Passive control of base pressure with static cylinder at supersonic flow
An experimental investigation for over expanded, perfectly expanded and under expanded supersonic jets is presented to study the effectiveness of a static cylinder to reduce base drag at Mach 2 through a converging diverging nozzle for a cross-sectional duct nozzle area ratio of 9. A static cylinder...
| Main Authors: | , , , |
|---|---|
| Format: | Conference or Workshop Item |
| Language: | English English |
| Published: |
Institute of Physics Publishing
2018
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/65383/ http://irep.iium.edu.my/65383/ http://irep.iium.edu.my/65383/ http://irep.iium.edu.my/65383/1/65383_Passive%20control%20of%20base%20pressure.pdf http://irep.iium.edu.my/65383/2/65383_Passive%20control%20of%20base%20pressure_SCOPUS.pdf |