Experimental research on flow development and control effectiveness in the duct at high speed

QR Code

Experimental research on flow development and control effectiveness in the duct at high speed

This paper presents an experimental study of suddenly expanded flows at supersonic speed is performed. A Convergent-divergent (C-D) nozzle is used with suddenly expanded duct. At the recirculation zone, the pressure is controlled by using four microjets of 1 mm diameter arranged at PCD of 1.3 as an...

Full description

Bibliographic Details
Main Authors:	Khan, Sher Afghan, Ahmad, Zaheer, Aabid, Abdul, Mokashi, Imran
Format:	Article
Language:	English English
Published:	Blue Eyes Intelligence Engineering & Sciences Publication 2019
Subjects:	TL780 Rockets
Online Access:	http://irep.iium.edu.my/74936/ http://irep.iium.edu.my/74936/7/74936%20Experimental%20Research%20on%20Flow%20Development.pdf http://irep.iium.edu.my/74936/13/74936_Experimental%20research%20on%20flow%20development%20and%20control%20effectiveness%20in%20the%20duct%20at%20high%20speed_Scopus.pdf

Similar Items

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 research on wall pressure distribution in C-D nozzle at Mach number 1.1 for area ratio 3.24
by: Khan, Sher Afghan, et al.
Published: (2019)

Enlarge duct length optimization for suddenly expanded flows
by: Pathan, Khizer 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)

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

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 behaviour in a suddenly expanded duct at supersonic mach number regimes using Taguchi design of experiments
by: Quadros, Jaimon Dennis, et al.
Published: (2018)

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)

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

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)

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)

Numerical investigation of splitter plate effect on the bluff body using finite volume method
by: Afifi, Azmil, 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)

Active control of wall pressure flow field at low supersonic Mach numbers
by: Asad Ullah, Mohammed, et al.
Published: (2016)

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)

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

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

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

Influence of micro jets on wall pressure for area ratio 3.24
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)

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

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

Pressure and its derivative with respect to piston Mach number for an oscillating cone
by: Shabana, Ayesha, et al.
Published: (2016)

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

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

Comparing the effect of different turbulence models on the CFD predictions of NACA0018 airfoil aerodynamics
by: Khan, Sher Afghan, et al.
Published: (2020)

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

Control of nozzle flow using microjets at supersonic Mach Regime
by: G M, Fharukh, 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)

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

Control of base pressure with micro jets:part-I
by: Rehman, Shafiqur, et al.
Published: (2008)

The contribution of Hassan al-Rammah to gunpowder and rocket technology
by: Ahmed Ghazal, Belal, et al.
Published: (2011)

Effect of micro jet control on the flow filed of the duct at Mach 1.5
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)

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 level of expansion and inertia level in a suddenly expanded flow
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)

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)

Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges
by: Crasta, Asha, et al.
Published: (2012)