Analysis of multi-plane PIV measurements in a turbulent boundary layer: large scale structures, coupled and decoupled motions

Size: px
Start display at page:

Download "Analysis of multi-plane PIV measurements in a turbulent boundary layer: large scale structures, coupled and decoupled motions"

Transcription

1 Perry Fest 2004 Queen s University, Kingston Analysis of multi-plane PIV measurements in a turbulent boundary layer: large scale structures, coupled and decoupled motions Ivan Marusic, Nick Hutchins, Will Hambleton, Ellen Longmire, Bharath Ganapathisubramani Department of Aerospace Engineering and Mechanics University of Minnesota Supported by the National Science Foundation David and Lucile Packard Foundation

2

3

4 Head & Bandyopadhyay (1981) R θ = deg 135 deg R θ = 9400

5 Inclined-plane stereo PIV configuration (b) 45 case 135 case

6 In plane measured components u, v, w are transformed into streamwise, spanwise and wall-normal velocities

7 Both inclination angles repeated at four different Reynolds numbers 45 case 135 case Re τ = 790 Re τ = 1140 Re τ = 2030 Re τ = 3071

8 Comparison of mean flow parameters with data from (-) Klebanoff (1954) and (- -) Spalart (1988).

9 Wall-parallel plane set-up

10 Wall-parallel plane R uu z + = 92 R uu z + = 530

11 Two-point correlation maps all three planes stacked together Re τ 1100

12 Two-point correlation maps all three planes stacked together Re τ 1100

13 Two-point correlation maps all three planes stacked together Re τ 1100

14 Two-point correlation maps all three planes stacked together Re τ 1100

15 Two-point correlation maps all three planes stacked together Re τ 1100

16 Two-point correlation maps all three planes stacked together Re τ 1100

17 Two-point correlation maps all three planes stacked together Re τ 1100

18 Two-point correlation maps all three planes stacked together Re τ 1100

19 Two-point correlation maps all three planes stacked together Re τ 1100

20 Two-point correlation maps all three planes stacked together Re τ 1100

21 Two-point correlation maps all three planes stacked together Re τ 1100

22 Two-point correlation maps all three planes stacked together Re τ 1100

23 Two-point correlation maps all three planes stacked together Re τ 1100 Note: positive correlations extend further in the z direction for the 45 than for the 135 case

24 Two-point correlation maps all three planes stacked together Re τ 1100 Note: positive correlations extend further in the z direction for the 45 than for the 135 case

25 This is due to inclined nature of the large-scale events Christensen s two-point correlations from streamwise / wall-normal plane PIV measurements

26 z + = 92 z/δ = 0.5

27

28 Coupled Decoupled

29 Re τ = 790, 1140, 2030, 3071

30 Marusic & Perry (1995) Adrian, Meinhart & Tomkins (2000)

31 All of the above is consistent with the scenario of packets of hairpin vortices Adrian, Meinhart & Tomkins (2000)

32 Instantaneous wall-parallel plane data Automated feature-extraction algorithm Ganapathisubramani, Longmire and Marusic, JFM 2003 z + = 92: packets contribute 27% of <-uw>, occupy 4% of area z + = 150: packets contribute 24% of <-uw>, occupy 4.5% of area NB: positive and negative uw included in %

33 Instantaneous swirl result plane 135

34 Instantaneous swirl result plane 135 Low-speed region

35 Instantaneous swirl result plane 135 flanked by +ve swirls

36 Instantaneous swirl result plane 135 and by -ve swirls

37 Instantaneous swirl result plane 135

38 Instantaneous swirl result - 45 plane Note: decreased occurrence of swirl over the 135 plane 45

39 The hairpin packet model to explain the increased occurrence of swirl in the 135 plane over the 45 case.

40 The hairpin packet model to explain the increased occurrence of swirl in the 135 plane over the 45 case. Low-speed region

41 Comparison of RMS swirl in the 45 and 135 planes.

42 Head & Bandyopadhyay (1981) R θ = deg 135 deg R θ = 9400

43 Conclusions Inclined 45 deg. and 135 deg. PIV shows clear evidence of inclined eddies. Two point correlation functions from multi-plane stereo PIV measurements indicate existence of long narrow coherent structures, with characteristics consistent with packets of hairpin eddies in log. region of boundary layer. Near-wall region, including log region, is characterized by wallcoupled or attached structures, while outer wake region is characterized by decoupled structures. Consistent with notion of wall-wake eddy models.

44

Coherent structures in turbulent boundary layers with adverse pressure gradients

Coherent structures in turbulent boundary layers with adverse pressure gradients Journal of Turbulence Vol. 11, No. 28, 21, 1 2 Coherent structures in turbulent boundary layers with adverse pressure gradients Jin Lee, Jae Hwa Lee, Joung-Ho Lee and Hyung Jin Sung Department of Mechanical

More information

PECASE: MULTI-SCALE EXPERIMENTS AND MODELING

PECASE: MULTI-SCALE EXPERIMENTS AND MODELING PECASE: MULTI-SCALE EXPERIMENTS AND MODELING IN WALL TURBULENCE AFOSR # FA9550-09-1-0701 (P.M. J. Schmisseur) Beverley J. McKeon Graduate Aerospace Laboratories California Institute of Technology http://mckeon.caltech.edu

More information

Predictive Inner-Outer Model for Turbulent Boundary Layers Applied to Hypersonic DNS Data

Predictive Inner-Outer Model for Turbulent Boundary Layers Applied to Hypersonic DNS Data 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 07-10 January 2013, Grapevine (Dallas/Ft. Worth Region), Texas AIAA 2013-0265 Predictive Inner-Outer Model

More information

SURFACE SHEAR STRESS FLUCTUATIONS IN THE ATMOSPHERIC SURFACE LAYER

SURFACE SHEAR STRESS FLUCTUATIONS IN THE ATMOSPHERIC SURFACE LAYER Proceedings of the Eleventh Asian Congress of Fluid Mechanics 22-25 May 2006, Kuala Lumpur, Malaysia SURFACE SHEAR STRESS FLUCTUATIONS IN THE ATMOSPHERIC SURFACE LAYER J. P. Monty [montyjp@unimelb.edu.au]

More information

Effect of Wall Temperature and Mach Number on the Turbulence Structure of Hypersonic Boundary Layers

Effect of Wall Temperature and Mach Number on the Turbulence Structure of Hypersonic Boundary Layers 47th AIAA Aerospace Sciences Meeting and Exhibit, January 5 8, 2009/Orlando, FL Effect of Wall Temperature and Mach Number on the Turbulence Structure of Hypersonic Boundary Layers I. Beekman, S. Priebe,

More information

UNIVERSITY OF MINNESOTA. This is to certify that I have examined this bound copy of a doctoral thesis by. Bharathram Ganapathisubramani

UNIVERSITY OF MINNESOTA. This is to certify that I have examined this bound copy of a doctoral thesis by. Bharathram Ganapathisubramani UNIVERSITY OF MINNESOTA This is to certify that I have examined this bound copy of a doctoral thesis by Bharathram Ganapathisubramani and have found that it is complete and satisfactory in all respects,

More information

Characterization of the Turbulence Structure in Supersonic Boundary Layers using DNS Data

Characterization of the Turbulence Structure in Supersonic Boundary Layers using DNS Data Characterization of the Turbulence Structure in Supersonic Boundary Layers using DNS Data Matthew J. Ringuette, M. Pino Martín, Aleander J. Smits, and Minwei Wu Mechanical and Aerospace Engineering Department

More information

Preliminary Study of the Turbulence Structure in Supersonic Boundary Layers using DNS Data

Preliminary Study of the Turbulence Structure in Supersonic Boundary Layers using DNS Data 35th AIAA Fluid Dynamics Conference, June 6 9, 2005/Toronto,Canada Preliminary Study of the Turbulence Structure in Supersonic Boundary Layers using DNS Data Ellen M. Taylor, M. Pino Martín and Alexander

More information

Interfaces of uniform momentum zones in turbulent boundary layers

Interfaces of uniform momentum zones in turbulent boundary layers J. Fluid Mech. (217), vol. 82, pp. 451 478. c Cambridge University Press 217 doi:1.117/jfm.217.197 451 Interfaces of uniform momentum zones in turbulent boundary layers Charitha M. de Silva 1,, Jimmy Philip

More information

The mean velocity profile in the smooth wall turbulent boundary layer : 1) viscous sublayer

The mean velocity profile in the smooth wall turbulent boundary layer : 1) viscous sublayer The mean velocity profile in the smooth wall turbulent boundary layer : 1) viscous sublayer u = τ 0 y μ τ = μ du dy the velocity varies linearly, as a Couette flow (moving upper wall). Thus, the shear

More information

Direct Numerical Simulations of Hypersonic Turbulent Boundary Layers

Direct Numerical Simulations of Hypersonic Turbulent Boundary Layers Direct Numerical Simulations of Hypersonic Turbulent Boundary Layers M. Pino Martín University of Maryland Aerospace Engineering Department UM Institute for Advanced Computing Studies Tutorial School on

More information

TURBULENCE IN ENGINEERING APPLICATIONS II INSTANTANEOUS FIELDS IN WALL-BOUNDED TURBULENCE

TURBULENCE IN ENGINEERING APPLICATIONS II INSTANTANEOUS FIELDS IN WALL-BOUNDED TURBULENCE TURBULENCE IN ENGINEERING APPLICATIONS II INSTANTANEOUS FIELDS IN WALL-BOUNDED TURBULENCE OUTLINE Introduction Review of the state of the art data and scaling Modeling of observations: what do the models

More information

Direct numerical simulation of hypersonic turbulent boundary layers with varying freestream Mach number

Direct numerical simulation of hypersonic turbulent boundary layers with varying freestream Mach number 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 4-7 January 2, Orlando, Florida AIAA 2-353 Direct numerical simulation of hypersonic turbulent boundary layers

More information

TURBULENT BOUNDARY LAYERS: CURRENT RESEARCH AND FUTURE DIRECTIONS

TURBULENT BOUNDARY LAYERS: CURRENT RESEARCH AND FUTURE DIRECTIONS TURBULENT BOUNDARY LAYERS: CURRENT RESEARCH AND FUTURE DIRECTIONS Beverley J. McKeon Graduate Aerospace Laboratories California Institute of Technology http://mckeon.caltech.edu * AFOSR #s FA9550-08-1-0049,

More information

HORSEHOE VORTICES IN UNIFORMLY SHEARED TURBULENCE

HORSEHOE VORTICES IN UNIFORMLY SHEARED TURBULENCE HORSEHOE VORTICES IN UNIFORMLY SHEARED TURBULENCE Christina Vanderwel Department of Mechanical Engineering University of Ottawa Ottawa, Ontario, Canada cvand072@uottawa.ca Stavros Tavoularis Department

More information

Spanwise structure and scale growth in turbulent boundary layers

Spanwise structure and scale growth in turbulent boundary layers J. Fluid Mech. (2003), vol. 490, pp. 37 74. c 2003 Cambridge University Press DOI: 10.1017/S0022112003005251 Printed in the United Kingdom 37 Spanwise structure and scale growth in turbulent boundary layers

More information

A predictive inner outer model for streamwise turbulence statistics in wall-bounded flows

A predictive inner outer model for streamwise turbulence statistics in wall-bounded flows J. Fluid Mech. (211), vol. 681, pp. 537 566. c Cambridge University Press 211 doi:1.117/jfm.211.216 537 A predictive inner outer model for streamwise turbulence statistics in wall-bounded flows ROMAIN

More information

Statistical and structural similarities between micro- and macroscale wall turbulence

Statistical and structural similarities between micro- and macroscale wall turbulence Microfluid Nanofluid (27) 3: 89 DOI.7/s44-6-5-8 RESEARCH PAPER V. K. Natrajan Æ E. Yamaguchi Æ K. T. Christensen Statistical and structural similarities between micro- and macroscale wall turbulence Received:

More information

CHARACTERISTICS OF MOMENTUM SOURCES AND SINKS IN TURBULENT CHANNEL FLOW

CHARACTERISTICS OF MOMENTUM SOURCES AND SINKS IN TURBULENT CHANNEL FLOW CHARACTERISTICS OF MOMENTUM SOURCES AND SINKS IN TURBULENT CHANNEL FLOW J. P. Monty 1 & J. C. Klewicki 2 Department of Mechanical Engineering, University of Melbourne, Parkville, Australia 1 montyjp@unimelb.edu.au

More information

A comparison of turbulent pipe, channel and boundary layer flows

A comparison of turbulent pipe, channel and boundary layer flows J. Fluid Mech. (29), vol. 632, pp. 431 442. c 29 Cambridge University Press doi:1.117/s2211297423 Printed in the United Kingdom 431 A comparison of turbulent pipe, channel and boundary layer flows J. P.

More information

Planar imaging measurements to study the effect of spanwise structure of upstream turbulent boundary layer on shock induced separation

Planar imaging measurements to study the effect of spanwise structure of upstream turbulent boundary layer on shock induced separation 44th AIAA Aerospace Sciences Meeting and Exhibit 9-2 January 26, Reno, Nevada AIAA 26-324 Planar imaging measurements to study the effect of spanwise structure of upstream turbulent boundary layer on shock

More information

Towards Reconciling the Large-Scale Structure of Turbulent Boundary Layers in the Atmosphere and Laboratory

Towards Reconciling the Large-Scale Structure of Turbulent Boundary Layers in the Atmosphere and Laboratory Boundary-Layer Meteorol (2012) 145:273 306 DOI 10.1007/s10546-012-9735-4 ARTICLE Towards Reconciling the Large-Scale Structure of Turbulent Boundary Layers in the Atmosphere and Laboratory Nicholas Hutchins

More information

THE STRUCTURE OF ZERO, FAVORABLE AND ADVERSE PRESSURE GRADIENT TURBULENT BOUNDARY LAYERS

THE STRUCTURE OF ZERO, FAVORABLE AND ADVERSE PRESSURE GRADIENT TURBULENT BOUNDARY LAYERS THE STRUCTURE OF ZERO, FAVORABLE AND ADVERSE PRESSURE GRADIENT TURBULENT BOUNDARY LAYERS Zambri Harun Dept. of Mechanical Engineering The University of Melbourne Victoria 3, Australia zambriharun@yahoo.com

More information

Experimental study on the role of spanwise vorticity and vortex

Experimental study on the role of spanwise vorticity and vortex Experimental study on the role of spanwise vorticity and vortex filaments in the outer region of open-channel flow QIGANG CHEN, PhD Student, Department of Hydraulic Engineering, Tsinghua University, Beijing

More information

Structure of turbulent flow over regular arrays of cubical roughness

Structure of turbulent flow over regular arrays of cubical roughness Structure of turbulent flow over regular arrays of cubical roughness Journal: Manuscript ID: mss type: Date Submitted by the Author: Complete List of Authors: Keyword: Journal of Fluid Mechanics JFM-6-S-35.R3

More information

Flow topology and non-local geometry of structures in a flat-plate turbulent boundary layer

Flow topology and non-local geometry of structures in a flat-plate turbulent boundary layer Center for Turbulence Research Proceedings of the Summer Program 2010 65 Flow topology and non-local geometry of structures in a flat-plate turbulent boundary layer By I. Bermejo-Moreno, C. Atkinson, S.

More information

Attached Eddy Model of Wall Turbulence

Attached Eddy Model of Wall Turbulence Annu. Rev. Fluid. Mech. 2019. 51:49 74 Annual Review of Fluid Mechanics Attached Eddy Model of Wall Turbulence Ivan Marusic and Jason P. Monty Department of Mechanical Engineering, The University of Melbourne,

More information

Two-dimensional energy spectra in high-reynolds-number turbulent boundary layers

Two-dimensional energy spectra in high-reynolds-number turbulent boundary layers J. Fluid Mech. (217), vol. 826, R1, doi:1.117/jfm.217.359 journals.cambridge.org/rapids Two-dimensional energy spectra in high-reynolds-number turbulent boundary layers Dileep Chandran 1,, Rio Baidya 1,

More information

The logarithmic region of wall turbulence: Universality, structure and interactions

The logarithmic region of wall turbulence: Universality, structure and interactions 8th Australasian Fluid Mechanics Conference Launceston, Australia 3-7 December 22 The logarithmic region of wall turbulence: Universality, structure and interactions Ivan Marusic Department of Mechanical

More information

Coherent structures in flow over hydraulic engineering surfaces

Coherent structures in flow over hydraulic engineering surfaces This article was downloaded by: [IAHR ] On: 11 October 2012, At: 15:33 Publisher: Taylor & Francis Informa Ltd Registered in England and Wales Registered Number: 1072954 Registered office: Mortimer House,

More information

Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature

Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature J. Fluid Mech. (21), vol. 655, pp. 419 445. c Cambridge University Press 21 doi:1.117/s221121959 419 Direct numerical simulation of hypersonic turbulent boundary layers. Part 2. Effect of wall temperature

More information

The logarithmic region of wall turbulence: Universality, structure and interactions

The logarithmic region of wall turbulence: Universality, structure and interactions 8th Australasian Fluid Mechanics Conference Launceston, Australia 3-7 December 22 The logarithmic region of wall turbulence: Universality, structure and interactions Ivan Marusic Department of Mechanical

More information

On coherent structure in wall turbulence

On coherent structure in wall turbulence Under consideration for publication in J. Fluid Mech. 1 On coherent structure in wall turbulence A. S. S H A R M A 1 A N D B. J. M c K E O N 2 arxiv:1301.7580v2 [physics.flu-dyn] 17 Jun 2013 1 Aerodynamics

More information

The role of coherent structures in subgrid-scale energy transfer within the log layer of wall turbulence

The role of coherent structures in subgrid-scale energy transfer within the log layer of wall turbulence PHYSICS OF FLUIDS 18, 065104 2006 The role of coherent structures in subgrid-scale energy transfer within the log layer of wall turbulence V. K. Natrajan and K. T. Christensen a Department of Theoretical

More information

Studies of the large-scale structure in adiabatic and moderately-wall-heated subsonic boundary layers

Studies of the large-scale structure in adiabatic and moderately-wall-heated subsonic boundary layers June 30 - July 3, 2015 Melbourne, Australia 9 7A-3 Studies of the large-scale structure in adiabatic and moderately-wall-heated subsonic boundary layers Stanislav Gordeyev Department of Aerospace and Mechanical

More information

arxiv: v1 [physics.flu-dyn] 5 May 2017

arxiv: v1 [physics.flu-dyn] 5 May 2017 This draft was prepared using the LaTeX style file belonging to the Journal of Fluid Mechanics arxiv:75.23v [physics.flu-dyn] 5 May 27 Two-dimensional energy spectra in high Reynolds number turbulent boundary

More information

Structure of high and low shear-stress events in a turbulent boundary layer

Structure of high and low shear-stress events in a turbulent boundary layer Structure of high and low shear-stress events in a turbulent boundary layer G. Gomit, R. de Kat and B. Ganapathisubramani Engineering and the environment, University of Southampton, Southampton, SO17 1BJ,

More information

Current Status of Basic Research in Hypersonic Turbulence

Current Status of Basic Research in Hypersonic Turbulence 39th AIAA Fluid Dynamics Conference and Exhibit, January 5 8 2009, Orlando FL Current Status of Basic Research in Hypersonic Turbulence Alexander J. Smits, 1 M. Pino Martin 1 and Sharath Girimaji 2 1 Princeton

More information

Very large-scale structures observed in DNS of turbulent channel flow with passive scalar transport

Very large-scale structures observed in DNS of turbulent channel flow with passive scalar transport 5 th Australasian Fluid Mechanics Conference 3-7 December 4 Very large-scale structures observed in DNS of turbulent channel flow with passive scalar transport H. Kawamura, H. Abe and Y. Matsuo Department

More information

High Reynolds number effects in wall turbulence

High Reynolds number effects in wall turbulence High Reynolds number effects in wall turbulence Ivan Marusic Department of Mechanical Engineering, University of Melbourne, Victoria 3, Australia imarusic@unimelb.edu.au Nicholas Hutchins Department of

More information

Towards capturing large scale coherent structures in boundary layers using particle image velocimetry.

Towards capturing large scale coherent structures in boundary layers using particle image velocimetry. 7th Australian Conference on Laser Diagnostics in Fluid Mechanics and Combustion Melbourne, Australia 9- December 25 Towards capturing large scale coherent structures in boundary layers using particle

More information

UNIVERSITY OF SOUTHAMPTON. Effects of Large-Scale Free-Stream Turbulence on a Zero-Pressure-Gradient Turbulent Boundary Layer.

UNIVERSITY OF SOUTHAMPTON. Effects of Large-Scale Free-Stream Turbulence on a Zero-Pressure-Gradient Turbulent Boundary Layer. UNIVERSITY OF SOUTHAMPTON FACULTY OF ENGINEERING AND THE ENVIRONMENT Aerodynamics and Flight Mechanics Research Group Effects of Large-Scale Free-Stream Turbulence on a Zero-Pressure-Gradient Turbulent

More information

Boundary Layer Interactions

Boundary Layer Interactions Unsteadiness Unsteadiness of of Shock Shock Wave Wave / / Turbulent Turbulent Boundary Layer Interactions Noel Clemens Department of Aerospace Engineering and Engineering Mechanics The University of Texas

More information

Progress in Pipe and Channel Flow Turbulence,

Progress in Pipe and Channel Flow Turbulence, Progress in Pipe and Channel Flow Turbulence, 1961-211 John Kim Department of Mechanical & Aerospace Engineering University of California, Los Angeles TCM 211, Marseille, France September 26-3, 211 Outline

More information

STRUCTURE OF HIGH REYNOLDS NUMBER ADVERSE PRESSURE GRADIENT TURBULENT BOUNDARY LAYER

STRUCTURE OF HIGH REYNOLDS NUMBER ADVERSE PRESSURE GRADIENT TURBULENT BOUNDARY LAYER STRUCTURE OF HIGH REYNOLDS NUMBER ADVERSE PRESSURE GRADIENT TURBULENT BOUNDARY LAYER Murat Tutkun,, William K. George, Michel Stanislas Norwegian Defence Research Establishment (FFI), P.O. Box 25, 227

More information

ROLE OF LARGE SCALE MOTIONS IN TURBULENT POISEUILLE AND COUETTE FLOWS

ROLE OF LARGE SCALE MOTIONS IN TURBULENT POISEUILLE AND COUETTE FLOWS 10 th International Symposium on Turbulence and Shear Flow Phenomena (TSFP10), Chicago, USA, July, 2017 ROLE OF LARGE SCALE MOTIONS IN TURBULENT POISEUILLE AND COUETTE FLOWS Myoungkyu Lee Robert D. Moser

More information

Regularity diagnostics applied to a turbulent boundary layer

Regularity diagnostics applied to a turbulent boundary layer Center for Turbulence Research Proceedings of the Summer Program 208 247 Regularity diagnostics applied to a turbulent boundary layer By H. J. Bae, J. D. Gibbon, R. M. Kerr AND A. Lozano-Durán Regularity

More information

Hairpin vortices in turbulent boundary layers

Hairpin vortices in turbulent boundary layers Journal of Physics: Conference Series OPEN ACCESS Hairpin vortices in turbulent boundary layers To cite this article: G Eitel-Amor et al 14 J. Phys.: Conf. Ser. 56 18 Recent citations - On the near-wall

More information

Laminar and turbulent comparisons for channel flow and flow control

Laminar and turbulent comparisons for channel flow and flow control J. Fluid Mech. (2007), vol. 570, pp. 467 477. c 2007 Cambridge University Press doi:10.1017/s0022112006003247 Printed in the United Kingdom 467 Laminar and turbulent comparisons for channel flow and flow

More information

Analysis of Shock Motion in STBLI Induced by a Compression Ramp Configuration Using DNS Data

Analysis of Shock Motion in STBLI Induced by a Compression Ramp Configuration Using DNS Data 45th AIAA Aerospace Science Meeting and Exhibit, January 8 11, 25/Reno, Nevada Analysis of Shock Motion in STBLI Induced by a Compression Ramp Configuration Using DNS Data M. Wu and M.P. Martin Mechanical

More information

FLOW-NORDITA Spring School on Turbulent Boundary Layers1

FLOW-NORDITA Spring School on Turbulent Boundary Layers1 Jonathan F. Morrison, Ati Sharma Department of Aeronautics Imperial College, London & Beverley J. McKeon Graduate Aeronautical Laboratories, California Institute Technology FLOW-NORDITA Spring School on

More information

The evolution and interaction of two shock-accelerated, unstable gas cylinders

The evolution and interaction of two shock-accelerated, unstable gas cylinders The evolution and interaction of two shock-accelerated, unstable gas cylinders Chris Tomkins, Kathy Prestridge, Paul Rightley, Mark Marr-Lyon, Robert Benjamin Summer students: James Doyle and Michael Schneider

More information

Journal of Fluid Science and Technology

Journal of Fluid Science and Technology Science and Technology LDV and PIV Measurements of the Organized Oscillations of Turbulent Flow over a Rectangular Cavity* Takayuki MORI ** and Kenji NAGANUMA ** **Naval Systems Research Center, TRDI/Ministry

More information

The Urban Canopy and the Plant Canopy

The Urban Canopy and the Plant Canopy The Urban Canopy and the Plant Canopy John Finnigan: CSIRO Australia Margi Bohm: University of Canberra Roger Shaw: U C Davis Ned Patton: NCAR Ian Harman: CSIRO Australia www.csiro.au Properties of turbulent

More information

Patterns of Turbulence. Dwight Barkley and Laurette Tuckerman

Patterns of Turbulence. Dwight Barkley and Laurette Tuckerman Patterns of Turbulence Dwight Barkley and Laurette Tuckerman Plane Couette Flow Re = U gap/2 ν Experiments by Prigent and Dauchot Re400 Z (Spanwise) 40 24 o Gap 2 Length 770 X (Streamwise) Examples: Patterns

More information

Computing Turbulent Channels at Experimental Reynolds Numbers

Computing Turbulent Channels at Experimental Reynolds Numbers 15th Australasian Fluid Mechanics Conference The University of Sydney, Sydney, Australia 13-17 December 2004 Computing Turbulent Channels at Experimental Reynolds Numbers J. Jiménez 1,2 and J.C. del Álamo

More information

Control of a Particle-Laden Jet Using a Piezo-electric Actuator

Control of a Particle-Laden Jet Using a Piezo-electric Actuator Control of a Particle-Laden Jet Using a Piezo-electric Actuator by Stamatios Pothos and Ellen K. Longmire 2 TSI Incorporated, P.O. BOX 6424, St. Paul, MN 5564 2 Department of Aerospace Engineering & Mechanics,

More information

HISTORY EFFECTS FOR CAMBERED AND SYMMETRIC

HISTORY EFFECTS FOR CAMBERED AND SYMMETRIC HISTORY EFFECTS FOR CAMBERED AND SYMMETRIC WING PROFILES A. Tanarro, R. Vinuesa and P. Schlatter Linné FLOW Centre, KTH Mechanics and Swedish e-science Research Centre (SeRC), SE-1 44 Stockholm, Sweden

More information

TODAY A very brief introduction to measuring turbulent flows... To back up some techniques used in papers today...

TODAY A very brief introduction to measuring turbulent flows... To back up some techniques used in papers today... TODAY A very brief introduction to measuring turbulent flows... To back up some techniques used in papers today... see last weeks handout for fuller list Laboratory 1. Flow Visualisation - dye, particles

More information

Effects of large-scale free stream turbulence on a turbulent boundary layer

Effects of large-scale free stream turbulence on a turbulent boundary layer Effects of large-scale free stream turbulence on a turbulent boundary layer Nicole S. Sharp Cornell University Presented in partial completion of the requirements for the degree of Master of Science in

More information

I C E T. (International Collaboration on Experiments in Turbulence)

I C E T. (International Collaboration on Experiments in Turbulence) I C E T (International Collaboration on Experiments in Turbulence) Coordinated Measurements in High Reynolds Number Turbulent Boundary Layers from Three Wind Tunnels Hassan Nagib IIT Alexander Smits Princeton

More information

Analysis of shock motion in shockwave and turbulent boundary layer interaction using direct numerical simulation data

Analysis of shock motion in shockwave and turbulent boundary layer interaction using direct numerical simulation data J. Fluid Mech. (8), vol. 594, pp. 7 8. c 8 Cambridge University Press doi:.7/s7944 Printed in the United Kingdom 7 Analysis of shock motion in shockwave and turbulent boundary layer interaction using direct

More information

COUPLING A BOUNDARY LAYER WALL SHEAR-STRESS MODEL WITH FIELD EXPERIMENTS IN A SHALLOW TIDAL RIVER

COUPLING A BOUNDARY LAYER WALL SHEAR-STRESS MODEL WITH FIELD EXPERIMENTS IN A SHALLOW TIDAL RIVER COUPLING A BOUNDARY LAYER WALL SHEAR-STRESS MODEL WITH FIELD EXPERIMENTS IN A SHALLOW TIDAL RIVER Romain Mathis Laboratoire de Mécanique de Lille CNRS UMR 87, Université Lille Nord de France 96 Villeneuve

More information

A PIV study of flow over interacting Barchan dunes

A PIV study of flow over interacting Barchan dunes A PIV study of flow over interacting Barchan dunes Jessica A. Palmer 1, Ricardo Mejia-Alvarez 2, Eric M. Rivera 3, James L. Best 4 and Kenneth T. Christensen 5 1: Department of Geology, University of Illinois,

More information

The role of coherent structures in subfilter-scale dissipation of turbulence measured in the atmospheric surface layer

The role of coherent structures in subfilter-scale dissipation of turbulence measured in the atmospheric surface layer JOT J OURNAL OF TURBULENCE http://jot.iop.org/ The role of coherent structures in subfilter-scale dissipation of turbulence measured in the atmospheric surface layer Matthew A Carper 1 and Fernando Porté-Agel

More information

The B009 data in the backward facing step experiment Report on the Data Analysis and evaluation

The B009 data in the backward facing step experiment Report on the Data Analysis and evaluation Communications on Hydraulic and Geotechnical Engineering 2004-05 ISSN 0169-6548 The B009 data in the backward facing step experiment Report on the Data Analysis and evaluation Nguyen Thanh Hoan* November

More information

Spatial resolution correction for wall-bounded turbulence measurements

Spatial resolution correction for wall-bounded turbulence measurements J. Fluid Mech. (11), vol. 7, pp. 1 3. c Cambridge University Press 11 doi:1.117/jfm.11.19 1 Spatial resolution correction for wall-bounded turbulence measurements A. J. SMITS 1, J. MONTY, M. HULTMARK 1,

More information

Direct and Large Eddy Simulation of stably stratified turbulent Ekman layers

Direct and Large Eddy Simulation of stably stratified turbulent Ekman layers Direct and Large Eddy Simulation of stably stratified turbulent Ekman layers Stimit Shah, Elie Bou-Zeid Princeton University 64 th APS DFD Baltimore, Maryland Nov 21, 211 Effect of Stability on Atmospheric

More information

A dynamic global-coefficient subgrid-scale eddy-viscosity model for large-eddy simulation in complex geometries

A dynamic global-coefficient subgrid-scale eddy-viscosity model for large-eddy simulation in complex geometries Center for Turbulence Research Annual Research Briefs 2006 41 A dynamic global-coefficient subgrid-scale eddy-viscosity model for large-eddy simulation in complex geometries By D. You AND P. Moin 1. Motivation

More information

ANALYSIS OF SHOCK MOTION IN STBLI USING DNS DATA

ANALYSIS OF SHOCK MOTION IN STBLI USING DNS DATA ANALYSIS OF SHOCK MOTION IN STBLI USING DNS DATA Minwei Wu and Pino Martin Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ 8544, USA * Abstract Direct numerical

More information

Toward low order models of wall turbulence using resolvent analysis

Toward low order models of wall turbulence using resolvent analysis Center for Turbulence Research Proceedings of the Summer Program 2016 305 Toward low order models of wall turbulence using resolvent analysis By K. Rosenberg, T. Saxton-Fox, A. Lozano-Durán, A. Towne AND

More information

Active drag reduction in a turbulent boundary layer based on plasma-actuatorgenerated streamwise vortices

Active drag reduction in a turbulent boundary layer based on plasma-actuatorgenerated streamwise vortices June 30 - July 3, 015 Melbourne, Australia 9 9A-5 Active drag reduction in a turbulent boundary layer based on plasma-actuatorgenerated streamwise vortices Chi Wai Wong, Yu Zhou, Yinzhe Li and Yupeng Li

More information

Project MaKoS - Manipulation and Control of Turbulent Flow

Project MaKoS - Manipulation and Control of Turbulent Flow DLR.de Page 1 Presentation MaKoS 05.12.2017 Project MaKoS - Manipulation and Control of Turbulent Flow Christina Voß, Markus Rütten Institute of Aerodynamics and Flow Technology Göttingen DLR - German

More information

Proceedings of the 4th Joint US-European Fluids Engineering Division Summer Meeting ASME-FEDSM2014 August 3-7, 2014, Chicago, Illinois, USA

Proceedings of the 4th Joint US-European Fluids Engineering Division Summer Meeting ASME-FEDSM2014 August 3-7, 2014, Chicago, Illinois, USA Proceedings of the 4th Joint US-European Fluids Engineering Division Summer Meeting ASME-FEDSM4 August 3-7, 4, Chicago, Illinois, USA FEDSM4-38 SUPPRESSION OF UNSTEADY VORTEX SHEDDING FROM A CIRCULAR CYLINDER

More information

SCALE INTERACTIONS IN THE FAR-FIELD OF A TURBULENT MIXING LAYER

SCALE INTERACTIONS IN THE FAR-FIELD OF A TURBULENT MIXING LAYER August 8-3, 3 Poitiers, France SCALE INTERACTIONS IN THE FAR-FIELD OF A TURBULENT MIXING LAYER Oliver R.H. Buxton Department of Aeronautics Imperial College London, UK o.buxton@imperial.ac.uk Bharathram

More information

Coherent structures and wall-pressure fluctuations modeling in turbulent boundary layers subjected to pressure gradients

Coherent structures and wall-pressure fluctuations modeling in turbulent boundary layers subjected to pressure gradients Coherent structures and wall-pressure fluctuations modeling in turbulent boundary layers subjected to pressure gradients Miloud Alaoui To cite this version: Miloud Alaoui. Coherent structures and wall-pressure

More information

Quantitative characterization of coherent structures in the buffer layer of near-wall turbulence. Part 1: streaks

Quantitative characterization of coherent structures in the buffer layer of near-wall turbulence. Part 1: streaks Exp Fluids (28) 45:999 3 DOI.7/s348-8-522-4 RESEARCH ARTICLE Quantitative characterization of coherent structures in the buffer layer of near-wall turbulence. Part : streaks J. Lin Æ J. P. Laval Æ J. M.

More information

ASSESSMENT OF TURBULENT BOUNDARY LAYERS ON A NACA4412 WING SECTION AT MODERATE Re

ASSESSMENT OF TURBULENT BOUNDARY LAYERS ON A NACA4412 WING SECTION AT MODERATE Re ASSESSMENT OF TURBULENT BOUNDARY LAYERS ON A NACA4412 WING SECTION AT MODERATE Re R. Vinuesa 1, S. M. Hosseini 1, A. Hanifi 1,2, D. S. Henningson 1 and P. Schlatter 1 1 Linné FLOW Centre, KTH Mechanics,

More information

Roughness Sub Layers John Finnigan, Roger Shaw, Ned Patton, Ian Harman

Roughness Sub Layers John Finnigan, Roger Shaw, Ned Patton, Ian Harman Roughness Sub Layers John Finnigan, Roger Shaw, Ned Patton, Ian Harman 1. Characteristics of the Roughness Sub layer With well understood caveats, the time averaged statistics of flow in the atmospheric

More information

Near Field Measurements of an Axisymmetric Turbulent Jet at Low Reynolds Numbers: A PIV and CTA Comparison

Near Field Measurements of an Axisymmetric Turbulent Jet at Low Reynolds Numbers: A PIV and CTA Comparison Near Field Measurements of an Axisymmetric Turbulent Jet at Low Reynolds Numbers: A PIV and CTA Comparison 1 Brian D. Landers, 2 Peter J. Disimile 1,2 Department of Aerospace Engineering, University of

More information

Turbulence Laboratory

Turbulence Laboratory Objective: CE 319F Elementary Mechanics of Fluids Department of Civil, Architectural and Environmental Engineering The University of Texas at Austin Turbulence Laboratory The objective of this laboratory

More information

Control of Flow over a Bluff Body

Control of Flow over a Bluff Body Annu. Rev. Fluid Mech. 2008 40 1056-8700/97/0610-00 Control of Flow over a Bluff Body Haecheon Choi 1,2, Woo-Pyung Jeon 1 and Jinsung Kim 1 1 School of Mechanical and Aerospace Engineering, Seoul National

More information

Investigation of the development of streamwise vortices from vortex generators in APG separation control using PIV

Investigation of the development of streamwise vortices from vortex generators in APG separation control using PIV Investigation of the development of streamwise vortices from vortex generators in APG separation control using PIV by K. P. Angele (1) and F. Grewe () (1) Department of Mechanics, KTH S-100 44 Stockholm,

More information

arxiv: v1 [physics.flu-dyn] 4 Aug 2014

arxiv: v1 [physics.flu-dyn] 4 Aug 2014 A hybrid RANS/LES framework to investigate spatially developing turbulent boundary layers arxiv:1408.1060v1 [physics.flu-dyn] 4 Aug 2014 Sunil K. Arolla a,1, a Sibley School of Mechanical and Aerospace

More information

arxiv: v1 [physics.flu-dyn] 10 Dec 2018

arxiv: v1 [physics.flu-dyn] 10 Dec 2018 REVISITING THE AMPLITUDE MODULATION IN WALL-BOUNDED TURBULENCE: TOWARDS A ROBUST DEFINITION Eda Dogan 1, Ramis Örlü 1, Davide Gatti 2, Ricardo Vinuesa 1 and Philipp Schlatter 1 1 Linné FLOW Centre, KTH

More information

SG Turbulence models for CFD

SG Turbulence models for CFD SG2218 2012 Turbulence models for CFD Stefan Wallin Linné FLOW Centre Dept of Mechanics, KTH Dept. of Aeronautics and Systems Integration, FOI There are no simple turbulent flows Turbulent boundary layer:

More information

Direct numerical simulation of a self-similar adverse pressure gradient turbulent boundary layer at the verge of separation

Direct numerical simulation of a self-similar adverse pressure gradient turbulent boundary layer at the verge of separation J. Fluid Mech. (217), vol. 829, pp. 392 419. c Cambridge University Press 217 doi:1.117/jfm.217.549 392 Direct numerical simulation of a self-similar adverse pressure gradient turbulent boundary layer

More information

Forcing large-scale coherent streaks in a zero pressure gradient turbulent boundary layer. Abstract

Forcing large-scale coherent streaks in a zero pressure gradient turbulent boundary layer. Abstract Forcing large-scale coherent streaks in a zero pressure gradient turbulent boundary layer Gregory Pujals, 1, 2 Carlo Cossu, 3 and Sebastien Depardon 2 1 LadHyX, CNRS-École Polytechnique, F-91128 Palaiseau,

More information

PIV measurements of turbulence in an inertial particle plume in an unstratified ambient

PIV measurements of turbulence in an inertial particle plume in an unstratified ambient PIV measurements of turbulence in an inertial particle plume in an unstratified ambient D.B. Bryant & S.A. Socolofsky Zachry Department of Civil Engineering, Texas A&M University, USA ABSTRACT: A high-speed

More information

The development of turbulent pipe flow

The development of turbulent pipe flow 16th Australasian Fluid Mechanics Conference Crown Plaza, Gold Coast, Australia 2-7 December 2007 The development of turbulent pipe flow J. Doherty, P.Ngan, J. Monty, M. Chong Department of Mechanical

More information

CHARACTERIZATION OF THE SECONDARY FLOW IN TURBULENT RECTANGULAR DUCTS WITH VARYING ASPECT RATIO

CHARACTERIZATION OF THE SECONDARY FLOW IN TURBULENT RECTANGULAR DUCTS WITH VARYING ASPECT RATIO June - July, 21 Melbourne, Australia 9 8A-1 CHARACTERIZATION OF THE SECONDARY FLOW IN TURBULENT RECTANGULAR DUCTS WITH VARYING ASPECT RATIO Ricardo Vinuesa Linné FLOW Centre, KTH Mechanics SE-1 Stockholm,

More information

Visualization of wall turbulence under artificial disturbance by piezo actuator array

Visualization of wall turbulence under artificial disturbance by piezo actuator array Visualization of wall turbulence under artificial disturbance by piezo actuator array By Takehiko Segawa *, Peiwen Li **, Yasuo Kawaguchi * and Hiro Yoshida * *Mechanical Engineering Laboratory, AIST MITI,

More information

elements remain in high frequency region and sometimes very large spike-shaped peaks appear. So we corrected the PIV time histories by peak cutting an

elements remain in high frequency region and sometimes very large spike-shaped peaks appear. So we corrected the PIV time histories by peak cutting an The Seventh International Colloquium on Bluff Body Aerodynamics and Applications (BBAA7) Shanghai, China; September 2-6, 2012 LES of fluctuating wind pressure on a 3D square cylinder for PIV-based inflow

More information

Convection in Three-Dimensional Separated and Attached Flow

Convection in Three-Dimensional Separated and Attached Flow Convection in Three-Dimensional Separated and Attached Flow B. F. Armaly Convection Heat Transfer Laboratory Department of Mechanical and Aerospace Engineering, and Engineering Mechanics University of

More information

Numerical Simulation of Freestream Acoustic Disturbances in Hypersonic Ground Facilities and Their Effect on Boundary Layer Transition

Numerical Simulation of Freestream Acoustic Disturbances in Hypersonic Ground Facilities and Their Effect on Boundary Layer Transition Numerical Simulation of Freestream Acoustic Disturbances in Hypersonic Ground Facilities and Their Effect on Boundary Layer Transition PI: Lian Duan --- YIP FA9550-14-1-0170 --- Missouri U. of S&T Project

More information

AN INVESTIGATION OF THE REYNOLDS NUMBER DEPENDENCE OF THE NEAR- WALL PEAK IN CANONICAL WALL BOUNDED TURBULENT CHANNEL FLOW

AN INVESTIGATION OF THE REYNOLDS NUMBER DEPENDENCE OF THE NEAR- WALL PEAK IN CANONICAL WALL BOUNDED TURBULENT CHANNEL FLOW University of Kentucky UKnowledge University of Kentucky Master's Theses Graduate School 2011 AN INVESTIGATION OF THE REYNOLDS NUMBER DEPENDENCE OF THE NEAR- WALL PEAK IN CANONICAL WALL BOUNDED TURBULENT

More information

Turbulent boundary layer over a three-dimensional rough wall

Turbulent boundary layer over a three-dimensional rough wall Turbulent boundary layer over a three-dimensional rough wall Gaetano Maria Di Cicca 1, Andrea Ferrari 2, Michele Onorato 3 1 Dipartimento di Ingegneria Meccanica e Aerospaziale, Politecnico di Torino,

More information

Active Control of Turbulence and Fluid- Structure Interactions

Active Control of Turbulence and Fluid- Structure Interactions Bonjour! Active Control of Turbulence and Fluid- Structure Interactions Yu Zhou Institute for Turbulence-Noise-Vibration Interaction and Control Shenzhen Graduate School, Harbin Institute of Technology

More information

2 Structure functions of boundary layer and pipe flow

2 Structure functions of boundary layer and pipe flow Exp Fluids (5) 5: DOI.7/s3-5-99-7 RESEARCH ARTICLE On the universality of inertial energy in the log layer of turbulent boundary layer and pipe flows D. Chung I. Marusic J. P. Monty M. Vallikivi A. J.

More information

Dual Vortex Structure Shedding from Low Aspect Ratio, Surface-mounted Pyramids

Dual Vortex Structure Shedding from Low Aspect Ratio, Surface-mounted Pyramids Dual Vortex Structure Shedding from Low Aspect Ratio, Surface-mounted Pyramids Robert J. Martinuzzi Department of Mechanical and Manufacturing Engineering Schulich School of Engineering University of Calgary

More information