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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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書誌詳細
主要な著者:	Aabid, Abdul, Khan, Sher Afghan
フォーマット:	論文
言語:	English English
出版事項:	Elsevier Ltd Kidlington Corporate Office, Kidlington, United Kingdom 2020
主題:	TL Motor vehicles. Aeronautics. Astronautics
オンライン･アクセス:	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 http://irep.iium.edu.my/81933/ http://www.elsevier.com/locate/matpr https://doi.org/10.1016/j.matpr.2020.06.538
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