Performance analysis of a scramjet inlet-isolator using experimental & numerical methods

Che-Idris, A., Saad, M.R., Zare-Behtash, H. and Kontis, K. (2012) Performance analysis of a scramjet inlet-isolator using experimental & numerical methods. In: 28th Congress of the International Council of the Aeronautical Sciences, Brisbane, Australia, 23-28 Sep,

Full text not currently available from Enlighten.

Publisher's URL: http://www.icas.org/ICAS_ARCHIVE/ICAS2012/ABSTRACTS/913.HTM

Abstract

The effects of variable geometry inlet on its performance were studied extensively. Experimental methods involved are Pressure Sensitive Paint, Particle Image Velocimetry, Colour Schlieren, oil flow and many other standard methods. Results show how flow structures inside inlet-isolator could determine its performance.

Item Type:Conference Proceedings
Status:Published
Refereed:Yes
Glasgow Author(s) Enlighten ID:Kontis, Professor Konstantinos and Zare-Behtash, Dr Hossein
Authors: Che-Idris, A., Saad, M.R., Zare-Behtash, H., and Kontis, K.
College/School:College of Science and Engineering > School of Engineering > Aerospace Sciences

University Staff: Request a correction | Enlighten Editors: Update this record