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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 ''

Experts

Emeritus Professor David Mee

Emeritus Professor
School of Mechanical and Mining Engineering
Faculty of Engineering, Architecture and Information Technology
David Mee
David Mee