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:
Online Access:http://irep.iium.edu.my/51373/1/our_paper.pdf
http://irep.iium.edu.my/51373/
http://jsrad.org/wp-content/2016/Issue%205,%202016/1j.pdf
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