Control of suddenly expanded flow with cavity at sonic Mach number
Airflow from a convergent nozzle at sonic Mach number expanded suddenly into a circular duct of larger cross-sectional area, provided with annular rectangular cavities, which was studied numerically, focusing attention on the base pressure, and the flow development in the enlarged duct. It was found...
Saved in:
| Main Authors: | , , |
|---|---|
| Other Authors: | |
| Format: | Book Chapter |
| Language: | English English |
| Published: |
Springer
2024
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/111346/6/49d0aee4-661b-4019-9579-d1f692033d79%20%281%29.pdf http://irep.iium.edu.my/111346/1/Ikhwan%20Paper.pdf http://irep.iium.edu.my/111346/ https://link.springer.com/bookseries/11693. |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|