Modelling of suddenly expanded flow process in supersonic Mach regime using design of experiments and response surface methodology
The present work is an attempt to model, analyze, and control the flow at the base of an abruptly expanded circular duct by using design of experiments (DOE) and response surface methodology (RSM). Tiny-jets in the form of orifice were positioned at an interval of 900, 6.5 mm from the primary axis o...
| Main Authors: | Quadros, Jaimon Dennis, Khan, Sher Afghan, A. J., Antony |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
university of Tehran
2018
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/64156/ http://irep.iium.edu.my/64156/1/64156_Modelling%20of%20Suddenly%20Expanded%20Flow.pdf http://irep.iium.edu.my/64156/2/64156_Modelling%20of%20Suddenly%20Expanded%20Flow_WOS.pdf |
Similar Items
Predictive modeling of suddenly expanded flow process in the Supersonic Mach number regime using response surface methodology
by: Quadros, Jaimon Dennis, et al.
Published: (2017)
by: Quadros, Jaimon Dennis, et al.
Published: (2017)
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)
by: Quadros, Jaimon Dennis, et al.
Published: (2020)
Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD
by: Quadros, Jaimon Dennis, et al.
Published: (2020)
by: Quadros, Jaimon Dennis, et al.
Published: (2020)
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)
by: Quadros, Jaimon Dennis, et al.
Published: (2018)
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)
by: Quadros, Jaimon Dennis, et al.
Published: (2018)
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)
by: Quadros, Jaimon Dennis, et al.
Published: (2018)
Experimental and numerical investigation of suddenly expanded flow field for supersonic Mach numbers with and without annular cavities
by: Quadros, Jaimon Dennis, et al.
Published: (2020)
by: Quadros, Jaimon Dennis, et al.
Published: (2020)
Investigation of effect of process parameters on suddenly expanded flows through an axi-symmetric nozzle for different Mach numbers using design of experiments
by: Quadros, Jaimon Dennis, et al.
Published: (2017)
by: Quadros, Jaimon Dennis, et al.
Published: (2017)
Control of suddenly expanded flow at low supersonic Mach
numbers
by: Chaudhury, Zakir Ilahi, et al.
Published: (2015)
by: Chaudhury, Zakir Ilahi, et al.
Published: (2015)
Optimization of area ratio and thrust in suddenly expanded flow at supersonic Mach numbers
by: Pathan, Khizer Ahmed, et al.
Published: (2018)
by: Pathan, Khizer Ahmed, et al.
Published: (2018)
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)
by: Pathan, Khizer Ahmed, et al.
Published: (2017)
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)
by: Quadros, Jaimon Dennis, 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)
by: Bashir, Musavir, et al.
Published: (2015)
Experimental investigations on wall pressure in suddenly enlarged ducts at supersonic Mach number regimes
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
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)
by: Quadros, Jaimon Dennis, et al.
Published: (2016)
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)
by: Bashir, Musavir, et al.
Published: (2016)
Control of nozzle flow using microjets at supersonic Mach Regime
by: G M, Fharukh, et al.
Published: (2019)
by: G M, Fharukh, et al.
Published: (2019)
Numerical simulation of suddenly expanded flow at Mach 2.2
by: Aabid, Abdul, et al.
Published: (2019)
by: Aabid, Abdul, 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)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
Determination of wall pressure flows at supersonic Mach numbers
by: Aabid, Abdul, et al.
Published: (2020)
by: Aabid, Abdul, et al.
Published: (2020)
Experiment on of nozzle flow with sudden expansion at Mach 1.1
by: Faheem, Mohammad, et al.
Published: (2019)
by: Faheem, Mohammad, et al.
Published: (2019)
Control of suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2006)
by: Khan, Sher Afghan, et al.
Published: (2006)
Base pressure control by supersonic micro jets in a suddenly expanded nozzle
by: Khan, Sher Afghan, et al.
Published: (2018)
by: Khan, Sher Afghan, et al.
Published: (2018)
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)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
CFD analysis of the supersonic nozzle flow with sudden expansion
by: Ahmed, Khizar Pathan, et al.
Published: (2016)
by: Ahmed, Khizar Pathan, et al.
Published: (2016)
Active control of suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2000)
by: Khan, Sher Afghan, et al.
Published: (2000)
Control of suddenly expanded flow from correctly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004)
by: Khan, Sher Afghan, et al.
Published: (2004)
Control of suddenly expanded flows with micro-jets
by: Khan, Sher Afghan, et al.
Published: (2003)
by: Khan, Sher Afghan, et al.
Published: (2003)
Active control of suddenly expanded flow from under expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2004)
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)
by: Khan, Sher Afghan, et al.
Published: (2019)
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)
by: Khan, Sher Afghan, et al.
Published: (2019)
Experimental study of suddenly expanded flow from correctly expanded nozzles
by: Khan, Sher Afghan, et al.
Published: (2016)
by: Khan, Sher Afghan, et al.
Published: (2016)
Active control of wall pressure flow field at low supersonic Mach numbers
by: Asad Ullah, Mohammed, et al.
Published: (2016)
by: Asad Ullah, Mohammed, et al.
Published: (2016)
Optimization of two-dimensional wedge flow field at
supersonic Mach number
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, et al.
Published: (2019)
Estimation of stability derivatives of a wedges at supersonic Mach numbers
by: Shanbhag, Pavithra, et al.
Published: (2017)
by: Shanbhag, Pavithra, et al.
Published: (2017)
Control of wall pressure flow field with micro jets and control effectiveness
by: Bashir, Musavir, et al.
Published: (2016)
by: Bashir, Musavir, et al.
Published: (2016)
Exprimental study suddenly expanded flow from correctly expanded nozzles
by: Fharukh, G M, et al.
Published: (2016)
by: Fharukh, G M, et al.
Published: (2016)
Analysis of variation of stiffness derivative with Mach number and angle of attack for a supersonic flow
by: Crasta, Asha, et al.
Published: (2016)
by: Crasta, Asha, et al.
Published: (2016)
Nozzle expansion level effect on a suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2006)
by: Khan, Sher Afghan, et al.
Published: (2006)
Base pressure control using micro-jets in supersonic flow regimes
by: Sethuraman, Vigneshvaran, et al.
Published: (2018)
by: Sethuraman, Vigneshvaran, et al.
Published: (2018)
Similar Items
-
Predictive modeling of suddenly expanded flow process in the Supersonic Mach number regime using response surface methodology
by: Quadros, Jaimon Dennis, et al.
Published: (2017) -
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) -
Prediction of base pressure in a suddenly expanded flow process at supersonic mach number regimes using ANN and CFD
by: Quadros, Jaimon Dennis, et al.
Published: (2020) -
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) -
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)