Numerical simulation of suddenly expanded flow at Mach 2.2
A numerical simulation has been performed to investigate the control of base pressure with microjets in a suddenly expanded duct. Microjets placed at the pitch circle diameter (PCD) of 13 mm, two micro jets of 1 mm orifice diameter located at 900 for active control. The flow Mach number of the inves...
| Main Authors: | Aabid, Abdul, Khan, Ambareen, Mazlan, Nur Musfira, Ismail, Mohd Azmi, Akhtar, M. Nishat, Khan, Sher Afghan |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
Blue Eyes Intelligence Engineering & Sciences Publication
2019
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/71060/ http://irep.iium.edu.my/71060/ http://irep.iium.edu.my/71060/1/71060_Numerical%20simulation%20of%20suddenly%20expanded.pdf http://irep.iium.edu.my/71060/2/71060_Numerical%20simulation%20of%20suddenly%20expanded_SCOPUS.pdf |
Similar Items
-
Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers
by: Pathan, Khizer Ahmed, et al.
Published: (2018) -
Effect of mach number in a suddenly expanded flow for area ratio 4.84
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012) -
Control of suddenly expanded flow from correctly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004) -
Control of suddenly expanded flows with micro-jets
by: Khan, Sher Afghan, et al.
Published: (2003) -
Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow
by: Bashir, Musavir, et al.
Published: (2015)