Analysis of area ratio in a CD nozzle with suddenly expanded
duct using CFD method

QR Code

Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method

Whereas the demand for missiles and rockets has exponentially augmented, but the difficulties related to the gas dynamics of these vehicles remains to be a threat. Whenever there is a sudden expansion, the pressure in the downstream is subatmospheric. This low pressure in the recirculation zone lea...

Full description

Bibliographic Details
Main Authors:	Khan, Sher Afghan, Aabid, Abdul, Ghasi, Fharukh Ahmed Mehaboobali, Al-Robaian, Abdulrahman, Alsagri, Ali Sulaiman
Format:	Article
Language:	English English
Published:	Penerbit Akademia Baru 2019
Subjects:	TL Motor vehicles. Aeronautics. Astronautics U Military Science (General)
Online Access:	http://irep.iium.edu.my/72294/ http://irep.iium.edu.my/72294/1/72294_Analysis%20of%20Area%20Ratio%20In%20a%20CD%20Nozzle.pdf http://irep.iium.edu.my/72294/7/72294_Analysis%20of%20area%20ratio%20in%20a%20CD%20nozzle_scopus.pdf

Similar Items

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 nozzle flow in a suddenly expanded duct with micro jets
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)

Investigation of the effects of nozzle exit mach number and nozzle pressure ratio on axisymmetric flow through suddenly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2019)

CFD analysis of effect of Mach number, area ratio and nozzle pressure ratio on velocity for suddenly expanded flows
by: Pathan, Khizer Ahmed, et al.
Published: (2017)

Exprimental study suddenly expanded flow from correctly expanded nozzles
by: Fharukh, G M, et al.
Published: (2016)

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

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

Modeling and analysis of convergent divergent nozzle with sudden expansion duct using finite element method
by: Aabid, Abdul, et al.
Published: (2019)

Modelling and analysis of convergent divergent nozzle with sudden expansion duct using finite element method
by: Aabid, Abdul, et al.
Published: (2019)

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

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

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

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

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)

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)

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)

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)

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

Computational and analytical investigation of aerodynamic derivatives of similitude delta wing model at hypersonic speeds
by: Bashir, Musavir, et al.
Published: (2017)

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

CFD analysis of splitter plate on bluff body
by: Aabid, Abdul, et al.
Published: (2019)

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

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

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)

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

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

Control of suddenly expanded flow for area ratio 3.61
by: Syed, Syed Ashfaq, et al.
Published: (2013)

Assessment of different turbulence models in simulating axisymmetric flow in suddenly expanded nozzles
by: Khan, Sher Afghan, 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)

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

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

Control of ideally expanded and under expanded nozzle flows with micro jets
by: G M, Fharukh Ahmed, et al.
Published: (2016)

Active control of suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2000)

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

Investigation of base pressure variations in internal and external suddenly expanded flows using CFD analysis
by: Pathan, Khizer Ahmed, 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)

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)

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)