12%
energy
12%
efficiency
12%
weight
12%
length
12%
cracks
12%
increasing
6%
surfaces
6%
finite element method
6%
tensile strength
6%
testing
6%
simulation
6%
joining
6%
metals
6%
layers
6%
microscopes
6%
crack propagation
6%
nonlinear problems
6%
resins
6%
correlations
6%
images
6%
yields
6%
shear strength
6%
aircraft
6%
configuration
6%
orientation
6%
plasticity
6%
experimental data
6%
fractures
6%
Engineering
Joints (Structural Components)
100%
Composite
100%
Design
100%
Damage Initiation
50%
Ply Thickness
45%
Peel Stress
27%
Final Failure
27%
Overlap Joint
18%
Joint Strength
18%
Failure (Mechanical)
18%
Design Parameter
18%
Single Lap Joint
18%
Bending Stiffness
13%
Carbon Fibre Reinforced Polymer
13%
High Load
13%
Maximum Load
13%
Bond Line
9%
Thickness
9%
Overlap Length
9%
Efficiency
9%
Performance
9%
Tensiles
9%
Acoustic Emission
9%
Failure Analysis
9%
Joint Design
9%
Cohesive Failure
4%
Stress Component
4%
Tensile Stress σ
4%
Digital Image Correlation
4%
Scale Structure
4%
Finite Element Method
4%
Experimental Result
4%
Failure Mode
4%
Fracture Surface
4%
Requirement
4%
Acoustic Energy
4%
Local Region
4%
Mechanical Performance
4%
Joining Technology
4%
Butt Joint
4%
Progression
4%
Stress Field
4%
Emission Measurement
4%
Fillet Geometry
4%
Strain Energy
4%
Crack Path
4%
Damage Onset
4%
Propagating Crack
4%
Testing
4%
Crack Initiation
4%
Lap Shear Strength
4%
Yield
4%
Tensile Test
4%
Experiments
4%
Detrimental Effect
4%
Full Scale
4%
Design Feature
4%
Adhesive Interface
4%
Beneficial Effect
4%
Design Concept
4%
Laminate
4%
Tensile Loads
4%
Ultimate Tensile Strength
4%
Overlap Region
4%
Fuselage
4%
Thin Ply
4%
Strain Field
4%
Material Science
Bonded Joint
100%
Composite Material
100%
Mechanical Strength
44%
Stiffness
44%
Adhesive
44%
Carbon Fiber
33%
Reinforced Plastic
33%
Bending
33%
Crack
22%
Ultimate Tensile Strength
22%
Tensile Loads
11%
Adhesive Bonding
11%
Materials
11%
Finite Element Method
11%
Plasticity
11%
Resin
11%
Laminated Composite
11%
Crack Initiation
11%
Metal
11%
Shear Strength
11%
Surface
11%
Stress Field
11%
Aircraft
11%
Keyphrases
Feature Stacking
9%
Polymer-bonded
9%
Global Topology
9%
Fuselage Structure
9%
Spew Fillet
9%
Global Geometry
9%
Traditional Joint
9%