Postgrad LIVE! Study Fairs

Birmingham | Edinburgh | Liverpool | Sheffield | Southampton | Bristol

University of Birmingham Featured PhD Programmes
University of Oxford Featured PhD Programmes
Coventry University Featured PhD Programmes
Swansea University Featured PhD Programmes
Birkbeck, University of London Featured PhD Programmes
"aeroelastic"×
10 miles

aeroelastic PhD Projects, Programs & Scholarships

We have 5 aeroelastic PhD Projects, Programs & Scholarships

  • "aeroelastic" ×
  • clear all
Order by 
Showing 1 to 5 of 5
  Quasi-3D beam models for the nonlinear aeroelastic response of metallic and composite structures
  Dr F Fazzolari, Dr S Fichera
Application Deadline: 10 August 2019
This PhD project will focus on developing a quasi-3D beam models tailored to nonlinear aeroelastic systems that will be coupled to the aeroelastic suite of Nastran for extending its aeroelastic capabilities.
  PhD Studentship: Development of an aeroelastic multi-disciplinary design optimization framework for large wind turbine systems
  Dr T Kim
Application Deadline: 28 January 2019
Reference number. WS23. Start date of studentship. 01 October 2019. Closing date of advert. 28TH January 2019. Interview date. TBC.
  Topology optimisation for nonlinear aeroelasticity
  Dr P Dunning, Dr A Maheri
Applications accepted all year round
The aim of the is project is to develop an efficient nonlinear aeroelastic topology optimisation method and apply it to design novel, high performing aeroelastic structures, such as wings and wind turbine blades.
  PhD Studentship: Understanding aeroelastic dynamics for aeroelastically tailored smart turbine blades
  Dr T Kim
Application Deadline: 28 January 2019
Reference number. WS22. Start date of studentship. 01 October 2019. Closing date of advert. 28th January 2019. Interview date. TBC.
  Hierarchical Optimization Approach to Detail Design of an Aircraft Wing
  Dr Alicia Kim
Application Deadline: 31 December 2018
This project will develop a hierarchical methodology to optimize an aircraft wing design. A unique novelty of the methodology that will be developed is that it will simultaneously optimize the overall wing mass and stiffness distribution as a subsystem and the detailed stiffener and skin components in a coupled way.
Show 10 15 30 per page
  • 1


FindAPhD. Copyright 2005-2018
All rights reserved.