The prediction of the long-term mechanical behaviour of aeronautical laminates

Composites Science and Technology

Volumn 61, Issue 3, 2001, Pages 439-443

  Gamby, D ^a   Lafarie Frenot, M C ^a   Vinet, A ^b   Guedra Degeorge, D ^b  

^a CNRS   (France)

^b AEROSPATIALE MATRA Centre Commun de Recherches Louis Blériot   (France)

Author keywords

A. Carbon fibres; A. Polymer matrix composites; B. Creep; B. Non linear behaviour; B. Plastic deformation

Indexed keywords

CARBON FIBER REINFORCED PLASTICS; CREEP TESTING; MATHEMATICAL MODELS; VISCOELASTICITY;

AERONAUTICAL LAMINATES;

LAMINATED COMPOSITES;

AEROSPACE TEXTILE; CARBON FIBER; FIBER REINFORCED COMPOSITE; LAMINATE; MECHANICAL PROPERTY;

EID: 0035048676     PISSN: 02663538     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0266-3538(00)00108-1     Document Type: Article

References (8)

1. The nonlinear viscoelastic-viscoplastic behavior of IM7/composites subjected to cyclic loading
2. Nonlinear viscoelastic and viscoplastic constitutive equations based on thermodynamics
3. Viscoelastic characterization of a non linear fiber-reinforced plastic
4. Damage modelling of the elementary ply for laminated composites
5. Three-dimensional, nonlinear viscoelastic analysis of laminated composites
6. Creep and recovery behavior of ultrahigh molecular weight polyethylene in the region of small uniaxial deformations
7. An integral constitutive equation for non-linear plasto-viscoelastic behavior of high density polyethylene