Influence of micro jets on the flow development in the enlarged duct at supersonic Mach number
In this paper, Computational fluid dynamics method is used to simulate the supersonic flow. Convergent-divergent (C-D) nozzle have been used with sudden expansion. The base pressure controlled by using the microjets of 1 mm of orifice diameter is arranged at ninety degrees at PCD 13 mm. The Mach num...
| Main Authors: | Khan, Sher Afghan, Aabid, Abdul, Saleel, Ahmed |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
International Journals of Engineering & Sciences (IJENS:)
2019
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/71238/ http://irep.iium.edu.my/71238/1/71238_Influence%20of%20Micro%20Jets%20on%20the%20Flow%20Development.pdf http://irep.iium.edu.my/71238/7/71238_Influence%20of%20micro%20jets%20on%20the%20flow_SCOPUS.pdf |
Similar Items
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)
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)
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)
by: Pathan, Khizer Ahmed, et al.
Published: (2018)
Determination of wall pressure flows at supersonic Mach numbers
by: Aabid, Abdul, et al.
Published: (2020)
by: Aabid, Abdul, et al.
Published: (2020)
Effects of micro jets on the flow field of the duct with sudden expansion
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)
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)
Effect of micro jet control on the flow filed of the duct at Mach 1.5
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, et al.
Published: (2019)
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)
Control of nozzle flow in a suddenly expanded duct with micro jets
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
Control of base flows with micro jet for area ratio of 6.25
by: Ali Baig, Maughal Ahmed, et al.
Published: (2012)
by: Ali Baig, Maughal Ahmed, et al.
Published: (2012)
Experimental research of wall pressure distribution and effect of micro jet at Mach 1.5
by: Azami, Muhammad Hanafi, et al.
Published: (2019)
by: Azami, Muhammad Hanafi, et al.
Published: (2019)
Effect of mach number on wall pressure flow field for area ratio 2.56
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
Control of suddenly expanded flows with micro-jets
by: Khan, Sher Afghan, et al.
Published: (2003)
by: Khan, Sher Afghan, et al.
Published: (2003)
Control of base flows with micro jets
by: Ahmed Ali Baig, Maughal, et al.
Published: (2011)
by: Ahmed Ali Baig, Maughal, et al.
Published: (2011)
Effect of mach number on stiffness and damping derivatives for oscillating hyersonic non-planar wedge
by: Crasta, Asha, et al.
Published: (2014)
by: Crasta, Asha, et al.
Published: (2014)
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)
Numerical simulation of suddenly expanded flow at Mach 2.2
by: Aabid, Abdul, et al.
Published: (2019)
by: Aabid, Abdul, et al.
Published: (2019)
Studies on wall pressure flow control by micro jets for high area ratio
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
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)
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 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)
Analytical estimation of stability derivatives of wing with curved leading edges at hypersonic mach number
by: Renita, sharon Monis, et al.
Published: (2020)
by: Renita, sharon Monis, et al.
Published: (2020)
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)
Effect of aspect ratio with roll moment derivative of a delta wing in supersonic flow
by: Crasta, Asha, et al.
Published: (2016)
by: Crasta, Asha, et al.
Published: (2016)
Active control of base pressure in supersonic regime
by: Khan, Sher Afghan, et al.
Published: (2006)
by: Khan, Sher Afghan, et al.
Published: (2006)
Supersonic similitude for oscillating non-planar wedge
by: Crasta, Asha, et al.
Published: (2014)
by: Crasta, Asha, et al.
Published: (2014)
Experimental studies of the base flow from the nozzles with sudden expansion with micro jets
by: Chaudhary, Zakir Ilahi, et al.
Published: (2016)
by: Chaudhary, Zakir Ilahi, et al.
Published: (2016)
Estimation of stability derivatives in pitch for an oscillating 2-D wedge in supersonic Flow
by: Pavithra, Shanbhag,, et al.
Published: (2016)
by: Pavithra, Shanbhag,, et al.
Published: (2016)
Base pressure control using micro-jets in supersonic flow regimes
by: Sethuraman, Vigneshvaran, et al.
Published: (2018)
by: Sethuraman, Vigneshvaran, et al.
Published: (2018)
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)
Control of base pressure with micro jets for area ratio 2.4
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
CFD simulation with analytical and theoretical validation of different flow parameters for the wedge at supersonic Mach number
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, et al.
Published: (2019)
Enlarge duct length optimization for suddenly expanded flows
by: Pathan, Khizer Ahmed, et al.
Published: (2020)
by: Pathan, Khizer Ahmed, et al.
Published: (2020)
Inspection of supersonic flows in a CD nozzle using experimental method
by: Azami, Muhammad Hanafi, et al.
Published: (2019)
by: Azami, Muhammad Hanafi, et al.
Published: (2019)
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)
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)
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)
Roll control reversal of variable swept wing in supersonic flow
by: Ibren, Mohamed, et al.
Published: (2019)
by: Ibren, Mohamed, et al.
Published: (2019)
Active control of flow through the nozzles at sonic Mach number
by: Ashfaq, Syed, et al.
Published: (2013)
by: Ashfaq, Syed, et al.
Published: (2013)
Similar Items
-
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) -
Experimental investigations on wall pressure in suddenly enlarged ducts at supersonic Mach number regimes
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) -
Determination of wall pressure flows at supersonic Mach numbers
by: Aabid, Abdul, et al.
Published: (2020) -
Effects of micro jets on the flow field of the duct with sudden expansion
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)