Active control of flow through the nozzles at sonic Mach number

QR Code

Active control of flow through the nozzles at sonic Mach number

The effectiveness of micro jets to control the base pressure in suddenly expanded axi-symmetric ducts are studied experimentally. As an active control in the form of four micro jets of 1 mm orifice diameter located at 900 intervals along a pitch circle diameter of 1.3 times the nozzle exit diameter...

Full description

Bibliographic Details
Main Authors:	Ashfaq, Syed, Khan, Sher Afghan, Rathakrishnan, Ethirajan
Format:	Article
Language:	English
Published:	RS Publication 2013
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://irep.iium.edu.my/49837/ http://irep.iium.edu.my/49837/1/SONIC_IJETED_15412253_ASHFAQ.pdf

Similar Items

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

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

Control of CD nozzle flow using microjets at Mach 2.1
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)

Control of nozzle flow using microjets at supersonic Mach Regime
by: G M, Fharukh, et al.
Published: (2019)

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

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)

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

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

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)

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

Studies on wall pressure of sonic flow through the converging nozzles for different area ratios
by: Ashfaq, Syed, et al.
Published: (2014)

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

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)

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

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)

Effect of mach number on wall pressure flow field for area ratio 2.56
by: Ashfaq, Syed, et al.
Published: (2014)

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)

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

Combined effect of nozzle pressure ratio and screech prone supersonic mach number in a suddenly expanded flow
by: Bashir, Musavir, et al.
Published: (2015)

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

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

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

Studies on suddenly expanded flow at different levels of over expansion for area ratio 3.24
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)

Experimental investigation of flow through convergent nozzle and the influence of micro jets on the enlarged duct flow field
by: Ashfaq, Syed, et al.
Published: (2014)

Sonic Under Expanded Flow Control With Micro Jets
by: Syed, Syed Ashfaq, et al.
Published: (2013)

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 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)

The effect of micro jets on wall pressure for sonic under expanded flow
by: Ashfaq, Syed, et al.
Published: (2014)

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)

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

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

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

Control of suddenly expanded flow from correctly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004)

Active control of suddenly expanded flow from under expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004)

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

Control of base pressure with micro jets for area ratio 2.4
by: Ashfaq, Syed, et al.
Published: (2014)