The effect of laminate stacking sequence of CFRP filament wound tubes subjected to projectile impact

Composite Structures

Volumn 58, Issue 2, 2002, Pages 259-270

  Will, M A ^a   Franz, T ^a   Nurick, G N ^a  

^a UNIVERSITY OF CAPE TOWN   (South Africa)

Author keywords

Carbon fibre reinforced polymer; Energy dissipation absorption; Filament wound; Projectile impact; Stacking sequence

Indexed keywords

CARBON FIBERS; ENERGY DISSIPATION; FRICTION; KINETIC ENERGY; LAMINATES; STRAIN;

STACKING SEQUENCES;

COMPOSITE STRUCTURES;

CARBON FIBER; FIBER REINFORCED COMPOSITE; IMPACT; INDUSTRIAL TEXTILE; KINETICS; LAMINATE;

EID: 0036839294     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(02)00050-8     Document Type: Article

References (17)

1. Predicting the penetration and perforation of FRP laminates struck normally by projectiles with different nose shapes
2. Penetration and perforation of thick FRP laminates
3. Numerical modelling of impact damage
4. The impact resistance of composite materials - A review
5. The effect of stacking sequence on impact damage in a carbon fibre/epoxy composite
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7. Experimental measurement of impact response in carbon/epoxy plates
8. Numerical simulation of fragmentation of composite material plates due to impact
9. Strength, toughness and fatigue properties
10. High strain-rate mechanical properties of a torospherical shell composed of IM7/E7T1-2 graphite epoxy composite
11. High velocity perforation behaviour of polymer composite laminates
12. Impact damage resistance of graphite/epoxy laminated composites