Damage behavior and assessment of aeronautical PMMA subjected to high-velocity water-jet impact

Engineering

• Aircraft Component 33%
• Characteristic Feature 33%
• Circumferential Crack 33%
• Damage Assessment 100%
• Damage Behavior 100%
• Damage Mechanism 33%
• Damaged Area 66%
• Delamination 33%
• Fighter Aircraft 33%
• Impact Event 33%
• Impact Velocity 33%
• Incident Angle 33%
• Initial Stage 33%
• Jet Velocity 33%
• Linear Relationship 33%
• Marine Safety 33%
• Single Impact 33%
• Stress Wave Interaction 33%
• Subsurface 66%
• Surface Crack 33%