An artificial turbulent spot is simulated in a zero free-stream turbulence base flow and a base flow with organized streaks. Six identification methods are used in order to isolate the turbulent spot from the surrounding nonturbulent fluid. These are (i) instantaneous wall-normal velocity v, (ii) instantaneous spanwise velocity w, (iii) instantaneous turbulent dissipation, (iv) λ2 criterion, (v) Q criterion, and (vi) gradient of the finite time Lyapunov exponent. All methods are effective in isolating the turbulent spot from the streaks. The robustness of each technique is determined from the sensitivity of the maximum spot dimensions to changes in threshold level. The Q criterion shows the least sensitivity for the zero free-stream turbulence case and the instantaneous turbulent dissipation technique is least sensitive in the organized streaks case. For both cases the v technique was the most sensitive to changes in threshold level.
Skip Nav Destination
e-mail: t.zaki@imperial.ac.uk
e-mail: donaldm@uidaho.edu
Article navigation
January 2013
Research-Article
Identifying Turbulent Spots in Transitional Boundary Layers
Brendan Rehill,
Ed J. Walsh,
Ed J. Walsh
Stokes Institute,
University of Limerick,
Limerick
, Ireland
Search for other works by this author on:
Philipp Schlatter,
Philipp Schlatter
Linné Flow Centre,
KTH Mechanics,
Stockholm
, Sweden
Search for other works by this author on:
Tamer A. Zaki,
e-mail: t.zaki@imperial.ac.uk
Tamer A. Zaki
Department of Mechanical Engineering,
Imperial College London,
London, UK
e-mail: t.zaki@imperial.ac.uk
Search for other works by this author on:
Donald M. McEligot
e-mail: donaldm@uidaho.edu
Donald M. McEligot
Mechanical Engineering Department,
University of Idaho,
Idaho Falls, Idaho 83402
e-mail: donaldm@uidaho.edu
Search for other works by this author on:
Brendan Rehill
e-mail: brendan.rehill@ul.ie
Ed J. Walsh
Stokes Institute,
University of Limerick,
Limerick
, Ireland
Luca Brandt
e-mail: luca@mech.kth.se
Philipp Schlatter
Linné Flow Centre,
KTH Mechanics,
Stockholm
, Sweden
Tamer A. Zaki
Department of Mechanical Engineering,
Imperial College London,
London, UK
e-mail: t.zaki@imperial.ac.uk
Donald M. McEligot
Mechanical Engineering Department,
University of Idaho,
Idaho Falls, Idaho 83402
e-mail: donaldm@uidaho.edu
Contributed by the International Gas Turbine Institute (IGTI) of ASME for publication in the JOURNAL OF TURBOMACHINERY. Manuscript received July 11, 2011; final manuscript received August 19, 2011; published online October 30, 2012. Editor: David Wisler.
J. Turbomach. Jan 2013, 135(1): 011019 (8 pages)
Published Online: October 30, 2012
Article history
Received:
July 11, 2011
Revision Received:
August 19, 2011
Citation
Rehill, B., Walsh, E. J., Brandt, L., Schlatter, P., Zaki, T. A., and McEligot, D. M. (October 30, 2012). "Identifying Turbulent Spots in Transitional Boundary Layers." ASME. J. Turbomach. January 2013; 135(1): 011019. https://doi.org/10.1115/1.4006395
Download citation file:
Get Email Alerts
Cited By
Related Articles
Accurate Prediction of Loss Using High Fidelity Methods
J. Turbomach (March,2021)
Passive Manipulation of Separation-Bubble Transition Using Surface Modifications
J. Fluids Eng (February,2009)
Transition Mechanisms in Separation Bubbles Under Low- and Elevated-Freestream Turbulence
J. Turbomach (January,2010)
Measurements of the Effects of Streamwise Riblets on Boundary Layer Turbulence
J. Fluids Eng (November,2017)
Related Proceedings Papers
Related Chapters
Cavitating Structures at Inception in Turbulent Shear Flow
Proceedings of the 10th International Symposium on Cavitation (CAV2018)
Introduction
Design and Analysis of Centrifugal Compressors
Extended Surfaces
Thermal Management of Microelectronic Equipment