On the Instantaneous Dynamics of the Large- Scale Structures In The Impinging Round Jet J. W. Hall & D. Ewing Department of Mechanical Engineering, McMaster.

Slides:



Advertisements
Similar presentations
P.W. Terry K.W. Smith University of Wisconsin-Madison Outline
Advertisements

Presented at NATO ASI May 2004 Solar-induced thermal effects on the flow in a street canyon Eric Savory Advanced Fluids Mechanics Research Group Dept of.
LARGE-EDDY SIMULATION and LAGRANGIAN TRACKING of a DIFFUSER PRECEDED BY A TURBULENT PIPE Sep 07, 2006 Fabio Sbrizzai a, Roberto Verzicco b and Alfredo.
Jonathan Morrison Beverley McKeon Dept. Aeronautics, Imperial College
University of Western Ontario
ON WIDTH VARIATIONS IN RIVER MEANDERS Luca Solari 1 & Giovanni Seminara 2 1 Department of Civil Engineering, University of Firenze 2 Department of Environmental.
On-Set of EHD Turbulence for Cylinder in Cross Flow Under Corona Discharges J.S. Chang, D. Brocilo, K. Urashima Dept. of Engineering Physics, McMaster.
Large roofs and sports stadiums
Direct numerical simulation study of a turbulent stably stratified air flow above the wavy water surface. O. A. Druzhinin, Y. I. Troitskaya Institute of.
Using wavelet tools to estimate and assess trends in atmospheric data Peter Guttorp University of Washington NRCSE.
An Experimental Investigation of Turbulent Boundary Layer Flow over Surface-Mounted Circular Cavities Jesse Dybenko Eric Savory Department of Mechanical.
Anisotropic Pressure and Acceleration Spectra in Shear Flow Yoshiyuki Tsuji Nagoya University Japan Acknowledgement : Useful discussions and advices were.
Experimental investigations of the flow during the stage separation of a space transportation system Andrew Hay Aerospace Engineering with German.
Dr. Laila Guessous Suresh Putta, M.S. Student Numerical Investigations of Pulsatile Flows To develop a better understanding of the characteristics of pulsating.
Evidence for a mixing transition in fully-developed pipe flow Beverley McKeon, Jonathan Morrison DEPT AERONAUTICS IMPERIAL COLLEGE.
Analysis of multi-plane PIV measurements in a turbulent boundary layer: large scale structures, coupled and decoupled motions Ivan Marusic, Nick Hutchins,
L ehrstuhl für Modellierung und Simulation UNIVERSITY of ROSTOCK | CHAIR OF MODELLING AND SIMULATION Physics of turbulence Lecture 2.
Dominant spanwise Fourier modes in the log and wake regions of the turbulent boundary layer Nick Hutchins, Ivan Marusic and Bharathram Ganapathisubramani.
Wind noise in hearing aids
THE AUSTRALIAN NATIONAL UNIVERSITY Infrasound Technology Workshop, 3-7 November 2008, Bermuda WIND NOISE REDUCTION AT IMS INFRASOUND STATIONS Douglas R.
Wind loading and structural response Lecture 18 Dr. J.D. Holmes
Development of Synthetic Air Jet Technology for Applications in Electronics Cooling Dr. Tadhg S. O’Donovan School of Engineering and Physical Sciences.
Computational Modeling of Turbulent Asymmetric Jet Flows Prof. Ed Akin Mechanical Engineering and Materials Science Rice University Houston, Texas Jon.
School of Aeronautical Engineering, Queen’s University Belfast Turbulent Wind Flow over a High Speed Train R K Cooper School of Aeronautical Engineering.
A H. Kyotoh, b R. Nakamura & a P. J. Baruah a a Institute of Engineering Mechanics and Systems, University of Tsukuba, Ibaraki, Japan b Third Plan Design.
The 2 nd Cross-Strait Symposium on Dynamical Systems and Vibration December 2012 Spectrum Characteristics of Fluctuating Wind Pressures on Hemispherical.
I.Z. Naqavi 1, E. Savory 1 & R.J. Martinuzzi 2 1 Advanced Fluid Mechanics Research Group Department of Mechanical and Materials Engineering The University.
Ye Zhao, Zhi Yuan and Fan Chen Kent State University, Ohio, USA.
Study of Oscillating Blades from Stable to Stalled Conditions 1 CFD Lab, Department of Aerospace Engineering, University of Glasgow 2 Volvo Aero Corporation.
Basic bluff-body aerodynamics II
Aerodynamic measurement of high-speed base flows Background The separated wake at the base of cylindrical bodies presents a number of challenges to aerodynamic.
Flow Control over Swept Edges Demetri Telionis Dept. of Engineering Science and Mechanics.
Computing Internal and External Flows Undergoing Instability and Bifurcations V. V. S. N. Vijay, Neelu Singh and T. K. Sengupta High Performance Computing.
Fluid Mechanics Laboratory University of Kentucky Active Control of Separation on a Wing with Conformal Camber David Munday and Jamey Jacob Department.
1 LES of Turbulent Flows: Lecture 15 (ME EN ) Prof. Rob Stoll Department of Mechanical Engineering University of Utah Fall 2014.
Experimental investigations on secondary structures in a fully developed turbulent jet and extension to fibre-laden case Alessandro Capone, Alfredo Soldati.
1 LES of Turbulent Flows: Lecture 16 (ME EN ) Prof. Rob Stoll Department of Mechanical Engineering University of Utah Fall 2014.
LES of Turbulent Flows: Lecture 2 (ME EN )
Turbulence effects on particle dispersion in a free-surface flow
1 Reduced-Order Modeling in the Frequency Domain for Actuated Flows Guy Ben-Dov* and Arne J. Pearlstein Department of Mechanical Science and Engineering.
Infrasounds and Background Free Oscillations Naoki Kobayashi [1] T. Kusumi and N. Suda [2] [1] Tokyo Tech [2] Hiroshima Univ.
U NIVERSITY OF S CIENCE AND T ECHNOLOGY OF C HINA CAS K EY L ABORATORY OF B ASIC P LASMA P HYSICS Recent experimental results of zonal flows in edge tokamak.
The Stability of Laminar Flows - 2
STABLY STRATIFIED SHEAR-PRODUCED TURBULENCE AND LARGE-SCALE-WAVES IN A LID DRIVEN CAVITY BEN-GURION UNIVERSITY OF THE NEGEV FACULTY OF ENGINEERING SCIENCES.
IT SB RAS1 DMD analysis of coherent structures in a turbulent forced jet S.S. Abdurakipov, V.M. Dulin, D.M. Markovich Institute of Thermophysics, Novosibirsk,
Chapter 3. Instability of the free plane and near – wall plane jet
Chapter 2. Physical processes responsible for evolution and downstream breakdown of a subsonic round jet Multimedia files Nos. 2.1 – 2.8 The results of.
Intermittency Analysis and Spatial Dependence of Magnetic Field Disturbances in the Fast Solar Wind Sunny W. Y. Tam 1 and Ya-Hui Yang 2 1 Institute of.
A comparative study of plane and radial turbulent wall jets
MITE Mixing Control of Fuel Jets Using Synthetic Jet Technology: Velocity Field Measurements Staci A. Davis and Ari Glezer Woodruff School of Mechanical.
Steps in Development of 2 D Turbine Cascades P M V Subbarao Professor Mechanical Engineering Department A Classical Method Recommended by Schlichting.……
Relativistic MHD Simulations of jets Relativistic MHD Simulations of jets Abstract We have performed 3D RMHD simulations to investigate the stability and.
Turbulent Convection and Anomalous Cross-Field Transport in Mirror Plasmas V.P. Pastukhov and N.V. Chudin.
Spatial Evolution of Resonant Harmonic Mode Triads in a Blasius Boundary Layer 37th AIAA Fluid Dynamics Conference and Exhibit José B. Dávila Department.
Interaction between vortex flow and microturbulence Zheng-Xiong Wang (王正汹) Dalian University of Technology, Dalian, China West Lake International Symposium.
Theory of Turbine Cascades P M V Subbarao Professor Mechanical Engineering Department Its Group Performance, What Matters.……
Vertical Axis Wind Turbine Noise
Spatial evolution of wall-imposed disturbance in pipe flow
Swirl intensity influence on interaction between non-swirling and swirling co-axial jets in a combustor configuration: LES and modelling study S. Šarić,
On the Hierarchical Scaling Behavior of Turbulent Wall-Flows
The application of an atmospheric boundary layer to evaluate truck aerodynamics in CFD “A solution for a real-world engineering problem” Ir. Niek van.
MAE 5130: VISCOUS FLOWS Introduction to Turbulent Flows
Experimental Characterization of Gas-Liquid Column:
COMPUTATIONAL MODELING OF PARTICLE TRANSPORT IN TURBULENT AIRFLOW
VORTICITY AND CIRCULATION WITHIN TWIN JETS ISSUING INTO A CROSSFLOW
Dept of Mechanical Engineering
Experimental and Numerical Investigation of Controlled, Small-Scale Motions in a Turbulent Shear Layer Bojan Vukasinovic, Ari Glezer Woodruff School of.
Analysis of the Gemini data
The formation of very long structures
Low-Re Separation Control by Periodic Suction Surface Motion
Presentation transcript:

On the Instantaneous Dynamics of the Large- Scale Structures In The Impinging Round Jet J. W. Hall & D. Ewing Department of Mechanical Engineering, McMaster University, Hamilton, Ontario, Canada

Perry Fest 2004 Kingston Turbulent Round Impinging Jet Flow visualization of impinging round jet, H/D=2.0, Re=20000, Popiel and Trass (1991).

Perry Fest 2004 Kingston Turbulent Plane Wall Jet Gogineni and Shih (1997)

Perry Fest 2004 Kingston Harvey and Perry’s Rebounding Vortex Harvey and Perry (1971)

Perry Fest 2004 Kingston Three-Dimensionality of Structures? Tsubokura (2003) Re=2,000 Forced at Strouhal Frequency Fully Developed Pipe Flow H/D = 9 Landreth and Adrian (1991) observed instantaneous flow was not symmetric in PIV measurements

Perry Fest 2004 Kingston Investigation of the Three-Dimensionality of Large-Scale Structures Hall et al (2002)

Perry Fest 2004 Kingston Effect of Nozzle-to-Plate Distance Jet Exiting a Long Pipe Re=23,000

Perry Fest 2004 Kingston Pressure Spectra

Perry Fest 2004 Kingston Azimuthal Spectra

Perry Fest 2004 Kingston Azimuthal Frequency Spectra, H/D=2.0 r/D=1.0 r/D=1.5

Perry Fest 2004 Kingston Two-Point, Two Time Correlations H/D=2.0 H/D=4.0 r 1 /D =1.0

Perry Fest 2004 Kingston Dynamics of the Instantaneous Structures Pressure sampled at 800Hz for 350 blocks of 400 data points  ESP scanner system at Boundary Layer Wind Tunnel, University of Western Ontario  Signals are phase corrected in post-processing Perform Proper Orthogonal Decomposition in Azimuthal Direction  Fourier Modes

Perry Fest 2004 Kingston Pressure Field, H/D=2.0 Mean Pressure Fluctuating Pressure

Perry Fest 2004 Kingston Comparison to microphone data Hall et al. (2003)

Perry Fest 2004 Kingston Pressure Spectra m=0 All modes

Perry Fest 2004 Kingston H/D=2.0 All modes m=0, +/-1 m=0

Perry Fest 2004 Kingston H/D=4.0 m=0, +/-1 All modes m=0 to +/-5

Perry Fest 2004 Kingston Impinging Jet DNS Tsubokura (2003) Re=2, 000 Forced at Strouhal Frequency H/D = 9 Satake and Kunugi (1998) Re=10000 H/D = 6, Confined Inlet Condition Fully Developed Pipe Flow

Perry Fest 2004 Kingston Wavelet Analysis: Instantaneous Pressure r/D=2.0 r/D=1.0 r/D=1.5 H/D=2

Perry Fest 2004 Kingston Wavelet Analysis: Azimuthal Modes All modes m=0 m=1 m=5 H/D =2, r/D =1.5

Perry Fest 2004 Kingston Wavelet Coefficients: Mode 0 r/D=2.0 r/D=1.0 r/D=1.5 H/D=2

Perry Fest 2004 Kingston Wavelet Coefficients: Mode 1 r/D=2.0 r/D=1.0 r/D=1.5 H/D=2

Perry Fest 2004 Kingston Azimuthal Mode 1: Precessing? r/D=1.0 r/D=1.5

Perry Fest 2004 Kingston Wavelet Analysis: Effect of H/D H/D =2, r/D =1.5 All modes m=0 m=1 m=5 H/D =4, r/D =1.5

Perry Fest 2004 Kingston Wavelet Analysis: Effect of H/D r/D =1.0 r/D =1.5 H/D=2.0 H/D=4.0

Perry Fest 2004 Kingston Concluding Remarks Measurements of the instantaneous wall pressure fluctuations were used to examine the development of the large-scale structures in the near field of the radial wall jet. The inclusion of at least azimuthal mode 1 was necessary to reasonable model the dynamics of the flow. Contributions from azimuthal mode 0 and 1 underwent variations in magnitude that persisted over periods corresponding to the passage of several structures. There were extended periods where the slope of the phase of mode 1 was linear suggesting there may be periods of jet precessing of varying duration and direction. Structures contributing to fluctuating wall pressure did not appear to become significantly more intermittent as H/D increased. There was less systematic variation of the phase of mode 1 as H/D increased suggesting less systematic jet precessing.