Impact of cavity location on base pressure at Supersonic Mach 1.8
In this day and age, researchers and engineers are actively exploring research in the supersonic Mach number flow field, primarily related to the base pressure of aerospace vehicles and nozzle variants. The boundary layer theory explained the flow separation caused by fluid motion. The turbulent b...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
The Scientific Press
2022
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/97904/7/97904_Impact%20of%20Cavity%20Location%20on%20Base%20Pressure.pdf http://irep.iium.edu.my/97904/ https://jmerd.net/archives/ |
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| Institution: | Universiti Islam Antarabangsa Malaysia |
| Language: | English |