Effect of level of expansion and inertia level in a suddenly expanded flow

QR Code

Effect of level of expansion and inertia level in a suddenly expanded flow

An experimental study has been carried out to assess the effectiveness of the active control in the form of micro jets to control the base pressure in a suddenly expanded axi-symmetric duct. Four micro jets of 1mm orifice diameter located at 90 intervals along a pitch circle diameter of 1.3 times t...

Full description

Bibliographic Details
Main Authors:	Chaudhary, Zakir Ilahi, Shinde, V.B, Ashfaq, Syed, Khan, Sher Afghan
Format:	Proceeding Paper
Language:	English
Published:	2015
Subjects:	TL500 Aeronautics TL780 Rockets TL787 Astronautics
Online Access:	http://irep.iium.edu.my/46657/ http://irep.iium.edu.my/46657/1/46657.pdf

Similar Items

Combined effect of relief and level of expansion in a suddenly expanded flow
by: Syed, Syed Ashfaq, et al.
Published: (2015)

Experimental study of suddenly expanded flow from correctly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2016)

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

Investigation of base flow for an axisymmetric suddenly expanded nozzle with micro JET
by: Chaudhary, Zakir Ilahi, et al.
Published: (2018)

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)

Effect of sudden expansion for varied area ratios at subsonic and sonic flow regimes
by: Sethuraman, Vigneshvaran, et al.
Published: (2016)

Effectiveness of micro-jets at different level of expansion
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)

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

Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow
by: Khan, Sher Afghan
Published: (2015)

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

Analysis of parameters affecting thrust and base pressure in suddenly expanded flow from nozzle
by: Pathan, Khizar Ahmed, et al.
Published: (2019)

Enlarge duct length optimization for suddenly expanded flows
by: Pathan, Khizer Ahmed, et al.
Published: (2020)

Experimental studies of the base flow from the nozzles with sudden expansion with micro jets
by: Chaudhary, Zakir Ilahi, et al.
Published: (2016)

Base and wall pressure control using cavities and ribs in suddenly expanded flows -an overview
by: Sethuraman, Vigneshvaran, et al.
Published: (2020)

Active control of base pressure in suddenly expanded flow for area ratio 4.84
by: Ali Baig, Maughal Ahmed, et al.
Published: (2012)

Influence of expansion level on base pressure and reattachment length
by: Pathan, Khizar Ahmed, et al.
Published: (2019)

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

Effect of nozzle pressure ratio and control jets location to control base pressure in suddenly expanded flows
by: Pathan, Khizer Ahmed, 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)

An investigation of effect of control jets location and blowing pressure ratio to control base pressure in suddenly expanded flows
by: Pathan, Khizar Ahmed, et al.
Published: (2020)

A cost-effective data acquisition instrumentation for measurement of base pressure and wall pressure in suddenly expanded flow through ducts
by: Sethuraman, Vigneshvaran, et al.
Published: (2019)

Base pressure behaviour in a suddenly expanded duct at supersonic mach number regimes using Taguchi design of experiments
by: Quadros, Jaimon Dennis, 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)

Influence of control mechanism on the flow field of duct at Mach 1.2 for area ratio 2.56
by: Khan, Sher Afghan, 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)

Study of effect of flow parameters on base pressure in a suddenly expanded duct at supersonic mach number regimes using CFD and design of experiments
by: Quadros, Jaimon Dennis, et al.
Published: (2018)

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

Wall Pressure Measurements Beneath the Supersonic Jets in an Abruptly Augmented Nozzle
by: Bashir, Musavir, et al.
Published: (2020)

Experimental research of wall pressure distribution and effect of micro jet at Mach 1.5
by: Azami, Muhammad Hanafi, et al.
Published: (2019)

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

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 flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25
by: Ashfaq, Syed, et al.
Published: (2014)

Influence of micro jets on wall pressure for area ratio 3.24
by: Ashfaq, Syed, et al.
Published: (2014)

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

Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges
by: Crasta, Asha, et al.
Published: (2015)

Comparative analysis of alternative fuels in detonation combustion
by: Azami, Muhammad Hanafi, et al.
Published: (2016)

Effect on base pressure in suddenly expanded flows with variable location of microjets
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)

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

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