Nozzle expansion level effect on a suddenly expanded flow

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Nozzle expansion level effect on a suddenly expanded flow

This investigation focuses attention on the effectiveness of active control in the form of micro-jets, located at the base region of a suddenly expanded axi-symmetric ducts, to control the base pressure. The experiments were conducted for Mach numbers 1.25, 1.3, 1.48, 1.6, 1.8, 2.0, 2.5, and 3.0 at...

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Bibliographic Details
Main Authors:	Khan, Sher Afghan, Rathakrishnan, E.
Format:	Article
Language:	English
Published:	Walter de Gruyter 2006
Subjects:	TL Motor vehicles. Aeronautics. Astronautics TL780 Rockets
Online Access:	http://irep.iium.edu.my/46701/ http://irep.iium.edu.my/46701/1/khan_s_a_-_2006_-_nozzle_expansion.pdf

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