Skin-stringer interface failure investigation of stringer-stiffened curved composite panels under hail ice impact

Engineering

• Composite Panel 100%
• Joints (Structural Components) 66%
• Impact Velocity 66%
• Stress Wave 66%
• Finite Element Analysis 66%
• Delamination 66%
• Dynamic Behavior 33%
• Numerical Methods 33%
• Loading Condition 33%
• Epoxy Composite 33%
• Failure Mechanism 33%
• Airframe 33%
• Dynamic Response 33%
• Scale Aircraft 33%
• Boundary Condition 33%
• Damage Mode 33%

Keyphrases

• Failure Investigation 100%
• Curved Composite Panels 100%
• Hail Ice Impact 100%
• Ice Sphere 33%
• Hail Ice 33%
• Residual Strength Evaluation 16%
• Delamination Area 16%
• Bonded Joints 16%
• Wave-dominated 16%
• Nonuniform Stiffness 16%
• Ice Composite 16%
• Sphere Impact 16%

Earth and Planetary Sciences

• Delamination 100%
• Impact Velocity 66%
• Stress Wave 66%
• Failure Mechanism 33%
• Mathematical Method 33%
• Dynamic Response 33%
• Bonded Joint 33%
• Residual Strength 33%