Passive control of base pressure with static cylinder at supersonic flow

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Passive control of base pressure with static cylinder at supersonic flow

An experimental investigation for over expanded, perfectly expanded and under expanded supersonic jets is presented to study the effectiveness of a static cylinder to reduce base drag at Mach 2 through a converging diverging nozzle for a cross-sectional duct nozzle area ratio of 9. A static cylinder...

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Bibliographic Details
Main Authors:	Asadullah, Mohammed, Khan, Sher Afghan, Asrar, Waqar, Sulaeman, Erwin
Format:	Proceeding Paper
Language:	English English
Published:	Institute of Physics Publishing 2018
Subjects:	TJ241 Machine construction (General)
Online Access:	http://irep.iium.edu.my/65383/ http://irep.iium.edu.my/65383/1/65383_Passive%20control%20of%20base%20pressure.pdf http://irep.iium.edu.my/65383/2/65383_Passive%20control%20of%20base%20pressure_SCOPUS.pdf

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