Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow

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Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow

This paper presents the results of an experimental study to evaluate the effectiveness of the micro jets to control the base pressure in a suddenly expanded flow at supersonic Mach numbers. Four micro jets of 1mm orifice diameter located at 90 intervals along a pitch circle diameter of 1.3 times th...

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Bibliographic Details
Main Authors:	Bashir, Musavir, Khan, Sher Afghan, Rajendran, Parvathy
Format:	Proceeding Paper
Language:	English
Published:	2015
Subjects:	TL500 Aeronautics TL780 Rockets
Online Access:	http://irep.iium.edu.my/46658/ http://irep.iium.edu.my/46658/1/46658.pdf

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