Determination of wall pressure flows at supersonic Mach numbers

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Determination of wall pressure flows at supersonic Mach numbers

This article investigates the wall pressure dissemination on a circular duct when the flow is exhausted into a CD nozzle. This study aims at to scrutinize the static pressure on the duct wall and its growth when the control is activated. The microjets are employed at the base at pitch circle radius...

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Bibliographic Details
Main Authors:	Aabid, Abdul, Khan, Sher Afghan
Format:	Article
Language:	English English
Published:	Elsevier Ltd Kidlington Corporate Office, Kidlington, United Kingdom 2020
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://irep.iium.edu.my/81933/ http://irep.iium.edu.my/81933/1/supersonic%20mach%20numbers.pdf http://irep.iium.edu.my/81933/7/81933_Determination%20of%20wall%20pressure%20flows_Scopus.pdf

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