Control of CD nozzle flow using microjets at Mach 2.1

QR Code

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...

Full description

Bibliographic Details
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:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	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)

Numerical simulations of a CD nozzle and the influence of the duct length
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)

Experiment on of nozzle flow with sudden expansion at Mach 1.1
by: Faheem, Mohammad, et al.
Published: (2019)

Active control of flow through the nozzles at sonic Mach number
by: Ashfaq, Syed, et al.
Published: (2013)

Determination of wall pressure flows at supersonic Mach numbers
by: Aabid, Abdul, et al.
Published: (2020)

Effect on base pressure in suddenly expanded flows with variable location of microjets
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)

Effects of micro jets on the flow field of the duct with sudden expansion
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)

Effect of micro jet control on the flow filed of the duct at Mach 1.5
by: Khan, Sher Afghan, et al.
Published: (2019)

CFD analysis of CD nozzle and effect of nozzle pressure ratio on pressure and velocity for suddenly expanded flows
by: Khan, Sher Afghan, et al.
Published: (2018)

Control of suddenly expanded flows from correctly expanded and under expanded nozzles at supersonic mach number for area ratio 2.56
by: Bashir, Musavir, et al.
Published: (2016)

Experimental studies on low speed converging nozzle flow with sudden expansion
by: Ashfaq, Syed, et al.
Published: (2014)

Studies on flow from convergent nozzle with sudden expansion and control effectiveness under the influence of micro jets
by: Ashfaq, Syed, et al.
Published: (2013)

Effect of mach number in a suddenly expanded flow for area ratio 4.84
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)

Inspection of supersonic flows in a CD nozzle using experimental method
by: Azami, Muhammad Hanafi, et al.
Published: (2019)

Nozzle expansion level effect on a suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2006)

Control of nozzle flow in a suddenly expanded duct with micro jets
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)

Active control of suddenly expanded flows from overexpanded nozzles
by: Khan, Sher, et al.
Published: (2002)

Experimental investigation of the base flow from the nozzles with sudden expansion
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)

Effect of area ratio on base pressure in a suddenly expanded duct for under expanded flow ft mach 1.87
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)

Study of base pressure behavior in a suddenly expanded duct at supersonic mach number regimes using statistical analysis
by: Quadros, Jaimon Dennis, et al.
Published: (2018)

Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method
by: Khan, Sher Afghan, et al.
Published: (2019)

Role of active control in increasing base pressure at Sonic Mach Number
by: G. M, Fharukh Ahmed, et al.
Published: (2019)

Design and fabrication of flying saucer utilizing coanda effect
by: Aabid, Abdul, et al.
Published: (2018)

Research onFlows for NACA 2412 airfoil using computational Fluid dynamics method
by: Kharulaman, Liyana, et al.
Published: (2019)

Experimental investigations on wall pressure in suddenly enlarged ducts at supersonic Mach number regimes
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)

Numerical simulation of suddenly expanded flow at Mach 2.2
by: Aabid, Abdul, et al.
Published: (2019)

Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for Mach 3.0 using CFD
by: Quadros, Jaimon Dennis, et al.
Published: (2016)

Base pressure control using micro-jets in supersonic flow regimes
by: Sethuraman, Vigneshvaran, et al.
Published: (2018)

Investigation of efficacy of low length-to-diameter ratio and nozzle pressure ratio on base pressure in an abruptly expanded flow
by: Ahmed, Fharrukh, et al.
Published: (2018)

Base pressure control by supersonic micro jets in a suddenly expanded nozzle
by: Khan, Sher Afghan, et al.
Published: (2018)

An investigation to control base pressure in suddenly expanded flows
by: Pathan, Khizer Ahmed, et al.
Published: (2018)

Modeling and structural analysis of three-dimensional wing
by: Mohd Zakuan, Muhammad Amir Mirza, et al.
Published: (2019)

CFD analysis of effect of area ratio on suddenly expanded flows
by: Pathan, Khizer Ahmed, et al.
Published: (2017)

CFD studies on triangular micro-vortex generators in flow control
by: Yashodhar, V., et al.
Published: (2017)

Control of suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2006)

Estimation of stability derivatives of a delta wing in hypersonic flow
by: Crasta, Asha, et al.
Published: (2012)

On numerical investigation of semi-empirical relation representing development length for a fluid flow in a closed conduit
by: Mohd Umair, Siddique, et al.
Published: (2019)

Numerical investigation of mathematical non-dimensional constant representing smoothness in the Nusselt profile
by: Ansari, Emad, et al.
Published: (2020)

Influence of micro jets on the flow development in the enlarged duct at supersonic Mach number
by: Khan, Sher Afghan, et al.
Published: (2019)

Wall pressure studies in a suddenly expanded flow for area ratio 2.56”
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)