Experimental studies on low speed converging nozzle flow with sudden expansion

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Experimental studies on low speed converging nozzle flow with sudden expansion

This paper presents the results of experimental studies conducted to study the base pressure field from a convergent nozzle to ascertain the effect of micro jets, the length to diameter ratio, Mach number and area ratio in a suddenly expanded flow. The Mach numbers of the present study are 0.2, 0.4,...

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Bibliographic Details
Main Authors:	Ashfaq, Syed, Khan, Sher Afghan
Format:	Article
Language:	English
Published:	International Journal of Emerging Technology and Advanced Engineering (IJETAE) 2014
Subjects:	TL Motor vehicles. Aeronautics. Astronautics TL787 Astronautics
Online Access:	http://irep.iium.edu.my/49898/ http://irep.iium.edu.my/49898/1/2014_JANUARY_IJETAE.pdf

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