Control of suddenly expanded flow at low supersonic Mach numbers
In the present study the experiments were conducted to control the base pressure from a convergent-divergent nozzle at low supersonic Mach numbers to assess the effectiveness of active control mechanism in the form of micro jets at different expansion level. The parameters considered in the presen...
| Main Authors: | , , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
IJERA
2015
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/46619/ http://irep.iium.edu.my/46619/ http://irep.iium.edu.my/46619/1/D58052433.pdf |