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Postgraduate research project

Aerodynamic and aeroacoustic effects of rotational, oscillating wing structures

Funding
Fully funded (UK only)
Type of degree
Doctor of Philosophy
Entry requirements
2:1 honours degree View full entry requirements
Faculty graduate school
Faculty of Engineering and Physical Sciences
Closing date

About the project

This project aims to investigate the rotational effects on an oscillating aerodynamic structure, using both experimental and numerical methods. 

Oscillation of aerodynamic structures are widely observed in many engineering applications, such as: 

  • flapping-wing aerial vehicles
  • drone or helicopter propellers
  • wind turbine blade

The aerodynamic and aeroacoustics effects of the unsteady flow conditions caused by the oscillation have been investigated for decades. However, for many rotating applications, understanding the combined effects of the structural rotation and oscillation are limited. Very few experimental results have been published due to the difficulty in designing a test rig.

You'll develop a test rig that can drive an oscillating rotating aerodynamic structure. This will reveal the periodic, transient aerodynamic and aeroacoustic characteristics. The outcome of this project can help improve the understanding to the three-dimensional and unsteady effects on an aerodynamic structure and develop high-performance, low-noise aerodynamic design in real applications. 

As a researcher on this project you'll benefit from:

  • being part of the Acoustic Group at the Institute of Sound and Vibration (ISVR)
  • our modern experimental facilities at the University of Southampton and the high-speed computational resource
  • being involved in an international, interdisciplinary, and motivated research team, with collaborative opportunities with renowned scholars at ISVR

You'll also be encouraged to participate at international academic conferences to present and discuss your research.