An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle

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An investigation of base flow control by wall pressure analysis in a suddenly expansion nozzle

This paper presents the results of an experimental investigation conducted at supersonic Mach number of 1.25 through a converging–diverging nozzle for diameter-ratio of 1.6. The experiments were conducted at different level of expansion viz. for correctly expanded and under expanded cases and, for...

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Bibliographic Details
Main Authors:	Khan, Sher Afghan, Bashir, Musavir, G M, Fharukh Ahmed, Ullah, M. Asad
Format:	Article
Language:	English
Published:	UNIV LAGOS 2016
Subjects:	TL787 Astronautics
Online Access:	http://irep.iium.edu.my/51373/ http://irep.iium.edu.my/51373/1/our_paper.pdf

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