This is a post-print of a paper from 15th Australasian Fluid Mechanics Conference 2004 published by AFMC. This version is reproduced with the permission of AFMC.Simultaneous dual-plane PIV experiments were performed instreamwise-spanwise planes in the log region of a turbulentboundary layer at a moderate Reynolds number (Ret » 1100).The acquired datasets were used to resolve all 9 velocity gradientsfrom which the complete vorticity vector and other invariantquantities like 3-D swirl strength were computed. Thesederived quantities were used to analyze and interpret the structuralcharacteristics and features of the boundary layer. Resultsof the vorticity vector and the 2-D swirl strength from the twoneighbouring planes indicate the existence ...
Spanwise structure and growth mechanisms in a turbulent boundary layer are investigated experimental...
An experiment has been performed in a turbulent boundary layer wind tunnel to study the coherent str...
University of Minnesota Ph.D. dissertation. March 2011. Major: Aerospace Engineering and Mechanics. ...
Simultaneous dual-plane PIV experiments, which utilized three cameras to measure velocity components...
© 2005 Springer Verlag. Publisher PDF version is restricted access in accordance with the Springer V...
This is a publisher’s PDF of an article published in Physics of Fluids 2006, published by American I...
Particle-image velocimetry (PIV) is used to measure instantaneous velocity fields in the streamwise ...
Particle-image velocimetry (PIV) is used to measure instantaneous velocity fields in the streamwise ...
The strength of vortical structures in a turbulent boundary layer is of interest in determining the ...
This is a publisher’s version of an article published in Journal of Fluid Mechanics © 2005 Cambridge...
Awaiting return of copyright permission formBy arranging the laser light-sheet and image plane of a ...
Dual-plane particle image velocimetry experiments were performed in a turbulent boundary layer with ...
Stereoscopic particle image velocimetry (PIV) measurements are made in streamwise–spanwise and incli...
Stereoscopic particle image velocimetry (PIV) was used to measure all three instantaneous components...
© Cambridge University Press. Hambleton, W.T., Hutchins, N., & Marusic, I. (2006). Simultaneous orth...
Spanwise structure and growth mechanisms in a turbulent boundary layer are investigated experimental...
An experiment has been performed in a turbulent boundary layer wind tunnel to study the coherent str...
University of Minnesota Ph.D. dissertation. March 2011. Major: Aerospace Engineering and Mechanics. ...
Simultaneous dual-plane PIV experiments, which utilized three cameras to measure velocity components...
© 2005 Springer Verlag. Publisher PDF version is restricted access in accordance with the Springer V...
This is a publisher’s PDF of an article published in Physics of Fluids 2006, published by American I...
Particle-image velocimetry (PIV) is used to measure instantaneous velocity fields in the streamwise ...
Particle-image velocimetry (PIV) is used to measure instantaneous velocity fields in the streamwise ...
The strength of vortical structures in a turbulent boundary layer is of interest in determining the ...
This is a publisher’s version of an article published in Journal of Fluid Mechanics © 2005 Cambridge...
Awaiting return of copyright permission formBy arranging the laser light-sheet and image plane of a ...
Dual-plane particle image velocimetry experiments were performed in a turbulent boundary layer with ...
Stereoscopic particle image velocimetry (PIV) measurements are made in streamwise–spanwise and incli...
Stereoscopic particle image velocimetry (PIV) was used to measure all three instantaneous components...
© Cambridge University Press. Hambleton, W.T., Hutchins, N., & Marusic, I. (2006). Simultaneous orth...
Spanwise structure and growth mechanisms in a turbulent boundary layer are investigated experimental...
An experiment has been performed in a turbulent boundary layer wind tunnel to study the coherent str...
University of Minnesota Ph.D. dissertation. March 2011. Major: Aerospace Engineering and Mechanics. ...