Influence of control mechanism on the flow field of duct at Mach 1.2 for area ratio 2.56

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Influence of control mechanism on the flow field of duct at Mach 1.2 for area ratio 2.56

In this paper, the outcome of the experimental investigation and the flow field development in the duct at a supersonic Mach number of 1.2 is presented. The experiments were conducted at various NPR which covers the condition of correct expansion and under expansion. A Convergent-divergent (C-D) noz...

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Bibliographic Details
Main Authors:	Khan, Sher Afghan, Aabid, Abdul, Chaudhary, Zakir Ilahi
Format:	Article
Language:	English English
Published:	Blue Eyes Intelligence Engineering & Sciences 2019
Subjects:	TL780 Rockets
Online Access:	http://irep.iium.edu.my/73657/ http://irep.iium.edu.my/73657/1/73657_Influence%20of%20Control%20Mechanism.pdf http://irep.iium.edu.my/73657/7/73657_Influence%20of%20control%20mechanism%20on%20the%20flow%20field%20of%20duct%20at%20mach%201.2%20for%20area%20ratio%202.56_Scopus.pdf

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