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Composite Design, Analysis & Life Prediction

Simple stress analysis of composite laminates may be conducted using classical lamination plate theory (CLPT) or anisotropic elasticity solutions. These methods may be combined with other methods, such as shear deformable plate theory and fracture analysis to determine the performance of laminates and serve as a good first tool. However, once the composite structure becomes more detailed with engineering features, such as holes, cutouts, joints, etc. it is not possible to use closed form solutions and reliance is often placed on finite element analysis.

The modelling of composite laminates using FEA involves additional steps to those for homogeneous materials. For example, the layered and anisotropic nature of the composite needs to be modelled either on a 'layer by layer' basis or using the aforementioned CLPT to determine the composite performance of an element containing several plies. The influence of bend twist couple in a laminate that is not symmetrical about its mid-plane also needs to be modelled. Further the failure of a composite material may included several mechanisms including cracks, delaminations and fibre failure.

Life prediction of composite materials and components requires the influence of combined service conditions on materials properties to be studied as a function of severity and duration. No generalised framework exists that can fully relate laboratory based property data to component life in service. Specific techniques can be used to overcome this shortcoming. For example, the application of probabilistic strength theories can account for orders of magnitude difference in stressed volume between coupons and engineering structures. Residual strength tests can be related to fracture data under appropriately defined conditions. Moisture permeability rates can be used to predict reduction in matrix modulus, porosity or matrix cracks and hence properties for a given material system. The reduction in stiffness from fatigue can be estimated from damage accumulation models. However, such theories cannot be easily applied to real components which experience varying stresses, temperatures and environments and are of a complex shape.

MERL provides an integrated approach to life prediction analysis, studying the mechanism of degradation in the laboratory under accelerated conditions, and then applies these under the defined conditions in service. This work is supported by the appropriate numerical analysis. Equipment exists at MERL for simulated service environments in the following areas:

  • Offshore oil & gas
  • Aerospace
  • Automotive
  • Marine
  • Renewable energies
  • Medical applications
  • Chemical processing

MERL staff have experience in both closed form solutions and finite element analysis including:
  • Closed form stress analysis of anisotropic and laminated plates
  • Finite element analysis (ABAQUS is MERL’s codes of choice)
  • Fatigue and fracture analysis (including development of automated modelling to facilitate fracture analysis) and crack path
  • Durability, delamination, crack growth assessment
  • Life prediction analysis
  • Design evaluation analysis

FEA contour plots of a DCB test coupon and a composite laminate bearing
 
 

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Materials Engineering Research Laboratory Limited is Wilbury Way,
Hitchin, Hertfordshire, UK, SG4 0TW.
Registered in England. Company registration number: 2015020.

Tel: +44(0)1462 427 850
Polymer Engineering, Testing, Inspection, Research and Development, UK