Grooved cavity as a passive controller behind backward facing step
A semicircular grooved cavity is designed for controlling the base pressure and hence the base drag in case of a backward facing step. This paper presents the effect of the continuous grooved cavity to control the base pressure for various compressible subsonic flow to minimize the base drag. The...
| Main Authors: | Khan, Sher Afghan, Alrobaian, Abdul Rahman, Asad Ullah, Mohammed, Khan, Abdul Mohsin |
|---|---|
| Format: | Article |
| Language: | English English |
| Published: |
Penerbit Akademia Baru
2019
|
| Subjects: | |
| Online Access: | http://irep.iium.edu.my/69634/ http://irep.iium.edu.my/69634/7/69634%20Grooved%20Cavity%20as%20a%20Passive%20Controller.pdf http://irep.iium.edu.my/69634/8/69634%20Grooved%20Cavity%20as%20a%20Passive%20Controller%20%20SCOPUS.pdf |
Similar Items
Passive control of base drag in compressible subsonic flow using multiple cavity
by: Khan, Sher Afghan, et al.
Published: (2018)
by: Khan, Sher Afghan, et al.
Published: (2018)
Passive control of base drag employing dimple in subsonic suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2018)
by: Khan, Sher Afghan, et al.
Published: (2018)
Flow control with aero-spike behind bluff body
by: Khan, Sher Afghan, et al.
Published: (2018)
by: Khan, Sher Afghan, et al.
Published: (2018)
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)
On numerical investigation of semi-empirical relation representing development length for a fluid flow in a closed conduit
by: Mohd Umair, Siddique, et al.
Published: (2019)
by: Mohd Umair, Siddique, et al.
Published: (2019)
Low-cost base drag reduction technique
by: Asad Ullah, Mohammed, et al.
Published: (2018)
by: Asad Ullah, Mohammed, et al.
Published: (2018)
Effect of angle of attack on damping derivatives of delta wing with full sine wave curved leading edge
by: Crasta, Asha, et al.
Published: (2015)
by: Crasta, Asha, et al.
Published: (2015)
Aerodynamic analysis of groove based vortex trap configuration on the retreating helicopter blade
by: Yaakub, Mohd Fauzi
Published: (2019)
by: Yaakub, Mohd Fauzi
Published: (2019)
Design and fabrication of flying saucer utilizing coanda effect
by: Aabid, Abdul, et al.
Published: (2018)
by: Aabid, Abdul, 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)
Modeling and analysis of convergent divergent nozzle with
sudden expansion duct using finite element method
by: Aabid, Abdul, et al.
Published: (2019)
by: Aabid, Abdul, et al.
Published: (2019)
Design and fabrication of unmanned arial vehicle for multi-mission tasks
by: Khan, Sher Afghan, et al.
Published: (2018)
by: Khan, Sher Afghan, et al.
Published: (2018)
Base pressure control using micro-jets in supersonic flow regimes
by: Sethuraman, Vigneshvaran, et al.
Published: (2018)
by: Sethuraman, Vigneshvaran, et al.
Published: (2018)
Oscillating supersonic delta wing with straight leading edges
by: Crasta, Asha, et al.
Published: (2012)
by: Crasta, Asha, et al.
Published: (2012)
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)
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)
Simulation of effect of various distances between front and rear body on drag of a non-circular cylinder
by: Sajali, Muhammad Fahmi Mohd, et al.
Published: (2019)
by: Sajali, Muhammad Fahmi Mohd, et al.
Published: (2019)
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)
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)
Control of base pressure with micro jets:part-I
by: Rehman, Shafiqur, et al.
Published: (2008)
by: Rehman, Shafiqur, et al.
Published: (2008)
Control of suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2006)
by: Khan, Sher Afghan, et al.
Published: (2006)
High incidence supersonic similitude for planar wedge
by: Crasta, Asha, et al.
Published: (2012)
by: Crasta, Asha, et al.
Published: (2012)
Estimation of stability derivatives of an oscillating hypersonic delta wings with curved leading edges
by: Crasta, Asha, et al.
Published: (2012)
by: Crasta, Asha, et al.
Published: (2012)
Stabilty derivatives in the newtonian limit
by: Crasta, Asha, et al.
Published: (2013)
by: Crasta, Asha, et al.
Published: (2013)
Stability derivatives of a delta wing with straight leading edge in the Newtonian limit
by: Crasta, Asha, et al.
Published: (2013)
by: Crasta, Asha, et al.
Published: (2013)
Oscillating supersonic delta wings with straight leading edges
by: Crasta, Asha, et al.
Published: (2012)
by: Crasta, Asha, et al.
Published: (2012)
Experimental studies on low speed converging nozzle flow with sudden expansion
by: Ashfaq, Syed, et al.
Published: (2014)
by: Ashfaq, Syed, et al.
Published: (2014)
Numerical investigation of semi-empirical relation representing nusselt number under waterjet impingement
by: Siddiqui, Mohammad Umair, et al.
Published: (2020)
by: Siddiqui, Mohammad Umair, et al.
Published: (2020)
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)
Role of ultrasonication duration and surfactant on characteristics of ZnO and CuO nanofluids
by: Afzal, Asif, et al.
Published: (2019)
by: Afzal, Asif, et al.
Published: (2019)
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)
CFD analysis of effect of area ratio on suddenly expanded flows
by: Pathan, Khizer Ahmed, et al.
Published: (2017)
by: Pathan, Khizer Ahmed, et al.
Published: (2017)
An investigation to control base pressure in suddenly expanded flows
by: Pathan, Khizer Ahmed, et al.
Published: (2018)
by: Pathan, Khizer Ahmed, 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)
Modeling and structural analysis of three-dimensional wing
by: Mohd Zakuan, Muhammad Amir Mirza, et al.
Published: (2019)
by: Mohd Zakuan, Muhammad Amir Mirza, et al.
Published: (2019)
Passive drag reduction of square back road vehicles
by: Altaf, Alaman, et al.
Published: (2014)
by: Altaf, Alaman, et al.
Published: (2014)
CFD studies on triangular micro-vortex generators in flow control
by: Yashodhar, V., et al.
Published: (2017)
by: Yashodhar, V., et al.
Published: (2017)
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)
Dynamic stability of unguided projectile with 6-
DOF trajectory modeling
by: Bashir, Musavir, et al.
Published: (2017)
by: Bashir, Musavir, et al.
Published: (2017)
Control of CD nozzle flow using microjets at Mach 2.1
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)
Similar Items
-
Passive control of base drag in compressible subsonic flow using multiple cavity
by: Khan, Sher Afghan, et al.
Published: (2018) -
Passive control of base drag employing dimple in subsonic suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2018) -
Flow control with aero-spike behind bluff body
by: Khan, Sher Afghan, et al.
Published: (2018) -
Exprimental study suddenly expanded flow from correctly expanded nozzles
by: Fharukh, G M, et al.
Published: (2016) -
On numerical investigation of semi-empirical relation representing development length for a fluid flow in a closed conduit
by: Mohd Umair, Siddique, et al.
Published: (2019)