Cavitation Bubbles in a Starting Submerged Water Jet

Similar documents
HIGH-SPEED OBSERVATIONS OF SUBMERGED WATER JETS ISSUING FROM AN ABRASIVE WATER JET NOZZLE

DEVELOPMENTS IN PIPELINE FILLING AND EMPTYING EXPERIMENTATION IN A LABORATORY PIPELINE APPARATUS

A Study of Pressure Safety Valve Response Times under Transient Overpressures

Free Surface Flow Simulation with ACUSIM in the Water Industry

Application of vortex generators in ship propulsion system design M. Oledal

Lab # 03: Visualization of Shock Waves by using Schlieren Technique

The Discussion of this exercise covers the following points:

Effects of separation distance on the vortical behaviour of jetimpingement

EFFECT OF CORNER CUTOFFS ON FLOW CHARACTERISTICS AROUND A SQUARE CYLINDER

Observed in Gas Injection

FLUID FORCE ACTING ON A CYLINDRICAL PIER STANDING IN A SCOUR

THE BRIDGE COLLAPSED IN NOVEMBER 1940 AFTER 4 MONTHS OF ITS OPENING TO TRAFFIC!

THE INFLOW OF UNWANTED AIR

Experiment 8: Minor Losses

CFD Simulation and Experimental Validation of a Diaphragm Pressure Wave Generator

Citation Journal of Thermal Science, 18(4),

Development of High-speed Gas Dissolution Device

Vortex Flow Meter Wafer or Flange Connection. - Steam - Liquid - Gas

Numerical investigation on the cavitating flow in Annular Jet Pump under different flow rate ratio

Development of a Shock Loading Simulation Facility


The acoustic emissions of cavitation bubbles in stretched vortices

CHARACTERISTICS OF AN AIR-COATED ABRASIVE SUSPENSION JET UNDER SUBMERGED CONDITION

Applied Fluid Mechanics

Visual Observation of Nucleate Boiling and Sliding Phenomena of Boiling Bubbles on a Horizontal Tube Heater

Hydrogen Bubble Dispersion and Surface Bursting Behaviour

Evaluation of Cavitation in a Liquid-Liquid Ejector

A Computational Assessment of Gas Jets in a Bubbly Co-Flow 1

Experimental investigation of the check valve behaviour when the flow is reversing

EWGAE 2010 Vienna, 8th to 10th September

A & AE 520 Background Information, Adapted from AAE334L, last revised 10-Feb-14 Page 1 1. SUPERSONIC WIND TUNNEL

Experimental investigation on air entrainment below impinging jets by means of video observations and image processing

FLOW VISUALIZATION STUDY ON TWO-PHASE CRYOGENIC FLOW

CHARACTERISTICS OF BUBBLE SPLITTING IN A TIP VORTEX FLOW

The Discussion of this exercise covers the following points: Pumps Basic operation of a liquid pump Types of liquid pumps The centrifugal pump.

A model for the bubble lift-off diameter in subcooled boiling flow in a horizontal channel

Study on Intensity of Blast Wave Generated from Vessel Bursting by Gas Explosion

Control of Air Bubble Cluster by a Vortex Ring Launched into Still Water

ANTI SHOCK RELIEF VALVE

Influence of rounding corners on unsteady flow and heat transfer around a square cylinder

Injector Dynamics Assumptions and their Impact on Predicting Cavitation and Performance

Figure 1: Two possible mechanisms of cavitation erosion.

Smart Water Application Technologies (SWAT)

Theoretical Solution 1, 9 th Asian Physics Olympiad (Mongolia)

WATER HYDRAULIC HIGH SPEED SOLENOID VALVE AND ITS APPLICATION

Vortex Meters for Liquids, Gas, and Steam

LASER INDUCED FLUORESCENCE MEASUREMENTS OF CARBON DIOXIDE DISSOLUTION IN WAVE-BREAKING TURBULENCE

Plane Turbulent Wall Jets in Limited Tailwater Depth

Modeling of bubble generated noise in tip vortex cavitation inception

Experimental Verification of Integrated Pressure Suppression Systems in Fusion Reactors at In-Vessel Loss-of -Coolant Events

MODELING AND SIMULATION OF VALVE COEFFICIENTS AND CAVITATION CHARACTERISTICS IN A BALL VALVE

VORTEX SHEDDING AND VORTEX FORMATION FROM A PAIR OF IN-LINE FORCED OSCILLATING TANDEM ARRANGED CIRCULAR CYINDERS IN A UNIFORM FLOW

XCFD4NRS. Experiments and CFD Codes Application to Nuclear Reactor Safety. OECD/NEA & International Atomic Energy Agency (IAEA) Workshop

Laser-Induced Bubbles in Glycerol-Water Mixtures

The Characteristics of Cavitation Bubbles Induced by the Secondary Shock Wave in an HM-3 Lithotripter and Its Effect on Stone Comminution

EXPERIMENTAL VALIDATION OF BEM CODE ANALYSIS OF BUBBLE SPLITTING IN A TIP VORTEX FLOW

Flow transients in multiphase pipelines

AN ANALYSIS ON HIGH PRESSURE DYNAMIC CALIBRATORS USED IN THE DEFENSE AREAS

An Experimental Study of Cavity Shedding Mechanisms for Unsteady Cloud Cavitation

Casing wall static pressure distribution behavior in a centrifugal compressor with asymmetric inlet/outlet structures

NUMERICAL INVESTIGATION OF THE FLOW BEHAVIOUR IN A MODERN TRAFFIC TUNNEL IN CASE OF FIRE INCIDENT

A comparison of NACA 0012 and NACA 0021 self-noise at low Reynolds number

Restriction Orifice. Single or Multi Stage Orifice to. Reduce Pressure or. Limit the Flow Rate

A Study on the Effects of Wind on the Drift Loss of a Cooling Tower

ADVANCES in NATURAL and APPLIED SCIENCES

Investigation on Divergent Exit Curvature Effect on Nozzle Pressure Ratio of Supersonic Convergent Divergent Nozzle

THREE DIMENSIONAL STRUCTURES OF FLOW BEHIND A

(Refer Slide Time: 2:16)

AN EXPERIMENTAL INVESTIGATION OF SPILLING BREAKERS

2. Materials and Methods

AIR-WATER FLOW STRUCTURES AT AN ABRUPT DROP WITH SUPERCRITICAL FLOW

AIRFLOW GENERATION IN A TUNNEL USING A SACCARDO VENTILATION SYSTEM AGAINST THE BUOYANCY EFFECT PRODUCED BY A FIRE

Experimental Study of Flow around a Circular Cylinder inside a Bubble Plume

Flow behavior of wakes in a three-phase slurry bubble column with viscous liquid medium

Flow characteristics over forward facing step and through abrupt contraction pipe and drag reduction

Bubble-bubble interactions and wall pressures/temperatures produced by the collapse of a bubble pair near a rigid surface

An underwater explosion is an explosion where the point of detonation is below the surface of the water.

Results and Discussion for Steady Measurements

Laboratory studies of water column separation

HYDRAULICS. H89.8D - Hydraulic Bench

Sound scattering by hydrodynamic wakes of sea animals

5th Congress of Alps-Adria Acoustics Association CAVITATION NOISE PHENOMENA IN CENTRIFUGAL PUMPS

Energy and mass transfer in gas-liquid reactors.

IMPROVING PLANT AERATION USING GAS INFUSION TECHNOLOGY

Quantification of the Effects of Turbulence in Wind on the Flutter Stability of Suspension Bridges

Experimental study on path instability of rising bubbles

Bubble Elimination Device in Hydraulic Systems

Experimental Analysis on Vortex Tube Refrigerator Using Different Conical Valve Angles

Assumptions 1 At specified conditions, air behaves as an ideal gas. 2 The volume of the tire remains constant.

EXPERIMENTAL ANALYSIS OF THE CONFLUENT BOUNDARY LAYER BETWEEN A FLAP AND A MAIN ELEMENT WITH SAW-TOOTHED TRAILING EDGE

Investigation of Recirculation Effects on the Formation of Vapor Bubbles in Centrifugal Pump Blades

Chapter 3 EXPERIMENTAL: EQUIPMENT, SET-UP, AND PROCEDURE

SEMATECH Provisional Test Method for Pressure Cycle Testing Filter Cartridges Used in UPW Distribution Systems

Causes and Remedies to 7 Instability Patterns in Blown Film Extrusion

Acoustical approach to analysis of energy conversions in an oscillating bubble

Unsteady airfoil experiments

Numerical Simulations of a Train of Air Bubbles Rising Through Stagnant Water

EXPERIMENTAL ANALYSIS OF VAPOUR BUBBLE GROWING ON A HEATED SURFACE

World Academy of Science, Engineering and Technology International Journal of Mechanical and Mechatronics Engineering Vol:6, No:1, 2012

CIRCULATION PRODUCTION AND SHEDDING FROM VERTICAL AXIS WIND TURBINE BLADES UNDERGOING DYNAMIC STALL

Transcription:

CAV21:sessionA7.5 1 Cavitation Bubbles in a Starting Submerged Water Jet K.Nakano, M.Hayakawa, S.Fujikawa and T.Yano Graduate School of Engineering, Hokkaido University, Sapporo, Japan Abstract The behavior of cavitation bubbles in a starting submerged water jet discharging from a circular nozzle is studied by a simple photography technique in a moderately low range of jet exit velocity. A number of small spherical bubbles are initially generated in a starting vortex formed at the jet tip and often connected circumferentially with each other in the form similar to a vortex ring. Nearly axisymmetric lumps of disconnected bubbles are also observed frequently. By analyzing photographic data acquired from the side and end view pictures of the ring-like bubbles, their average properties, such as trajectory, geometry and size, are evaluated. 1. Introduction It is well known that the cavitation inception occurs when cavitation nuclei in a liquid are exposed to a sufficiently low pressure, comparable with the vapor pressure of the liquid, to cause their unstable and explosive growth (Arndt 1981; Brennen 1995). In submerged water jets where the mean static pressure is generally much higher than vapor pressure, the onset of cavitation is believed to take place in low pressure regions produced by vortical structures. Observations by Ooi(1985) and Gopalan et al.(1999) show that the cavitation inception in initially laminar jets does not occur in the cores of rolled-up vortices but in the cores of secondary vortices which are formed randomly. This suggests that the investigations of the generation process of bubbles are quite difficult in turbulent regions in jets. One of the approaches to circumvent the difficulty would be to deal with cavitating jet flows, where well-organized vortices are formed either periodically or reproducibly, such as in a self-excited jet (Chahine & Genoux 1983). In the present work, we employ an impulsively-started jet, where a starting vortex of the jet should produce nearly axisymmetric low pressure. This low pressure may lead to the formation of ring-like cavitation bubbles in the near field of the jet. We shall study the behavior of such ring-like cavities. 2. Experimental setup and conditions The experimental apparatus consists of a closed water reservoir connected to an air compressor, a water reservoir opened to the atmosphere, and a 15mm-diameter circular pipe connecting the two reservoirs, as shown in Fig.1. Water flow is operated by an electromagnetic valve and discharged into a still water from an orifice-type nozzle with the exit diameter of

CAV21:sessionA7.5 2 5mm. A piezoelectric pressure transducer with the resonance frequency of about 3kHz is mounted in the pipe at 65mm upstream the nozzle exit. The output signal of the transducer is used to measure the transient pressure change of water in the pipe, as well as to detect the onset of flow and to trigger a light source for photography. The light source is a flash light with the nominal lightening duration of.2 ms which is short enough for individual cavitation bubbles to be captured as still images in pictures under the present test conditions. Flow observations are made by two cameras; one is located just downstream and above the nozzle exit, and the other is outside the open reservoir and facing to the nozzle exit section. Experiments were performed for the gauge pressure level, p g, of the closed water reservoir in the range.3 -.5MPa, and the cross-sectional mean velocity, Uj, at the nozzle exit in the range 15.3-19.5m/s. The corresponding Reynolds numbers based on Uj and orifice diameter D(=5mm) are (7.5-1)x1 5. Tap water was used without any treatment for degassing, so that the dissolved air content would be in a nearly saturated condition. Water temperature was kept 2 3 C throughout the experiments. Figure 2 shows an example of the pressure transducer signal, where p* indicates the difference in water pressure across the nozzle, and the origin in time t is arbitrary. The mechanism of the electromagnetic valve used is such that as electric current is supplied, a subsidiary valve(called pilot valve ) opens first and a small amount of water discharges, and thereafter a main valve starts to open. Owing to this mechanism, p* shows first a bump and then a sharp rise, followed by a gradual increase to the maximum. Because the bump was found to appear reproducibly prior to the onset of the main flow, we used it as the trigger signal of flashing the light and also as the temporal origin in the results to be presented. 3. Results We visualized first starting vortices using dye-marked water. Soon after the flow was initiated, a mushroom-shaped concentration of dye was observed at the jet tip. When p g >.4MPa, the mush-room-shaped structure was followed by another large concentration of dye. These concentrations are both associated with starting vortices; that is, the leading one is due to the pilot valve opening and the second one to the main valve opening. Similar observations, repeatedly made by reducing the amount of dye, showed that spherical bubbles appear mostly in the leading and the second dye-concentrated regions, and tend to be aligned in the azimuthal direction to take a form similar to a ring. This suggests that the cavitation inception does occur inside the starting vortices. In later stages of jet development, smaller bubbles were found to be formed behind the starting vortices; some were in groups and the others were randomly distributed in the jet shear layer. In what follows, results obtained at p g =.5MPa will be presented, with primarily focusing on the behavior of ring-like lumps of bubbles. Some side-view pictures taken at different stages of jet development are shown in Figs. 3(a-d). We have confirmed from many close-up pictures that most of ring-like lumps of bubbles consist of a number of small and nearly spherical bubbles, and the shapes of lumps resemble rosaries or circular chains of beads, rather than azimuthally uniform rings. Ring-

CAV21:sessionA7.5 3 like lumps of disconnected bubbles were also observed frequently(see, for example, Fig.3c). Bubbles at the jet tip were even smaller and often isolated due to the comparatively weak circulation of the leading vortex caused by the pilot-valve opening. For convenience of description, the ring-like lump of bubbles, including disconnected ones, will be hereafter referred to as "bubble ring". Figures 4 shows the streamwise position of bubble rings as a function of time, where the leading and the second bubble rings are shown by triangles and circles, respectively. The leading and the second bubble rings move downstream with distictly different velocities; the former travels slower at roughly 4m/s and the latter at 1m/s in <8. When two bubble rings are successively formed, the second bubble ring catches up and interacts with the leading one at around =6(see, for example, Fig.3d). Observations of end-view pictures showed that almost all the bubble rings seldom maintain the axisymmetric shape as convected downstream, and often undergo a wavy deformation, probably reflecting the occurrence of the azimuthal instabillity of a vortex ring(widnall & Sullivan 1973). The bubble rings were found to persist downstream up to =15-2, but it was not clear to what extent they could survive, because of the increasing distortion and diffusion of bubble rings further downstream. Figures 5(a,b) show the streamwise variations of the average diameter D r and thickness d r of bubble rings, which were evaluated from the side- and/or end-view pictures. The diameter D r, which is initially close to the orifice diameter, increases with x in accordance with the vortex ring growth. The thickness of bubble rings appears to reach its maximum at =3-4, followed by a gradual decrease with increasing x. From D r and d r, we calculated the approximate volume V r of bubble ring, with assuming its geometry to be a torus. The result is shown in Fig.6, where V r is represented in a logarithmic scale. The volume exhibits a rapid increase up to about =3, beyond which it does not increases any further, in contrast to the continuous increase of the bubble ring diameter. Figure 7 shows the average diameter, d i, of individual bubbles forming a bubble ring. The typical size of bubbles contained in the bubble ring exhibits an abrupt increase soon after its formation, followed by a gradual decrease. These results indicate that outside the formation region, the evolution of bubble rings is not much affected by the dissolved air in water surrounding the jet flow. In particular, the approximately constant values of V r and d i in >5 suggest that no significant air entrainment occurs beyond the jet potential core during the evolution of bubble rings. 4. Conclusions Cavitation bubbles in a starting water jet were studied in a moderately low range of jet exit speed. The reproducible nature of the starting jet helped us to observe the behavior of bubbles by a simple photography technique. The main results are summarized as follows. (1) In early stages of jet development, cavitation bubbles are mostly generated inside the starting vortices and connected with each other in the form of a ring.

CAV21:sessionA7.5 4 (2) Once formed, the bubble rings travel downstream with the starting vortices and often survive beyond 2 times the nozzle diameter. (3) The average size of the individual bubbles forming the bubble rings quickly increases in the vicinity of nozzle and then gradually decreases as they travel downstream. (4) In later stages of jet development, isolated bubbles are formed behind the starting vortices; some are in groups and others are randomly distributed in the jet shear layer. The authors would like to thank Mr.Yutaka Nozaki for his help in constructing experimental facilities and devices. References Arndt,R.E.A 1981 Cavitation in fluid machinery and hydraulic structures. Ann.Rev. Fluid Mech. 13, 273-328. Brennen,C.E. 1995 Cavitation and Bubble Dynamics, Oxford University Press. Chahine,G.L and Genoux,Ph.F. 1983 Collapse of a cavitating vortex ring. J.Fluids Engg. 15, 4-45. Gopalan,S., Katz,J. and Knio,O. 1994 The flow structure in the near field of jets and its effect on cavitation inception. J.Fluid Mech.398, 1-43. Ooi,K.K. 1985 Scale effects on cavitation inception in submerged water jets: a new look. J.Fluid Mech. 151, 367-39. Widnall,S.E. and Sullivan,J.P. 1973 On the stability of vortex rings. Rroc.Roy.Soc. Lond. A 33, 335-353. (1) Closed water tank (2) Water reservoir (3) Air compressor (4) Pressure gauge (5) Water supply (6) Electromagnetic valve (7) Pressure sensor/ transducer (8) Orifice-type nozzle (9) Camera (1) Flash light (11) Pulse circuit Figure 1. Schematic of experimental setup.

CAV21:sessionA7.5 5 Figure 2. An example of pressure transducer signal; p g =.5MPa. a b Cc d Figure 3. Four examples showing bubble rings. Flow is from left to right.

CAV21:sessionA7.5 6 12 8 Figure 4. Streamwise position of bubble rings as a function of time. 4 5 1 15 t ms 4 3 Dr/D 2 1 2 4 8 12 dr mm 1 4 8 12 Figure 5. Diameter and thickness of bubble rings; (a) diameter, (b) thickness.

CAV21:sessionA7.5 7 1.E+3 1.E+2 Vr mm^3 1.E+1 1.E+ 1.E-1 4 8 12 Figure 6. Approximate volume of bubble rings..6.4 di mm.2 4 8 12 Figure 7. Average diameter of individual bubbles in bubble rings.