Experimental investigations on wall pressure in suddenly enlarged ducts at supersonic Mach number regimes

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Experimental investigations on wall pressure in suddenly enlarged ducts at supersonic Mach number regimes

This paper presents the results of an experimental work carried out to find the wall pressure distribution in a suddenly enlarged duct. The enlarged duct is attached to the exit of a convergent- divergent axisymmetric nozzle. The area ratio (i.e. ratio between cross sectional arean of the sudden exp...

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Bibliographic Details
Main Authors:	Baig, Maugal Ahmed Ali, Khan, Sher Afghan, Rathakrishnan, E.
Format:	Article
Language:	English
Published:	rspublication 2012
Subjects:	TL Motor vehicles. Aeronautics. Astronautics TL780 Rockets
Online Access:	http://irep.iium.edu.my/49921/ http://irep.iium.edu.my/49921/1/baig_m_a_-_2012_-_experimental_investigations_on_wall_pressure-IJETED.pdf

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