Numerical simulations of a CD nozzle and the influence of the duct length

QR Code

Numerical simulations of a CD nozzle and the influence of the duct length

A numerical method is used to observe the effect of microjets control on wall pressure spreading in sudden expansion two-dimensional planar duct. In order to find the microjet effectiveness 2-jets of 1 mm diameter orifice located precisely at 900 of intervals along a pitch-circle-distance (PCD) of 1...

Full description

Bibliographic Details
Main Authors:	Akhtar, Mohammad Nishat, Abu Bakar, Elmi, Aabid, Abdul, Khan, Sher Afghan
Format:	Article
Language:	English English
Published:	Blue Eyes Intelligence Engineering & Sciences 2019
Subjects:	T Technology (General) TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://irep.iium.edu.my/74733/ http://irep.iium.edu.my/74733/1/74733_Numerical%20Simulations%20of%20a%20CD%20Nozzle.pdf http://irep.iium.edu.my/74733/7/74733_Numerical%20simulations%20of%20a%20CD%20nozzle%20and%20the%20influence%20of%20the%20duct%20length_Scopus.pdf

Similar Items

Control of CD nozzle flow using microjets at Mach 2.1
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)

Effects of micro jets on the flow field of the duct with sudden expansion
by: Akhtar, Mohammad Nishat, et al.
Published: (2019)

Control of nozzle flow in a suddenly expanded duct with micro jets
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)

Analysis of area ratio in a CD nozzle with suddenly expanded duct using CFD method
by: Khan, Sher Afghan, 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)

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)

Experiment on of nozzle flow with sudden expansion at Mach 1.1
by: Faheem, Mohammad, et al.
Published: (2019)

Active control of flow through the nozzles at sonic Mach number
by: Ashfaq, Syed, et al.
Published: (2013)

Modeling and analysis of convergent divergent nozzle with sudden expansion duct using finite element method
by: Aabid, Abdul, et al.
Published: (2019)

Experimental studies on low speed converging nozzle flow with sudden expansion
by: Ashfaq, Syed, et al.
Published: (2014)

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)

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)

Inspection of supersonic flows in a CD nozzle using experimental method
by: Azami, Muhammad Hanafi, et al.
Published: (2019)

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)

Investigation of efficacy of low length-to-diameter ratio and nozzle pressure ratio on base pressure in an abruptly expanded flow
by: Ahmed, Fharrukh, et al.
Published: (2018)

Nozzle expansion level effect on a suddenly expanded flow
by: Khan, Sher Afghan, et al.
Published: (2006)

Design and fabrication of flying saucer utilizing coanda effect
by: Aabid, Abdul, et al.
Published: (2018)

Determination of wall pressure flows at supersonic Mach numbers
by: Aabid, Abdul, et al.
Published: (2020)

Active control of suddenly expanded flows from overexpanded nozzles
by: Khan, Sher, et al.
Published: (2002)

Experimental investigation of the base flow from the nozzles with sudden expansion
by: Chaudhary, Zakir Ilahi, et al.
Published: (2015)

Control of nozzle flow using microjets at supersonic Mach Regime
by: G M, Fharukh, et al.
Published: (2019)

Numerical investigation of mathematical non-dimensional constant representing smoothness in the Nusselt profile
by: Ansari, Emad, et al.
Published: (2020)

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)

Experimental investigations on wall pressure in suddenly enlarged ducts at supersonic Mach number regimes
by: Baig, Maugal Ahmed Ali, et al.
Published: (2012)

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)

Base pressure control by supersonic micro jets in a suddenly expanded nozzle
by: Khan, Sher Afghan, et al.
Published: (2018)

Modeling and structural analysis of three-dimensional wing
by: Mohd Zakuan, Muhammad Amir Mirza, et al.
Published: (2019)

Research onFlows for NACA 2412 airfoil using computational Fluid dynamics method
by: Kharulaman, Liyana, et al.
Published: (2019)

Base pressure control using micro-jets in supersonic flow regimes
by: Sethuraman, Vigneshvaran, et al.
Published: (2018)

Oscillating supersonic delta wing with straight leading edges
by: Crasta, Asha, et al.
Published: (2012)

Role of ultrasonication duration and surfactant on characteristics of ZnO and CuO nanofluids
by: Afzal, Asif, et al.
Published: (2019)

High incidence supersonic similitude for planar wedge
by: Crasta, Asha, et al.
Published: (2012)

Oscillating supersonic delta wings with straight leading edges
by: Crasta, Asha, et al.
Published: (2012)

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)

CFD analysis of effect of area ratio on suddenly expanded flows
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)

CFD studies on triangular micro-vortex generators in flow control
by: Yashodhar, V., et al.
Published: (2017)

Dynamic stability of unguided projectile with 6- DOF trajectory modeling
by: Bashir, Musavir, et al.
Published: (2017)

Influence of low length-to-diameter ratio and nozzle pressure ratio in an abruptly expanded flow
by: Khan, Sher Afghan
Published: (2015)

Low-cost base drag reduction technique
by: Asad Ullah, Mohammed, et al.
Published: (2018)