An experimental investigation of the impact response and Post-impact shear buckling behaviour of hybrid composite laminates

Engineering

• Lamination 100%
• Reduction 66%
• Thickness 66%
• Buckling Load 66%
• Matrix Cracking 66%
• Failure Load 66%
• Hybrid Composite 33%
• Buckling Behavior 33%
• Impact Energy 33%
• Energy Level 33%
• Glass Laminate 33%
• Carbon Laminate 33%
• Experimental Investigation 33%
• Buckling 33%
• Glass Surface 33%
• In-Plane Shear 33%
• Fibre Breakage 33%
• Damage Location 33%
• Impact Loads 33%
• Shear Behavior 33%
• Impact Response 33%
• Delamination 33%