Experimental investigation of a vertical round free turbulent jet

QR Code

Experimental investigation of a vertical round free turbulent jet

An experimental investigation of the flow in a vertical round free turbulent jet has been carried out. This study attempts to map the Reynolds stresses and to determine the differences in mean velocity profiles, turbulence intensity profiles, and velocity spectra in the flow of a vertical round free...

Full description

Bibliographic Details
Main Authors:	Zayan, Jalal Mohammad, Asrar, Waqar, Hoda, Asif
Format:	Proceeding Paper
Language:	English English
Published:	2013
Subjects:	QC Physics TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/35159/ http://irep.iium.edu.my/35159/4/Experimental_investigation_of_a_vertical_round_free_turbulent_jet.pdf http://irep.iium.edu.my/35159/1/Exp_Investigation_of_a_vertical_round_free_turbulent_jet.pdf

Similar Items

Experimental investigation of a new spiral wingtip
by: Siddiqui, Naseeb, et al.
Published: (2018)

Experimental investigation of wing tip vortex
by: Elsayed, Omer Ali, et al.
Published: (2009)

A gas-kinetic BGK solver for two-dimensional turbulent compressible flow
by: Ong, Jiunn Chit, et al.
Published: (2008)

Experimental investigation of the vortical flow around a reverse delta wing using PIV
by: Altaf, Afaq, et al.
Published: (2010)

Experimental investigation of free wing IIUM-UAV configuration
by: Omar, Ashraf Ali, et al.
Published: (2010)

Experimental investigation of the influence of a reverse delta type add-on device on the flap-tip vortex of a wing
by: Altaf, Afaq, et al.
Published: (2017)

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 studies of the base flow from the nozzles with sudden expansion with micro jets
by: Chaudhary, Zakir Ilahi, et al.
Published: (2016)

Investigation of aerodynamic parameters of a hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2012)

Numerical investigation of the flow over delta wing and reverse delta wing
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)

An Experimental Study Of Unsteady Vortex / Turbulent Boundary Layer Interactions
by: Haji Serakawi, Abdul Rashid
Published: (2011)

Numerical investigation of the vortical flow over delta wing and reverse delta wing
by: Omar, Ashraf Ali E., et al.
Published: (2012)

Investigation of the vortical flow around a reverse delta wing
by: Altaf, Afaq, et al.
Published: (2011)

Analysis of an airfoil using a transition and turbulence model
by: Islam, Mazharul, et al.
Published: (2016)

Control of base flows with micro jets
by: Ahmed Ali Baig, Maughal, et al.
Published: (2011)

Low reynolds number numerical simulation of the aerodynamic coefficients of a 3D wing
by: Malik, Khurshid, et al.
Published: (2018)

Control of suddenly expanded flows with micro-jets
by: Khan, Sher Afghan, et al.
Published: (2003)

Design, fabrication and experimental testing of IIUM free wing unmanned aerial vehicle (IIUM-FWUAV)
by: Omar, Ashraf Ali E., et al.
Published: (2011)

Development of a jet powered floating platform (in air)
by: Zharif, M., et al.
Published: (2011)

Literature review : Biomimetic and conventional aircraft wing tips
by: Ahmed Siddiqui, Naseeb, et al.
Published: (2017)

Numerical study of effect of spoiler configuration on wake vortex alleviation
by: Ludin@Jamaluddin, Hani, et al.
Published: (2015)

Estimation of aerodynamic parameters of IIUM hybrid airship
by: Andan, Amelda Dianne, et al.
Published: (2011)

Evaluation of aircraft wing-tip vortex using PIV
by: Elsayed, Omer Ali, et al.
Published: (2009)

Higher order compact-flowfield dependent variation (HOC-FDV) solution of one-dimensional problems
by: Elfaghi, Abdulhafid M., et al.
Published: (2010)

Study of the reverse delta wing
by: Altaf, Afaq, et al.
Published: (2011)

The accuracy of the gas-kinetic BGK finite difference method for solving 3-D compressible inviscid flows
by: Ong, Jiunn Chit, et al.
Published: (2011)

Span load modification via differential spoiler setting
by: Elsayed, Omer Ali, et al.
Published: (2010)

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 pressure with micro jets for area ratio 2.4
by: Ashfaq, Syed, et al.
Published: (2014)

CFD analysis of a SD 7003 airfoil with a local correlation based transition and turbulence model
by: Islam, Mazharul, et al.
Published: (2017)

CFD analysis of a SD 7003 airfoil with a local correlation based transition and turbulence model
by: Islam, Mazharul, et al.
Published: (2016)

Experimental research of wall pressure distribution and effect of micro jet at Mach 1.5
by: Azami, Muhammad Hanafi, et al.
Published: (2019)

Reynolds averaged navier-stokes flow computation of RAE2822 airfoil using gas-kinetic BGK Scheme
by: Ong, Jiunn Chit, et al.
Published: (2009)

A high order compact-flowfield dependent variation (HOC-FDV)method for inviscid flows
by: Elfaghi, Abdulhafid M., et al.
Published: (2010)

Higher order compact-flowfield dependent variation (HOCFDV) method for solving navier-stokes equations
by: Elfaghi, Abdulhafid M., et al.
Published: (2010)

Influence of micro jets on the flow development in the enlarged duct at supersonic Mach number
by: Khan, Sher Afghan, et al.
Published: (2019)

Studies on wall pressure flow control by micro jets for high area ratio
by: Ashfaq, Syed, et al.
Published: (2014)

Effect of diamond shaped strut with cylindrical pitch rod in subsonic wind tunnel testing
by: UlHaque, Anwar, et al.
Published: (2017)

Wind tunnel testing on a generic model of a hybrid lifting hull
by: UlHaque, Anwar, et al.
Published: (2016)

Impact of a reverse delta type add-on device on the flap-tip vortex of a wing
by: Altaf, Afaq, et al.
Published: (2016)