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Solid Mechanics & Materials Engineering Group

Current Research Projects of Prof. David Nowell

Prof. David Nowell

Fretting Fatigue and Fretting Wear


Fretting fatigue occurs when contacting surfaces are subjected to oscillating loading and can be responsible for premature failure in components such as spline joints, bolted and rivetted connections and dovetail joints between aircraft engine blades and discs. Research in this area has been taking place in Oxford for a number of years and we have four dedicated rigs for experiments on fretting fatigue and fretting wear. Recent work in this area included participation in a joint EPSRC project with the University of Nottingham, which developed improved life prediction methods by combining models of the fretting wear and fretting fatigue processes.  A number of smaller experimental projects are also being carried out, including work on fretting fatigue of composites (Rolls-Royce), and high temperature fretting (Rolls-Royce/TSB). Research student Rodolfo Fleury started in 2011 and is looking at fretting fatigue problems involving single crystal materials.


People
Prof. D. Nowell, Prof. D. A. Hills, R.J. Paynter, R. Fleury
Sponsor
Rolls-Royce plc, Technology Strategy Board (SILoET) programme)
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Friction

Work on fretting has led to a more fundamental interest in the origins and modelling of frictional behaviour.  An EPSRC project is being carried out with Imperial College, aimed at developing a more predictive approach to the incorporation of friction in larger scale models, e.g. for the prediction of vibration or structural integrity.  The initial phase of the work focussed on developing a robust method of measuring interface response which is largely independent of macroscopic geometry.  More recent work has examined the pressure dependence of tangential stiffness and fundamental modelling of asperity interaction.

People
Prof. D. Nowell, Prof. D. A. Hills, D. Mulvihill
Sponsor
EPSRC, Rolls-Royce plc,
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Modelling and Prediction of Residual Stress

David Nowell has been involved in a number of projects involving the prediction and measurement of residual stress and/or the consequences of such stress fields for structural integrity.  An EPSRC project with the University of Bristol developed analytical tools for use with the deep hole drilling method of residual stress measurement.  Another project, funded by Rolls-Royce and the DTI, involved the modelling of residual stress fields induced by the inertia welding process.  The approach adopted employed a distribution on misfit strains (eigenstrains) to capture the fundamental deformation induced by the process.  An EPSRC project is now underway in collaboration with the Universities of Manchester and Swansea which will generate improved understanding of the Laser Shock Peening process, used to induce compressive surface residual stress.  Research at Oxford is building on the earlier eigenstrain work in order to develop a robust and validated model of the peening process
 
People
Prof. D. Nowell, Prof. F.P.E. Dunne, Dr M. Achintha
Sponsor
 EPSRC, Rolls-Royce plc

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Singularities and Stress Analysis

David Nowell's work on contact mechanics has led to an interest in other problems involving stress singularities.  Most recently, he was involved in the European ‘LITEBUS’ project, where Oxford was responsible for developing strategies for adhesive joining of components in a lightweight composite bus structure.  Angelos Mintzas made considerable progress in developing the use of generalised stress intensity factors as a failure criterion in adhesive joints.

People
Prof. D. Nowell, Prof. R.D. Adams,
Sponsor

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Plasticity-induced Fatigue Crack Closure


David Nowell has a wide interest in the field of fatigue and has undertaken a number of projects in this area.  Recent work has included a combined experimental and modelling investigation of plasticity induced fatigue crack closure.  This has relevance to the prediction of propagation behaviour of cracks under non-uniform loading conditions.  The experimental side of the work has developed image correlation techniques as a practical tool for measurement of fatigue crack closure.

People
 Prof. D. Nowell
Sponsor

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Foreign Object Damage


Foreign object damage occurs when small hard objects such as stones are ingested by aircraft engines. In many cases the resulting damage causes a significant reduction in the fatigue life of the blade. Experiments have been carried out using the high speed gas guns at Oxford to introduce representative damage to the leading edges of blades. Modelling work has also been carried out using the DYNA finite element package and a damage parameter based material model. We have proposed a methodology for the prediction of residual fatigue life based on short crack arrest. Work carried out under a European project (RAMGT) involved the extension of the method to cope with damaged blades subject to combined cycle fatigue loading.  Experimental test work is also carried out for a number of customers.

People
 Prof. D. Nowell, Dr C. Siviour
Sponsor
Rolls-Royce plc