Active control of base pressure in supersonic regime

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Active control of base pressure in supersonic regime

This paper presents an experimental investigation to study the effectiveness of micro jets to control base pressure in suddenly expanded axi-symmetric ducts. Four micro jets of 1-mm orifice dia located at 90° intervals along a pitch circle dia of 1.3 times the nozzle exit dia in the base region are...

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Bibliographic Details
Main Authors:	Khan, Sher Afghan, Rathakrishnan, E.
Format:	Article
Language:	English
Published:	Institution of Engineers, India 2006
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/46703/ http://irep.iium.edu.my/46703/1/AS_151.pdf

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