Keyphrases
Design Performance
100%
Design Analysis
100%
Aircraft Panel
100%
Composite Patch Repair
100%
Adhesively Bonded Composites
100%
Bonded Composite Patch
100%
Aluminum Panels
100%
Composite Patch
75%
Boron
50%
Military
50%
Aircraft Structure
50%
Skin Stress
50%
Epoxy
25%
Aging
25%
Service Life
25%
Advanced Composites
25%
Assure
25%
U.S. Air Force
25%
Patch Material
25%
Tension Test
25%
Stress Distribution
25%
Degrees of Freedom
25%
Analytical Results
25%
Stress Value
25%
Crack Front
25%
Nonlinear Finite Element Analysis
25%
Testing Machine
25%
Adhesive Materials
25%
Stress Decrease
25%
Uniaxial Tensile Test
25%
Instron
25%
Load Capability
25%
Aerodynamic Loads
25%
Structural Loads
25%
Pre-crack
25%
AA2024-T3
25%
Structural Efficiency
25%
Epoxy Composites
25%
Uniaxial Tensile Loading
25%
Composite Ply
25%
Continued Airworthiness
25%
Repaired Structure
25%
Stress Shift
25%
Hexagonal Elements
25%
Engineering
Patch Repair
100%
Bonded Composite Patch
100%
Aluminum Panel
100%
Design Analysis
100%
Composite Patch
75%
Tensile Testing
50%
Test Specimen
50%
Aircraft Structure
50%
Boron Epoxy
50%
Experimental Investigation
25%
Degree of Freedom
25%
Tensiles
25%
Crack Front
25%
Testing Machine
25%
Analytical Result
25%
Linear Finite Element
25%
Structural Load
25%
Epoxy Adhesive
25%
Epoxy Composite
25%
Clad Aluminum
25%
Advanced Composite
25%
Epoxy Patch
25%
Composite Ply
25%
Continued Airworthiness
25%
Aerodynamic Load
25%
Critical Point
25%
Finite Element Analysis
25%
Service Life
25%