Job Opportunities in United Kingdom

The role

We are seeking a motivated interdisciplinary researcher to join the University of Bristol, as part of the Airbus led Aerospace Technology Institute / IUK funded DAWS2 project. The work involves the prediction of Limit Cycle Oscillations (LCOs) for preparation for wind tunnel / flight tests of aircraft wings incorporating a semi-aeroelastic hinge (SAH). CFD tools coupled with FE structural models will be developed to predict LCOs on highly flexible wings incorporating the SAH.
As part of the role, it would be expected that the candidate works closely with Airbus and other partners in the DAWS2 project, making regular presentations, writing progress reports and completing project deliverables. The successful candidate will be part of a team of researchers working on different aspects of the DAWS2 project.
DAWS2 (Development of Advanced Wing Solutions) will focus on the development of Ultra Efficient technologies to cut fuel burn and weight, independent of the fuel choice, for a new high build rate product using wing span as a key enabler.

What will you be doing?

You should apply if

• A 1st class degree in Aerospace or Mechanical Engineering (or related subject).
• Experience of unsteady numerical aeroelastic modelling of aircraft wings using high fidelity methods (e.g. CFD and FE).
• Experience in the analysis and interpretation of data sets, including search and optimisation.
• Excellent oral and written communication skills.
• Proactive self-starter able to define & produce new processes & procedures.
• Inquisitive nature with an interest & skills in problem-solving.

For informal enquiries please contact: Prof Ann Gaitonde ann.gaitonde@bristol.ac.uk

Additional information

Contract type: Open ended (Fixed term funding until 31/5/2026)
Work pattern: Full time
Grade: I / J
Salary: Grade I £37,999 – £43,878 per annum; Grade J £42,632 - £47,874 per annum
School/Unit: School of Civil, Aerospace and Design Engineering
This advert will close at 23:59 UK time on 4/11/2024

Our strategy and mission

Available documents

• ACAD107770 - RA8 CFD Limit Cycle Characterization for High Aspect Ratio Wings with Semi Aeroelastic Hinge - JD.docx