Enhancing Scramjet Performance By Boundary Layer Combustion (2006–2008)

Abstract:
We aim to reduce the aerodynamic drag of high-speed flight vehicles. A major impediment to achieving hypersonic flight is the high level of frictional forces that typically account for half the aerodynamic drag of the vehicle. A novel technique for reducing frictional drag has recently been proposed and tested in Australia. Boundary layers are ''
Grant type:
ARC Discovery Projects
Researchers:
  • Professor
    School of Mechanical and Mining Engineering
    Faculty of Engineering, Architecture and Information Technology
Funded by:
Australian Research Council