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/ 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) -
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) -
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) -
Control of suddenly expanded flow at low supersonic Mach
numbers
by: Chaudhury, Zakir Ilahi, et al.
Published: (2015) -
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)