Control of nozzle flow using microjets at supersonic Mach Regime

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Control of nozzle flow using microjets at supersonic Mach Regime

This article reports the active control of base flows using the experimental procedure. Active control of base pressure helps in reducing the base drag in aerodynamic devices having suddenly expanded flows. Active control in the form of microjets having 0.5 mm radius placed at forty-five degrees apa...

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Bibliographic Details
Main Authors:	G M, Fharukh, Khan, Sher Afghan
Format:	Article
Language:	English English English
Published:	Materials and Energy Research Center 2019
Subjects:	TL Motor vehicles. Aeronautics. Astronautics TL780 Rockets
Online Access:	http://irep.iium.edu.my/73710/ http://irep.iium.edu.my/73710/1/73710_Control%20of%20Nozzle%20Flow%20Using%20Microjets.pdf http://irep.iium.edu.my/73710/2/73710_Control%20of%20Nozzle%20Flow%20Using%20Microjets_SCOPUS.pdf http://irep.iium.edu.my/73710/13/73710_Control%20of%20Nozzle%20Flow%20Using%20Microjets_wos.pdf

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