Control of suddenly expanded flow at low supersonic Mach
numbers

Control of suddenly expanded flow at low supersonic Mach numbers

In the present study the experiments were conducted to control the base pressure from a convergent-divergent nozzle at low supersonic Mach numbers to assess the effectiveness of active control mechanism in the form of micro jets at different expansion level. The parameters considered in the presen...

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Bibliographic Details
Main Authors:	Chaudhury, Zakir Ilahi, Shinde, V.B, Syed, Syed Ashfaq, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	IJERA 2015
Subjects:	TJ1040 Machinery exclusive of prime movers
Online Access:	http://irep.iium.edu.my/46619/ http://irep.iium.edu.my/46619/ http://irep.iium.edu.my/46619/1/D58052433.pdf

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