Experiments on wall pressure at an area ratio 4.84 in a suddenly expanded flow field at supersonic Mach numbers

Experiments on wall pressure at an area ratio 4.84 in a suddenly expanded flow field at supersonic Mach numbers

The present investigation intends to review the flow control mechanism’s effectiveness through a circular orifice of 1 mm diameter generating sonic flow at the exit even though experiments were conducted for various NPRs and a fixed level of expansion. Tests were conducted at Mach 1.87 for correct...

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Bibliographic Details
Main Authors: Khan, Sher Afghan, Chaudhary, Zakir Ilahi, Baig, Maughal Ahmed Ali, Ridwan, R, Chethan, K.M., Faheem, Mohammed
Format: Conference or Workshop Item
Language:English
English
Published: AIP 2022
Subjects:
TL Motor vehicles. Aeronautics. Astronautics
Online Access:http://irep.iium.edu.my/96514/1/96514_Experiments%20on%20wall%20pressure%20at%20an%20area%20ratio%204.84.pdf
http://irep.iium.edu.my/96514/7/96514_Experiments%20on%20wall%20pressure%20_Scopus.pdf
http://irep.iium.edu.my/96514/
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Institution: Universiti Islam Antarabangsa Malaysia
Language: English
English

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http://irep.iium.edu.my/96514/1/96514_Experiments%20on%20wall%20pressure%20at%20an%20area%20ratio%204.84.pdf
http://irep.iium.edu.my/96514/7/96514_Experiments%20on%20wall%20pressure%20_Scopus.pdf
http://irep.iium.edu.my/96514/

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