Micro-Ramps for Hypersonic Flow Control

Shock/boundary layer interaction (SBLI) is an undesirable phenomenon, occurring in high-speed propulsion systems. The conventional method to manipulate and control SBLI is using a bleed system that involves the removal of a certain amount of mass of the inlet flow to control boundary layer separatio...

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Bibliographic Details
Main Authors: Konstantinos Kontis, Azam Che-Idris, Hossein Zare-Behtash, Mohd R. Saad
Format: Article
Language:English
Published: MDPI AG 2012-04-01
Series:Micromachines
Subjects:
Online Access:http://www.mdpi.com/2072-666X/3/2/364