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Details of Grant 

EPSRC Reference: GR/J56882/01
Title: PREDICTION OF DAMAGE INITIATION AND GROWTH IN COMPOSITE MATERIALS: MICROMECHANICAL MODELLING PHASE II
Principal Investigator: Wisnom, Professor M
Other Investigators:
Researcher Co-Investigators:
Project Partners:
BAE Systems Hexcel Composites Ltd National Physical Laboratory NPL
Pre Nexus Migration QinetiQ Rolls-Royce Plc (UK)
Department: Aerospace Engineering
Organisation: University of Bristol
Scheme: LINK
Starts: 01 June 1994 Ends: 31 March 1996 Value (£): 66,248
EPSRC Research Topic Classifications:
Materials Characterisation
EPSRC Industrial Sector Classifications:
Aerospace, Defence and Marine Manufacturing
Related Grants:
Panel History:  
Summary on Grant Application Form
Micromechanical finite element models will be developed to predict the behaviour of cross-ply, angle-ply and quasi-isotropic laminates containing damage under tension loading. Modelling of delamination will also be undertaken, using a simple ply drop-off configuration. The applicability of the models to design features will be assessed by attempting to model progression of damage in the region of a hole in a cross-ply laminate. The models will be validated against experimental data generated by other members of the LINK consortium. Parametric studies will be undertaken to understand the main parameters affecting behaviour. The finite element models will also be used to determine the range of validity of analytical models being developed as part of the LINK programme.
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Further Information:  
Organisation Website: http://www.bris.ac.uk