Passive control of base pressure with static cylinder at supersonic flow

An experimental investigation for over expanded, perfectly expanded and under expanded supersonic jets is presented to study the effectiveness of a static cylinder to reduce base drag at Mach 2 through a converging diverging nozzle for a cross-sectional duct nozzle area ratio of 9. A static cylinder...

詳細記述

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書誌詳細
主要な著者: Asadullah, Mohammed, Khan, Sher Afghan, Asrar, Waqar, Sulaeman, Erwin
フォーマット: Conference or Workshop Item
言語:English
English
出版事項: Institute of Physics Publishing 2018
主題:
オンライン・アクセス:http://irep.iium.edu.my/65383/1/65383_Passive%20control%20of%20base%20pressure.pdf
http://irep.iium.edu.my/65383/2/65383_Passive%20control%20of%20base%20pressure_SCOPUS.pdf
http://irep.iium.edu.my/65383/
http://iopscience.iop.org/article/10.1088/1757-899X/370/1/012050
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