Shock-Physics, Compressible Flows and Directed Energy Systems

Kostas KontisCraig White

The vision is to create integrated process understanding by conducting numerical and experimental studies looking at shock-physics and compressible phenomena associated with interactions of platform technologies, spanning air and space, through challenging environments.

The research theme progresses technologies enabling the survival and operation of systems through a range of terrestrial, near-Earth space, planetary surface, and subsurface conditions and supports the sustainability of aerospace missions. It is dedicated to supporting industries in developing their businesses and generating high-value jobs, income, and impact on the local and national economy.

Our methodologies are adopted worldwide in academia and industry. Typical funders include Rolls-Royce plc, ESA/ESTEC, DSTL-MoD, US Air Force, Airbus Operation Ltd, and others.

Research topics are shown below:

  • Jets in high-speed crossflow: Transverse injection into supersonic/hypersonic cross flow is encountered in Scramjet combustors, thrust vector control systems, reaction control jets, etc. The effects of Re/m, type of injectant gas, roughness, location of injection and location of an impinging shock are investigated

  • Directed energy deposition systems using ns-DBD, Lasers and microwaves 

  • Shock Wave Boundary Layer Interactions  

  • Scramjet intakes, compression surfaces and cavities

  • Flow control at high speeds

  • Shock diffraction phenomena and Richtmyer-Meshkov Instabilities.

Our partners

Rolls-Royce plc, ESA/ESTEC, DSTL-MoD, US Air Force, Airbus