Control of CD nozzle flow using microjets at Mach 2.1
This paper reports the outcome of the wind tunnel investigation performed to study the effectiveness of the control jets to regulate the base pressure in an abruptly expanded circular pipe. Tiny jets four in a number, of 1 mm orifice diameter located at ninety degrees in cross shape along a pitch ci...
Main Authors: | Akhtar, Mohammad Nishat, Abu Bakar, Elmi, Aabid, Abdul, Khan, Sher Afghan |
---|---|
Format: | Article |
Language: | English English |
Published: |
Blue Eyes Intelligence Engineering & Sciences
2019
|
Subjects: | |
Online Access: | http://irep.iium.edu.my/74734/ http://irep.iium.edu.my/74734/ http://irep.iium.edu.my/74734/ http://irep.iium.edu.my/74734/1/74734_Control%20of%20CD%20Nozzle%20Flow.pdf http://irep.iium.edu.my/74734/7/74734_Control%20of%20CD%20nozzle%20flow%20using%20microjets%20at%20mach%202.1_Scopus.pdf |
Similar Items
-
Control of nozzle flow using microjets at supersonic Mach Regime
by: G M, Fharukh, et al.
Published: (2019) -
Experiment on of nozzle flow with sudden expansion at Mach 1.1
by: Faheem, Mohammad, et al.
Published: (2019) -
Numerical simulations of a CD nozzle and the influence of the duct length
by: Akhtar, Mohammad Nishat, et al.
Published: (2019) -
Active control of flow through the nozzles at sonic Mach number
by: Ashfaq, Syed, et al.
Published: (2013) -
Effect on base pressure in suddenly expanded flows with variable location of microjets
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)