Rolls Royce UTCin Combustion System Aerothermal Processes

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Mark Cassell BEng

Photo of  Mark Cassell

Research Associate

Research Group: 
Applied Aerodynamics

 

Research Interests:
Aero-acoustics, combustion system aerodynamics, acoustic damping, unsteady fluid dynamics

Background

Member of the Rolls-Royce UTC in Combustion System Aerothermal Processes since 2012.

Specialities:

  • Passive damping systems for gas turbine combustors
  • Experimental and numerical study of gas turbine aero-acoustic interactions

Education:

  • BEng(hons) Aeronautical Engineering, Loughborough University, 2012
  • PhD, ‘Development of aerodynamic and acoustic enhanced damping configurations for gas turbine combustion systems’, Loughborough University

Research

Experimental, computational and analytical study of aero-acoustics within modern gas turbines. This includes the development and analysis of acoustic damping devices and unsteady fluid dynamics of fuel systems and injectors.

Publications and Awards

View Publications for Mark Cassell