FINAL REPORT. Office of Naval Research. entitled. Anatol Roshko Theodore Von Karman Professor of Aeronautics

Similar documents
Structure and mixing of a transverse jet in incompressible flow

Curriculum Vitae of Sergio Pirozzoli

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

Vortex Induced Vibrations

Module 3: Velocity Measurement Lecture 15: Processing velocity vectors. The Lecture Contains: Data Analysis from Velocity Vectors

U U Technical Monitor

LDA-Measurements of Jets in Crossflow for Effusion Cooling Applications

Studies on the Transition of the Flow Oscillations over an Axisymmetric Open Cavity Model

This paper is part of the following report: UNCLASSIFIED

Journal of Fluid Science and Technology

PROPERTIES OF THE FLOW AROUND TWO ROTATING CIRCULAR CYLINDERS IN SIDE-BY-SIDE ARRANGEMENT WITH DIFFERENT ROTATION TYPES

Validation 3. Laminar Flow Around a Circular Cylinder

TIME-AVERAGED PHENOMENOLOGICAL INVESTIGATION OF A WAKE BEHIND A BLUFF BODY

The Computations of Jet Interaction on a Generic Supersonic Missile

DIRECT NUMERICAL SIMULATIONS OF HIGH SPEED FLOW OVER CAVITY. Abstract

POTENTIAL TURBULENCE MODEL PREDICTIONS OF FLOW PAST A TRIANGULAR CYLINDER USING AN UNSTRUCTURED STAGGERED MESH METHOD

Applied Thermal and Fluid Engineering. Energy Engineering (Thermal Engineering Laboratory)

4' DTIC. ,.94 jl _ AD-A I ELEC -, ANNUAL REPORT 1 OCT 92 THROUGH 30 SEPT 93 C OFFICE OF NAVAL RESEARCH OCEAN TECHNOLOGY PROGRAM

J. Fluid Meeh. (1974). vol. 64, part 4, pp Printed in Great Britain 775 On density effects and large structure in turbulent mixing layers By

TURBULENT VORTEX SHEDDING FROM TRIANGLE CYLINDER USING THE TURBULENT BODY FORCE POTENTIAL MODEL

Numerical Study of Natural Unsteadiness Using Wall-Distance-Free Turbulence Models

Lecture 7. Turbulence

Experimental characterization of flow field around a square prism with a small triangular prism

Analysis of a Dual-Mode Scramjet Engine Isolator Operating From Mach 3.5 to Mach 6

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

UWE has obtained warranties from all depositors as to their title in the material deposited and as to their right to deposit such material.

On the flow interactions of multiple jets in cross-flow

FEDSM COMPUTATIONAL AEROACOUSTIC ANALYSIS OF OVEREXPANDED SUPERSONIC JET IMPINGEMENT ON A FLAT PLATE WITH/WITHOUT HOLE

AEROACOUSTIC INVESTIGATION OF THE EFFECT OF A DETACHED FLAT PLATE ON THE NOISE FROM A SQUARE CYLINDER

Numerical Investigation of the Transonic Base Flow of A Generic Rocket Configuration

International Conference on Methods of Aerophysical Research, ICMAR 2008

Laboratory Studies of Fire Whirls (preliminary)

DYNAMIC SEPARATION CONTROL IN A LOW-SPEED ASYMMETRIC DIFFUSER WITH VARYING DOWNSTREAM BOUNDARY CONDITION

CHARACTERISTICS OF ELLIPTIC CO-AXIAL JETS

Introduction to Turbulence AEEM Why study turbulent flows?

Tandem Spheres: Motivation and Case Specification

PIV measurements of cold flow field in a partially premixed bluff body burner M. Dutka, 1, M. Ditaranto 2, T. Løvås 1

LARGE-SCALE COHERENT TURBULENCE STRUCTURES IN A COMPRESSIBLE MIXING LAYER FLOW

TURBINE BURNERS: Engine Performance Improvements; Mixing, Ignition, and Flame-Holding in High Acceleration Flows

Numerical Investigation of Thermal Performance in Cross Flow Around Square Array of Circular Cylinders

Simulation of Flow around a Surface-mounted Square-section Cylinder of Aspect Ratio Four

Turbulent shear-layer mixing: growth-rate compressibility scaling

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

Dynamic Pressure Characterization of a Dual-Mode Scramjet

Numerical investigation of swirl flow inside a supersonic nozzle

CFD Simulation of Internal Flowfield of Dual-mode Scramjet

A comparison of turbulence models for an impinging jet in a crossflow

Module 2: External Flows Lecture 12: Flow Over Curved Surfaces. The Lecture Contains: Description of Flow past a Circular Cylinder

A Pair of Large-incidence-angle Cylinders in Cross-flow with the Upstream One Subjected to a Transverse Harmonic Oscillation

Drag on flat plates of arbitrary porosity

EFFECT OF CARBON DIOXIDE, ARGON AND HYDROCARBON FUELS ON THE STABILITY OF HYDROGEN JET FLAMES

Initiation of stabilized detonations by projectiles

Experimental investigation of flow control devices for the reduction of transonic buffeting on rocket afterbodies

Publication 97/2. An Introduction to Turbulence Models. Lars Davidson, lada

Detailed Outline, M E 521: Foundations of Fluid Mechanics I

Vortex wake and energy transitions of an oscillating cylinder at low Reynolds number

Simulation of Turbulent Lifted Flames and their Transient Propagation

NUMERICAL SIMULATION OF THE FLOW AROUND A SQUARE CYLINDER USING THE VORTEX METHOD

1. Introduction, tensors, kinematics

Vortex-Array Model of a Shear Layer Perturbed by a Periodically Pitching Airfoil

The Effect of Endplates on Rectangular Jets of Different Aspect Ratios

Effect of Mach number on Wall Pressure Flow Field for Area Ratio 2.56

Chapter 6 An introduction of turbulent boundary layer

Theoretical Gas Flow through Gaps in Screw-type Machines

Observations of supersonic free shear layers

Shock induced boundary layer separation and associated unsteadiness

CFD Analysis of Micro-Ramps for Hypersonic Flows Mogrekar Ashish 1, a, Sivakumar, R. 2, b

Vortex shedding from slender surface mounted pyramids

Experimental Analysis on Incompressible circular and noncircular Fluid Jet through Passive Control Method

Chapter 5 Phenomena of laminar-turbulent boundary layer transition (including free shear layers)

FLUID MECHANICS. ! Atmosphere, Ocean. ! Aerodynamics. ! Energy conversion. ! Transport of heat/other. ! Numerous industrial processes

LES of an auto-igniting C 2 H 4 flame DNS

BLUFF-BODY AERODYNAMICS

Corrugated Tabs for Supersonic Jet Control (Keynote Paper)

FLUID MECHANICS. Atmosphere, Ocean. Aerodynamics. Energy conversion. Transport of heat/other. Numerous industrial processes

A STUDY OF GASEOUS TRANSVERSE INJECTION AND MIXING PROCESS IN A SIMULATED ENGINE INTAKE PORT

Turbulent Boundary Layers & Turbulence Models. Lecture 09

Separation Control on High Lift Low-Pressure Turbine Airfoils Using Pulsed Vortex Generator Jets

Numerical modelling for assessment of wind flow pattern and wind load on a rectangular cylinder for different aspect ratios

Evolution of large eddies in compressible shear layers

Numerical Investigation of a Transverse Jet in a Supersonic Crossflow Using Large Eddy Simulation

Impact of numerical method on auto-ignition in a temporally evolving mixing layer at various initial conditions

arxiv:physics/ v1 [physics.flu-dyn] 14 Mar 2000 Wavelet Cross-Correlation Analysis of Turbulent Mixing from Large-Eddy-Simulations

Boundary-Layer Theory

Lecture 9 Laminar Diffusion Flame Configurations

Experimental Study of Near Wake Flow Behind a Rectangular Cylinder

Syllabus for AE3610, Aerodynamics I

Computational Investigations of High-Speed Dual-Stream Jets

Turbulence Instability

Modelling Nozzle throat as Rocket exhaust

EXPERIMENTAL INVESTIGATION ON THE NONCIRCULAR INCOMPRESSIBLE JET CHARACTERISTICS

VISCID/INVISCID INTERACTION ANALYSIS OF EJECTOR WINGS. M. Bevilaqua, C. J. Woan, and E. F. Schum

Step-Wake Stabilized Jet Diffusion Flame in a Transverse Air Stream

Experimental Aerodynamics. Experimental Aerodynamics

Rayleigh-Taylor Unstable Flames



NANOPARTICLE COAGULATION AND DISPERSION IN A TURBULENT PLANAR JET WITH CONSTRAINTS

OTIC AD-A ATION PAGE1 S EECTE IJ. OLD DOMINION UNIVERSITYREOTNMR 46TH STREET & COLLEY AVENUE NORFOLD VA, Al SR*TR.

THE STRUCTURE OF FLOW FIELD IN SMALL SIZE VORTEX FLOW METERS

Transcription:

to F11 F rnpv FINAL REPORT 4to Office of Naval Research on Contract No. N00014-85-C-0646 Work Unit No. 4328-434 entitled STRUCTURE AND MIXING IN TURBULENT SHEAR FLOWS 1 July 1985-31 October 1988 Anatol Roshko Theodore Von Karman Professor of Aeronautics Graduate Aeronautical Laboratories. California Institute of Technology Pasadena, California 2 1 FEB Ing A Y. napproved i :.;. a -r,, r': c 'crd atile; itsl 89 2 j071..........., n t~ ro e

-2- SUMMARY The research problems in turbulent mixing studied under this contract were the following: Supersonic turbulent mixing layers) j. Transverse jets I,!'. Burning free jets Theoretical models Significant results obtained are briefly summarized in the fogwing Discussion. Complete descriptions of the research and of the results are contained in the references cited... --- DISCUSSION Supersonic Turbulent Mixing Layers The relationships of large structures and growth rate to convective Mach number M, were further investigated. Measurements of large-scale structure convective velocity, by double-exposure spark Schlieren photography, showed that entrainment may be unexpectedly asymmetric at high values of M,, where compressibility has a large reducing effect on growth rate. The investigations are reported and described in the following publications and contributions. Publications in refereed journals D. Papamoschou and A. Roshko 1988 Observations of supersonic free shear layers. Sadhana, J. Indian Academy of Sciences, 12, Feb., 1-14. D. Papamoschou and A. Roshko, 1988 "The turbulent compressible shear layer: An experimental study," J. Fluid Mechanics 197, 453-477. D. Papamoschou, 1988 "Diffuser performance of two-stream supersonic wind tunnels," accepted for publication in the AIAA Journal. D. Papamoschou, 1988 "A two-spark schlieren system for very-high velocity measurements," submitted for publication to Experiments in Fluids.

-3- Invited and contributed reports D. Papamoschou, "Outstanding issues in the area of compressible mixing," Invited Lecture at the International Workshop on the Physics of Compressible Mixing, Princeton University, October 1988. D. Papamoschou, "Structure of the Compressible Turbulent Shear Layer," AIAA 89-0126 presented at the AIAA 27th Aerospace Sciences Meeting, January, 1989. Transverse Jets New insights were obtained into the large vortical structure in turbulent jets injected into a uniform cross flow. A train of trailing vortices, which are quite intense under some conditions, has been discovered in the wake of such a transverse jet. This is reminiscent of the vortex street behind a solid cylinder but has a very different genesis. It is not a result of "vortex shedding" off the cylindrical jet but originates in the boundary layer of the wall from which the jet issues, after a complex process of unsteady separation and convection in the field of the jet. Publications T. Fric and A. Roshko 1988 "Views of the transverse jet near field," Physics of Fluids, 31, no. 9, Sept., 2390. T. Fric and A. Roshko 1988 "Structure in the near field of the transverse jet". Submitted to the Symposium on Turbulent Shear Flows, Stanford University, 21-23 August, 1989. Burning Free Jets A mechanism has been proposed in which the stability of a lifted turbulent jet flame is determined by the strain between large-scale structures in the jet flow field. A model has been developed using simple chemistry and large-scale flow parameters which provides u linear relationship between the liftoff height and the jet exit velocity for a simple non-coflowing axisymmetric jet flame. This model agrees well with our experimentally measured liftoff heights for a variety of pure fuels. The fluctuations in liftoff height measured in the present study are consistent with flame propagation from one large-scale structure to its upstream neighbor, and provide evidence that large-scale dynamics determne the stabilization condition.

-4- Contributed Reports Richard C. Miake-Lye and Jay A. Hammer 1988 Lifted turbulent jet flames; a stability criterion based on the jet large-scale structure. Presented at the 22nd International Symposium on Combustion, 14-19 August, Seattle, Washington. Theoretical Models t A model of turbulent mixing and chemical reaction product in turbulent jets and mixing layers has been formulated. It is based on the concept that molecular mixing occurs during and at the end of cascades from the largest to the smallest scales in the flow. Molecular transport comes into play in the "flame sheets" that form between reactant streams, and it is in these effects that the model predictions differ significantly from models based on mean-flow gradient diffusion concepts. It explains the experimentally observed effects of Reynolds number, Schmidt number and Damk6hler number. It is found that Reynolds number influences the effective reaction rate for Re as high as 106 and that the reaction rate becomes mixing limited for values of the Damk6hler number, based on time of flight to the measuring station and the overall reaction time, of about 40. The model contains two physical constants, with clear physical meaning, that are determined from experiment. The crucial role of Taylor scale (in addition to Kolmogoraff scale) is demonstrated. Contributed Reports J.E. Broadwell and M.G. Mungal 1988 "Molecular mixing and chemical reactions in turbulent shear layers." Presented at the 22nd International Symposium on Combustion, 14-19 August, Seattle, Washington. J.E. BroadweU 1988 "A model for reactions in turbulent jets: effects of Reynolds, Schmidt, and Damk6hler numbers." In: Proceedings of the July 1987 U.S.-France Workshop, Turbulent Reactive Rows, Vol. 1, Springer-Verlag. J.E. Broadwell 1988 "Molecular mixing and chemical reactions in turbulent shear flows." In: Disorder and Mixing, E. Guyon, Y. Pomeau, E. Charlaix, J.-P. Nadal, eds., Kiuwer Publishing, in press.

-5- Other Publications and Reports Cimbala, J., Nagib, H. and Roshko, A. 1985 "Large Structure in the Far Wakes of Two-Dimensional Bluff Bodies". J. Fluid Mechanics 190, 265-298. Bemal, L.P. and Roshko, A. 1986 Streamwise vortex structure in plane mixing layers". J. Fluid Mechanics 170, 499-525. Bemal, L.P. 1988 The statistics of the organized vortical structure in turbulent mixing layers. Physics of Fluids 31, no. 9, September, 2533-2543. 7~ / Z -3G 13 _..-. ~ 1j?...,