Effect of area ratio on base pressure in a suddenly expanded duct for under expanded flow ft mach 1.87

QR Code

Effect of area ratio on base pressure in a suddenly expanded duct for under expanded flow ft mach 1.87

The results of an experimental investigation carried out to control the base pressure in a suddenly expanded axi-symmetric passage is presented in this paper. An active control in the form of micro jets is employed to control the base pressure. Air injection at four locations at the base, symmetric...

Full description

Bibliographic Details
Main Authors:	Baig, Maugal Ahmed Ali, Khan, Sher Afghan, Khan, Mohammad Yunus
Format:	Article
Language:	English
Published:	2012
Subjects:	TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/49922/ http://irep.iium.edu.my/49922/1/baig_m_a_-_2012_-_IJMIE_Journal_Effect_of_Area_Ratio_on_Base_P.pdf

Similar Items

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

Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers
by: Pathan, Khizer Ahmed, et al.
Published: (2018)

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

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

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

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

Prediction of base pressure in a suddenly expanded flow the processes at supersonic Mach Number Regimes using ANN and CFD
by: Quadros, Jaimon Dennis, et al.
Published: (2020)

Control of suddenly expanded flows with micro-jets
by: Khan, Sher Afghan, et al.
Published: (2003)

Base pressure studies from over expanded nozzle for area ratio 2.56
by: Baig, Maughal Ahmed Al, et al.
Published: (2012)

Investigation of base pressure variations in internal and external suddenly expanded flows using CFD analysis
by: Pathan, Khizer Ahmed, et al.
Published: (2019)

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 investigations on wall pressure in suddenly enlarged ducts at supersonic Mach number regimes
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)

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)

Influence of micro jets on the flow development in the enlarged duct at supersonic Mach number
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)

Base pressure control by supersonic micro jets in a suddenly expanded nozzle
by: Khan, Sher Afghan, 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)

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

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

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

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

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

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

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

Effect of mach number on stiffness and damping derivatives for oscillating hyersonic non-planar wedge
by: Crasta, Asha, et al.
Published: (2014)

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

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

CFD analysis of the supersonic nozzle flow with sudden expansion
by: Ahmed, Khizar Pathan, et al.
Published: (2016)

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)

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

Analytical estimation of stability derivatives of wing with curved leading edges at hypersonic mach number
by: Renita, sharon Monis, et al.
Published: (2020)

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

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 wall pressure flow control by micro jets for high area ratio
by: Ashfaq, Syed, et al.
Published: (2014)

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)

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

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

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