Experimental research of wall pressure distribution and effect of micro jet at Mach 1.5
In this paper, a study on the effect of the control on the wall pressure as well as the quality of the flow when tiny jets were employed. The small jet aimed to regulate the base pressure at the base region of the suddenly expanded duct and wall pressure distribution is carried out experimentally. T...
| Main Authors: | Azami, Muhammad Hanafi, Faheem, Mohammed, Aabid, Abdul, Mokashi, Imran, Khan, Sher Afghan |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
Blue Eyes Intelligence Engineering & Sciences Publication
2019
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/74318/ http://irep.iium.edu.my/74318/7/74318%20Experimental%20Research%20of%20Wall%20Pressure.pdf http://irep.iium.edu.my/74318/8/74318%20Experimental%20Research%20of%20Wall%20Pressure%20SCOPUS.pdf |
Similar Items
Experimental research on wall pressure distribution in C-D nozzle at Mach number 1.1 for area ratio 3.24
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, et al.
Published: (2019)
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)
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)
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)
Wall Pressure Measurements Beneath the Supersonic Jets in
an Abruptly Augmented Nozzle
by: Bashir, Musavir, et al.
Published: (2020)
by: Bashir, Musavir, 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)
Pressure and its derivative with respect to piston Mach number for an oscillating cone
by: Shabana, Ayesha, et al.
Published: (2016)
by: Shabana, Ayesha, et al.
Published: (2016)
Experimental research on flow development and control effectiveness in the duct at high speed
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, et al.
Published: (2019)
Influence of control mechanism on the flow field of duct at Mach 1.2 for area ratio 2.56
by: Khan, Sher Afghan, et al.
Published: (2019)
by: Khan, Sher Afghan, 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)
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)
by: Pathan, Khizer Ahmed, et al.
Published: (2019)
Investigation of base flow for an axisymmetric suddenly
expanded nozzle with micro JET
by: Chaudhary, Zakir Ilahi, et al.
Published: (2018)
by: Chaudhary, Zakir Ilahi, et al.
Published: (2018)
An investigation of effect of control jets location and blowing pressure ratio to control base pressure in suddenly expanded flows
by: Pathan, Khizar Ahmed, et al.
Published: (2020)
by: Pathan, Khizar Ahmed, et al.
Published: (2020)
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)
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)
by: Sethuraman, Vigneshvaran, et al.
Published: (2019)
Base and wall pressure control using cavities and ribs in suddenly expanded flows -an overview
by: Sethuraman, Vigneshvaran, et al.
Published: (2020)
by: Sethuraman, Vigneshvaran, et al.
Published: (2020)
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 base pressure with micro jets:part-I
by: Rehman, Shafiqur, et al.
Published: (2008)
by: Rehman, Shafiqur, et al.
Published: (2008)
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)
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)
Numerical investigation of splitter plate effect on the bluff body using finite volume method
by: Afifi, Azmil, et al.
Published: (2020)
by: Afifi, Azmil, et al.
Published: (2020)
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)
Influence of expansion level on base pressure and reattachment length
by: Pathan, Khizar Ahmed, et al.
Published: (2019)
by: Pathan, Khizar Ahmed, et al.
Published: (2019)
Role of active control in increasing base pressure at Sonic Mach Number
by: G. M, Fharukh Ahmed, et al.
Published: (2019)
by: G. M, Fharukh Ahmed, et al.
Published: (2019)
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)
Comparative analysis of alternative fuels in detonation
combustion
by: Azami, Muhammad Hanafi, et al.
Published: (2016)
by: Azami, Muhammad Hanafi, et al.
Published: (2016)
Analysis of parameters affecting thrust and base pressure in
suddenly expanded flow from nozzle
by: Pathan, Khizar Ahmed, et al.
Published: (2019)
by: Pathan, Khizar Ahmed, et al.
Published: (2019)
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)
Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow
by: Khan, Sher Afghan
Published: (2015)
by: Khan, Sher Afghan
Published: (2015)
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)
Enlarge duct length optimization for suddenly expanded flows
by: Pathan, Khizer Ahmed, et al.
Published: (2020)
by: Pathan, Khizer Ahmed, et al.
Published: (2020)
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)
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)
Comparing the effect of different turbulence models on the CFD predictions of NACA0018 airfoil aerodynamics
by: Khan, Sher Afghan, et al.
Published: (2020)
by: Khan, Sher Afghan, et al.
Published: (2020)
Effect of level of expansion and inertia level in a suddenly expanded flow
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)
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)
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)
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)
by: Khan, Sher Afghan, et al.
Published: (2018)
The contribution of Hassan al-Rammah to gunpowder and rocket technology
by: Ahmed Ghazal, Belal, et al.
Published: (2011)
by: Ahmed Ghazal, Belal, et al.
Published: (2011)
Similar Items
-
Experimental research on wall pressure distribution in C-D nozzle at Mach number 1.1 for area ratio 3.24
by: Khan, Sher Afghan, et al.
Published: (2019) -
Influence of micro jets on wall pressure for area ratio 3.24
by: Ashfaq, Syed, et al.
Published: (2014) -
Active control of wall pressure flow field at low supersonic Mach numbers
by: Asad Ullah, Mohammed, 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) -
Wall Pressure Measurements Beneath the Supersonic Jets in
an Abruptly Augmented Nozzle
by: Bashir, Musavir, et al.
Published: (2020)