|Funding for:||UK Students, EU Students|
|Funding amount:||£20,000 approximately, per annum - potentially tax free, plus tuition fees and travel allowance|
|Placed On:||27th July 2018|
|Expires:||27th October 2018|
Application Deadline: October 2018
Start Date: October 2018
Eligibility: UK, EU
Duration of award: 4 years
Supervisor: Dr Supriyo Ganguly and Dr Yigeng Xu
Cranfield University and Airbus are seeking a top class candidate to undertake research leading to the award of an International Engineering Doctorate awarded jointly by the Universities of Warwick, Exeter and Cranfield.
The aim of the proposed programme is to understand and quantify benefits of laser peening in improving fatigue life and residual strength of butt jointed aircraft fuselage structures. Laser peening is known to improve the life of a component subjected to dynamic loading through introduction of near surface compressive residual stress state which delays crack initiation and also reduces crack growth rate. Friction stir welding was established as a viable solid state joining process for fuselage structures. However, as any other high temperature joining process, it would introduce tensile residual stress field and also lead to microstructural changes in the wrought alloy which would reduce the strength. Thus the mechanical properties would be adversely affected in such joints and as such an integral structure would have a single load path that would enhance crack initiation and propagation rate. Laser shock peening can be an effective tool to redistribute the stress originated from FSW process and introduce beneficial compressive residual stress state that would enhance integrity of such structure. However, it is important to understand the spatial location of the laser peened area, within the overall joint structure, and the intensity with which the peening process should be performed to maximize the benefit from this process. The effect of laser peening process would be quantified by non-destructive residual stress determination using neutron and synchrotron X-rays to understand the underpinning mechanism of interaction between the compressive stress induced by peening and tensile stress by the welding process. The impact of compressive stress field by laser peening on reducing potential effect crack initiation from weld defects such as lack of penetration would be investigated as well.
This project will investigate the following;
Candidates should have a minimum of an upper second (2.1) honours degree (or equivalent) in Materials Science or Mechanical Engineering.
Qualifying students receive an attractive enhanced stipend which could be tax and NI free depending on your personal circumstances, paid by the Centre and topped up by a contribution from Airbus. For 2018 this totals approximately £20,000 tax free per annum.
The funding is for four years and will also cover University tuition fees and all course fees as well as a travel allowance to attend courses.
How to apply:
To apply please complete our online enquiry form and upload your CV.
For further information please contact:
Type / Role: