Control of base pressure with micro jets for area ratio 2.4
This paper presents the results of experimental studies to control the base pressure from a convergent nozzle to ascertain the effect of level of expansion in a suddenly expanded flow at sonic Mach number. An active control in the form of four micro jets of 1 mm orifice diameter located at 900 inter...
| Main Authors: | Ashfaq, Syed, Khan, Sher Afghan, Rathakrishnan, Ethirajan |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Praise Worthy Prize
2014
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/49828/ http://irep.iium.edu.my/49828/1/IREME-2014.pdf |
Similar Items
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)
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)
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)
Control of suddenly expanded flows with micro-jets
by: Khan, Sher Afghan, et al.
Published: (2003)
by: Khan, Sher Afghan, et al.
Published: (2003)
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)
Influence of micro jets on wall pressure for area ratio 3.24
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
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)
Base pressure studies from over expanded nozzle for area ratio 2.56
by: Baig, Maughal Ahmed Al, et al.
Published: (2012)
by: Baig, Maughal Ahmed Al, et al.
Published: (2012)
Active control of base pressure in supersonic regime
by: Khan, Sher Afghan, et al.
Published: (2006)
by: Khan, Sher Afghan, et al.
Published: (2006)
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)
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)
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)
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)
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)
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)
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)
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)
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)
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)
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)
Active control of base pressure in suddenly expanded flow for area ratio 4.84
by: Ali Baig, Maughal Ahmed, et al.
Published: (2012)
by: Ali Baig, Maughal Ahmed, et al.
Published: (2012)
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)
Control of base pressure with micro jets:part-I
by: Rehman, Shafiqur, et al.
Published: (2008)
by: Rehman, Shafiqur, et al.
Published: (2008)
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)
Effectiveness of micro-jets at different level of expansion
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)
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)
Studies on flow from convergent nozzle with sudden expansion and control effectiveness under the influence of micro jets
by: Ashfaq, Syed, et al.
Published: (2013)
by: Ashfaq, Syed, et al.
Published: (2013)
The effect of micro jets on wall pressure for sonic under expanded flow
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
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)
Base pressure control using micro-jets in supersonic flow regimes
by: Sethuraman, Vigneshvaran, et al.
Published: (2018)
by: Sethuraman, Vigneshvaran, 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)
by: Pathan, Khizer Ahmed, et al.
Published: (2019)
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)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
Wall pressure studies in a suddenly expanded flow for area ratio 2.56”
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)
Modelling of a three-shaft high-bypass-ratio engine performance and emission prediction using hydrogen fuels
by: Wan Yahya, M.Z., et al.
Published: (2019)
by: Wan Yahya, M.Z., et al.
Published: (2019)
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)
Supersonic similitude for oscillating non-planar wedge
by: Crasta, Asha, et al.
Published: (2014)
by: Crasta, Asha, et al.
Published: (2014)
Studies on wall pressure of sonic flow through the converging nozzles for different area ratios
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
Development of a jet powered floating platform (in air)
by: Zharif, M., et al.
Published: (2011)
by: Zharif, M., et al.
Published: (2011)
Effect of aspect ratio with angle of attack of an oscillating hypersonic delta wing with straight leading edges
by: Crasta, Asha, et al.
Published: (2015)
by: Crasta, Asha, et al.
Published: (2015)
Similar Items
-
Studies on wall pressure flow control by micro jets for high area ratio
by: Ashfaq, Syed, et al.
Published: (2014) -
Control of base flows with micro jet for area ratio of 6.25
by: Ali Baig, Maughal Ahmed, et al.
Published: (2012) -
Control of base flows with micro jets
by: Ahmed Ali Baig, Maughal, et al.
Published: (2011) -
Control of suddenly expanded flows with micro-jets
by: Khan, Sher Afghan, et al.
Published: (2003) -
Effect of mach number on wall pressure flow field for area ratio 2.56
by: Ashfaq, Syed, et al.
Published: (2014)