Active control of wall pressure flow field at low supersonic Mach numbers

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Active control of wall pressure flow field at low supersonic Mach numbers

This paper presents an experimental study of airflow from convergent-divergent nozzles discharged into enlarged duct, focusing attention on the flow development in the duct. To investigate the influence of active control on the flow field developed in the duct, the micro jets of 0.05 mm radius orifi...

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Bibliographic Details
Main Authors:	Asad Ullah, Mohammed, Bashir, Musavir, Janvekar, Ayub, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	International Organization of Scientific Research ( IOSR ) 2016
Subjects:	TL780 Rockets
Online Access:	http://irep.iium.edu.my/54286/ http://irep.iium.edu.my/54286/1/Asadullah.pdf

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