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Delamination Analysis of A Class of AP-PLY Composite Laminates
Weiling Zheng
Aerospace Structures & Computational Mechanics
Research output
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Thesis
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Dissertation (TU Delft)
320
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Dive into the research topics of 'Delamination Analysis of A Class of AP-PLY Composite Laminates'. Together they form a unique fingerprint.
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INIS
accuracy
22%
applications
11%
architecture
11%
beams
66%
bending
22%
capacity
11%
corrections
11%
crack growth
11%
crack propagation
11%
cracks
100%
damage
33%
energy
100%
failures
22%
fibers
11%
finite element method
33%
growth
22%
inclusions
11%
industry
11%
interfaces
11%
layers
33%
loading
11%
membranes
11%
optimization
33%
resins
33%
singularity
22%
solutions
11%
speed
11%
stiffness
11%
strains
88%
thickness
11%
tolerance
22%
Engineering
Beam Structure
10%
Characteristics
10%
Cohesive Element
10%
Composite
100%
Composite Beam
30%
Composite Structure
20%
Correction Factor
10%
Delamination
100%
Delamination Growth
10%
Delamination Onset
20%
Equivalent Stiffness
10%
Existing Crack
10%
Failure Process
10%
Fiber
10%
Finite Element Solution
10%
Laminate
70%
Low Speed
10%
Maximum Stress Criterion
10%
Models
10%
Neutral Axis
10%
Numerical Calculation
10%
Obtains
10%
Optimization
30%
Plane Load
10%
Singularities
20%
Step Approach
10%
Strain-Energy Release Rate
70%
Thickness Direction
10%
Three-Point Bending Test
10%
Material Science
Analytical Method
11%
Beam Theory
11%
Bending
22%
Composite Laminate
100%
Composite Material
44%
Composite Structure
22%
Crack
55%
Crack Growth
11%
Crack Propagation
11%
Damage Tolerance
22%
Dissimilar Material
11%
Fiber
11%
Finite Element Method
11%
Finite Element Modeling
22%
Isotropic Material
11%
Membrane
11%
Resin
33%
Small Crack
22%
Stiffness
11%