Base pressure control and temperature distribution along the duct at supersonic Mach number: a comprehensive CFD approach - part II
The development of space shuttles and high-performance military aircraft has made the study of turbulent flow in separated regions a key area of research. Researchers are also interested in turbulent flow under transonic and supersonic conditions, particularly when it separates suddenly and expands...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | en |
| Published: |
Pushpa Publishing House
2025
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/122897/7/122897_Base%20pressure%20control%20and%20temperature.pdf http://irep.iium.edu.my/122897/ https://pphmjopenaccess.com/aafm/article/view/3753 |
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