Face/core disbond fatigue growth in honeycomb cored aircraft sandwich elements under mixed mode flatwise tension loading

Engineering

• Mixed Mode 100%
• Core Interface 66%
• Mode Mixity 66%
• Two Dimensional 33%
• Input Data 33%
• Good Agreement 33%
• Experimental Measurement 33%
• Numerical Prediction 33%
• Interface Crack 33%
• Test Specimen 33%
• Double-Cantilever Beam 33%
• Energy Release Rate 33%
• Beam Specimen 33%
• Fatigue Analysis 33%
• Damage Growth 33%
• Sandwich Structures 33%
• Nomex 33%
• Fatigue Crack Propagation 33%
• Fatigue Model 33%
• Crack Surface Displacement 33%
• Mode Separation 33%
• Finite Element Modeling 33%
• Crack Propagation 33%
• Numerical Model 33%
• Fracture Mechanics 33%
• Bending Moment 33%
• Phase Angle 33%
• Subroutine 33%

Keyphrases

• Flatwise Tension 100%
• Modified Paris Law 50%
• Crack Propagation Energy 50%