Computer modelling of impact on curved fibre composite panels

Composite Structures

Volumn 47, Issue 1-4, 1999, Pages 789-796

  Leylek, Zafer ^a   Scott, Murray L ^a   Georgiadis, Steve ^b   Thomson, Rodney S ^c  

^a RMIT UNIVERSITY   (Australia)

^b Aerospace Technologies of Australia Limited   (Australia)

^c Cooperative Research Centre for Advanced Composite Structures Limited ^*  (Australia)

Author keywords

Explicit FE simulation; Impact; Impact damage

Indexed keywords

COMPUTER SIMULATION; EQUATIONS OF MOTION; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; MATRIX ALGEBRA; SHEAR STRESS; STRAIN; STRENGTH OF MATERIALS; STRESS ANALYSIS;

COMPOSITE MESH DENSITY; COMPOSITE PANEL CURVATURE; IMPACT DAMAGE; IMPACTOR WEIGHT; RESIDUAL STRENGTH;

CARBON FIBER REINFORCED PLASTICS;

COMPUTER SIMULATION; FIBER REINFORCED COMPOSITE; IMPACT RESISTANCE; MODEL;

EID: 0033304378     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(00)00055-6     Document Type: Conference Paper

References (7)

1. Effect of curvature on the impact damage characteristics and residual strength of composite plates
2. The influence of varying projectile mass on the impact response of CFRP
3. Non-penetrating impact behavior of CFRP at low and intermediate velocities
4. Crashworthy evaluation of a 1/5-scale model composite fuselage concept
5. Compression response of a sandwich fuselage keel panel with and without damage
6. Impact response of graphite-epoxy cylindrical panels