Effect of mach number on wall pressure flow field for area ratio 2.56

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Effect of mach number on wall pressure flow field for area ratio 2.56

This paper presents the experimental results on the flow characteristics of a suddenly expanded flow from the convergent nozzle for subsonic flow. In the present study micro jets were used to investigate the effect of micro jets on wall pressure flow field in the enlarged duct. Accordingly an active...

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Bibliographic Details
Main Authors:	Ashfaq, Syed, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	International Organozation of Scientific Research (IOSR) Journals 2014
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/49919/ http://irep.iium.edu.my/49919/1/2014_MARCH_APRIL_IOSR_JMCE.pdf

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