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Control of CD nozzle flow using microjets at Mach 2.1

Control of CD nozzle flow using microjets at Mach 2.1

This paper reports the outcome of the wind tunnel investigation performed to study the effectiveness of the control jets to regulate the base pressure in an abruptly expanded circular pipe. Tiny jets four in a number, of 1 mm orifice diameter located at ninety degrees in cross shape along a pitch ci...

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Bibliographic Details
Main Authors: Akhtar, Mohammad Nishat, Abu Bakar, Elmi, Aabid, Abdul, Khan, Sher Afghan
Format: Article
Language:English
English
Published: Blue Eyes Intelligence Engineering & Sciences 2019
Subjects:
TL Motor vehicles. Aeronautics. Astronautics
Online Access:http://irep.iium.edu.my/74734/
http://irep.iium.edu.my/74734/
http://irep.iium.edu.my/74734/
http://irep.iium.edu.my/74734/1/74734_Control%20of%20CD%20Nozzle%20Flow.pdf
http://irep.iium.edu.my/74734/7/74734_Control%20of%20CD%20nozzle%20flow%20using%20microjets%20at%20mach%202.1_Scopus.pdf
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http://irep.iium.edu.my/74734/
http://irep.iium.edu.my/74734/
http://irep.iium.edu.my/74734/
http://irep.iium.edu.my/74734/1/74734_Control%20of%20CD%20Nozzle%20Flow.pdf
http://irep.iium.edu.my/74734/7/74734_Control%20of%20CD%20nozzle%20flow%20using%20microjets%20at%20mach%202.1_Scopus.pdf

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