Base pressure control and temperature distribution along the duct at supersonic Mach number: a comprehensive CFD approach - Part 1
Sudden expansion is widespread in industry and at the base of rockets and missiles. Managing base pressure in supersonic flows is crucial for reducing drag and enhancing the performance of high-speed vehicles, such as missiles and rockets. This study investigates the use of quarter-circular ribs to...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | en |
| Published: |
Pushpa Publishing House, India
2025
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/122854/1/122854_Base%20pressure%20control.pdf http://irep.iium.edu.my/122854/ https://pphmjopenaccess.com/aafm/article/view/3552 |
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