A model of a COMAC aircraft

Transonic flutter prediction of aircraft

Investigators

COMAC supervisors and contact details:

Dr Bocheng Zhang (张波成)

Imperial supervisor and contact details:

Prof Rafael Palacios

Researchers:
Dr Bryn Ubald

Project overview

The project will investigate robust computational methods for efficient prediction of aeroelastic instabilities on wings and aircraft operating in the transonic regime.