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...
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主要な著者: | , , , |
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フォーマット: | Conference or Workshop Item |
言語: | English English |
出版事項: |
Institute of Physics Publishing
2018
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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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