Influence of control mechanism on the flow field of duct at Mach 1.2 for area ratio 2.56
In this paper, the outcome of the experimental investigation and the flow field development in the duct at a supersonic Mach number of 1.2 is presented. The experiments were conducted at various NPR which covers the condition of correct expansion and under expansion. A Convergent-divergent (C-D) noz...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English English |
| Published: |
Blue Eyes Intelligence Engineering & Sciences
2019
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/73657/ http://irep.iium.edu.my/73657/ http://irep.iium.edu.my/73657/ http://irep.iium.edu.my/73657/1/73657_Influence%20of%20Control%20Mechanism.pdf http://irep.iium.edu.my/73657/7/73657_Influence%20of%20control%20mechanism%20on%20the%20flow%20field%20of%20duct%20at%20mach%201.2%20for%20area%20ratio%202.56_Scopus.pdf |
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http://irep.iium.edu.my/73657/1/73657_Influence%20of%20Control%20Mechanism.pdf
http://irep.iium.edu.my/73657/7/73657_Influence%20of%20control%20mechanism%20on%20the%20flow%20field%20of%20duct%20at%20mach%201.2%20for%20area%20ratio%202.56_Scopus.pdf