Background and Motivation

Size: px
Start display at page:

Download "Background and Motivation"

Transcription

1 Background and Motivation Cavitation has been investigated in a variety of flows: Tip vortices, e.g., Arndt et al. (1991), Arndt and Maines (2000), Hsiao et al. (2003). Lifting and curved surfaces, e.g., Leger and Ceccio (1998), Astolfi et al. (2000), Gopalan and Katz (2000). Free shear layers, e.g., Ooi and Acosta (1983), O Hern (1990), Ran and Katz(1994), Gopalan et al. (1999), Laberteaux and Ceccio (2001). Literature on cavitation for 2D turbulent shear layer flow past an open cavity is non-existent. Previous studies emphasized self-excited (self-sustained) oscillations of shear layer; (e.g., Rockwell and Knisely (1979), Tang and Rockwell (1983), Lin and Rockwell (2001), etc.); Lack of information on the pressure field and the associated occurrence of cavitation. Cavitation: Vaporization of liquid under the effect of depressurization (Brennen, 1995, Arndt, 2002). Knowledge of the pressure distribution is of fundamental importance for understanding the inception and subsequent develpoment of cavitation.

2 Use of Cavitation Bubbles as Pressure Sensors Cavitation inception index i p i p v U Pressure coefficient of the flow field i 1 2 U Principle of use of cavitation bubbles as pressure sensors If cavitation bubbles are observed in the flow field, then that means the instantaneous local minimum fluctuating pressure reaches the vapor pressure level, i.e., pmin p v. Thus at that instance, the local minimum pressure coefficient has roughly the same magnitude as the cavitation index, more specifically, Cpmin i, since we can always adjust the ambient pressure so that the 2 conditions for cavitation at local area are satisfied, i.e., Cp min ( pmin p ref ) (0.5U ) i. The adjustment of the ambient pressure will not affect the flow structure, thus the magnitude of the cavitation index i represents the maximum possible fluctuation of Cp in the flow field. Representative work of use of cavitation bubbles as pressure sensors Ooi and Acosta (1983), T.J. O Hern (1990), Ran and Katz (1991, 1994) i Measurement of the inception index Carried out using visual observations by keeping the velocity constant and reducing the pressure of the facility until cavitation appears. p Cavitation inception index Mean static pressure at inception Vapor pressure of the liquid Free stream velocity Density of the Liquid Cp p v 2 p p ref U pressure P min time Lower ambient Pressure ~ P P ref ~ P P ref ~ P i ~ P v

3 Lock-on Behavior of Cavitation Inception on 2D Cavity Flow Flow Direction Cavity Trailing Edge 10 mm (a) t = 0 s (b) t = 33.3s (c) t = 66.7 s (d) t = 100 s (e) t = 133.3s (f) t = 200 s Free stream speed: 10 m/s Recording speed: 30,000 fps Cavitation inception index: 0.9 (water is saturated with air) Speed of replay = 10 fps 10 mm Top view Flow (g) t = s (h) t =400s (i) t = s Flow (j) t = s (k) t = 800 s (l) t = s (m) t = s (n) t = s (o) t = s Click to launch the movie Lock-on: Occurs above the step. Flow (p) t = s (q) t = s (r) t = s (s) t = 2200 s (t) t = s (u) t = s The cavitation process appear to be cyclic. Periodic: ~ 320 Hz.

4 Ensemble Averaged Velocity and Pressure Distributions Ue = 5.0 m/s; Re=167,500 (based on cavity width) u / U e v /U e Pressure Distribution upstream of T.E. Cp Trailing Edge (a) Cavity Wall Trailing Edge (b) Cavity Wall Cp Cprms Lowest mean pressure location in entire flow field Trailing Edge (c) Cavity Wall -0.2 Trailing Edge (d) Cavity Wall

5 i PDF of Pressure Fluctuations around the Trailing Corner Developed Cavitation at = 0.37, Ue = 10m/s, D.O. level Ue = 5.0 m/s; Re=167,500 (based on cavity width) 0.8ppm Cavitation Inception Index ~ -0.7 Cp P v P i P 1 2 U (m/s) Pv U Vapor pressure of water Static pressure upstream of cavity opening P, U Cpmin i Cavity Trailing Edge The spatial pressure measurements are in full-agreement with cavitation indices measurements.

6 Developed Cavitation at = 0.37, Ue = 10m/s, D.O. level 0.8ppm Recording speed: 8,000 fps; Replay speed: 10 fps; Top View 38 mm Click to launch the movie Trailing-Edge Flow Shedding vortices away upstream Trailing edge cavitation appears Shedding vortices approach T.E. Trailing edge cavitation disappears

7 Developed Cavitation at = 0.37, Ue = 10m/s, D.O. level 0.8ppm Recording speed: 8,000 fps; Replay speed: 5 fps Click to launch the movie Recording speed: 30,000 fps; Replay speed: 10 fps Click to launch the movie

8 Developed Cavitation at = 0.37, Ue = 10m/s, D.O. level 0.8ppm 38 mm (p) t = 0 s (q) t = 500s (r) t = 750 s (p) t = 1250 s (q) t = 1500s (r) t = 2000 s (p) t = 2250 s (q) t = 2750s (r) t = 3000 s (p) t = 3250 s (q) t = 3750s (r) t = 4000 s (p) t = 4250 s (q) t = 4500s (r) t = 5000 s Flow Shedding vortices away upstream (p) t = 5250 s (q) t = 5500s (r) t = 5750 s Trailing edge cavitation appears Shedding vortices approach T.E. Trailing edge cavitation disappears Recording speed: 8,000 fps; Replay speed: 10 fps Click to launch the movie

9 Low Vorticity Shedding Vortex Location and Pressure above T.E: Sample Pictures P (pascal) L U Shedding vortex near T.E. Cavity Trailing Edge Cavity Trailing Edge High pressure above T.E. High Vorticity L U P (pascal) Shedding away upstream Cavity Trailing Edge Cavity Trailing Edge Low pressure above T.E. Ue = 5m/s

10 Conditional Sampling L U Cp PDF of V Threshold: V<0 Threshold: V<0 217 samples L U Cp Threshold: V>0 Threshold: V>0 753 samples

11 Vortex Shedding Frequency from Pressure Spectrum Flow Direction P, U Cavity Wall Frequency (Hz) Ue=5m/s Trailing Edge fw U e Location of Pressure Transducer fl fl n Ue Frequency (Hz) Ue=10m/s Ue=5m/s Theory Ue=10m/s fl c 1 n U U 4 e c Take 0. 5 e U e (Martin et al, 1975; Blake, 1986 L=38.1 mm n Frequency of shedding vortices impinging on the trailing corner based on high-speed movie: ~320Hz. Cycle: ~3ms. Shedding vortex convection speed: 5~6m/s. In agreement with Blake (1986).

12 Cavitation Inception High-Speed Movie Free stream speed: 10 m/s Recording speed: 30,000 fps Replay speed: 10 fps Dissolved Oxygen Level: 8.0 ppm Cavitation inception index: 0.91 Dissolved Oxygen Level: 1.4 ppm Cavitation inception index: 0.52 Click to launch the movie Click to launch the movie 10 mm 10 mm

13 Forward Protruding of Cavitation in Degassed Water Flow Direction Side view 4 mm (a) t= 0.0 ms (c) t= 1.0 ms (b) t= 0.5 ms (d) t= 1.5 ms Free stream speed: 10 m/s Image recording speed: 2,000 fps Cavitation inception index: 0.53 Dissolved oxygen concentration: 1.7 ppm (e) t= 2.0 ms Cavity Trailing Edge (f) t= 2.5 ms

14 A Rare Cavitation Event Captured in the Shear Layer Side view Flow Direction (a) t= 0.0 ms (c) t= 1.0 ms 4 mm (b) t= 0.5 ms (d) t= 1.5 ms Free stream speed: 10 m/s Image recording speed: 2,000 fps Cavitation inception index: 0.53 Dissolved oxygen concentration: 1.7 ppm Cavity Trailing Edge The pressure minima in the shear layer are sufficiently low to initiate cavitation once a nucleus is available, though very rare statistically.

15 Measured Cavitation Inception Index Definition of cavitation inception index: P v P U i P 1 2 P U Vapor pressure of water v Static pressure measured upstream of cavity opening Free stream velocity measured upstream of cavity opening Density of water i Measured cavitation inception indices at different dissolved oxygen concentrations Flow Direction P, U Trailing Edge U (m/s) Cavity Wall L=38.1 mm H=30.0 mm Cavitation inception index is velocity dependent. Note: the dissolved air content has a substantial impact on the cavitation inception index.

16 PDF of Pressure Fluctuation and Measured Cavitation Inception Indices Cavitation index: 0.53, D.O.: 1.7ppm Cp rms Cavitation Inception Indices Ue=10m/s Re=335,000(based on cavity width) Re = 340 U (m/s)

17 Conclusions The onset of cavitation always occurs on top of the cavity trailing edge. The cavitation inception process appears to be cyclic, with frequency that matches theoretical predictions of vortex shedding frequencies. The mean spatial pressure distribution and PDFs of pressure fluctuations explains why the onset of cavitation is always locked on the cavity trailing edge. Flow induced by interaction of shear layer vortex structures with the downstream corner generates a cyclic pressure field, and consequently, a cyclic cavitation process, even at very low cavitation indices. Pressure velocity and pressure-rate of strain correlations have been measured. Analysis of trends is in progress.

Experimental Setup. Flow Direction Leading Edge. Field of View (25 25 mm) Trailing Edge. Cavity Wall. H=30.0 mm. L=38.1 mm

Experimental Setup. Flow Direction Leading Edge. Field of View (25 25 mm) Trailing Edge. Cavity Wall. H=30.0 mm. L=38.1 mm Exerimental Setu High Seed Camera PCO.dimax, 1 bit Resolution: 1008x1000 ixels @ 4500 fs Resolution: 000x000 ixels @ 1400 fs High Reetition Rate Laser Photonics DM60-57 Nd:YLF Maximum ulse rate - 10 khz

More information

CAV2001:sessionA Shridhar Gopalan and Joseph Katz The Johns Hopkins University, Baltimore MD

CAV2001:sessionA Shridhar Gopalan and Joseph Katz The Johns Hopkins University, Baltimore MD CAV2001:sessionA6.004 1 Tip Leakage Cavitation, Associated Bubble ynamics, Noise, Flow Structure and Effect of Tip Gap Size Shridhar Gopalan and Joseph Katz The Johns Hopkins University, Baltimore M Han

More information

Flow structure and modeling issues in the closure region of attached cavitation

Flow structure and modeling issues in the closure region of attached cavitation PHYSICS OF FLUIDS VOLUME 12, NUMBER 4 APRIL 2000 Flow structure and modeling issues in the closure region of attached cavitation Shridhar Gopalan and Joseph Katz Department of Mechanical Engineering, The

More information

The influence of developed cavitation on the flow of a turbulent shear layer

The influence of developed cavitation on the flow of a turbulent shear layer PHYSICS OF FLUIDS VOLUME 14, NUMBER 10 OCTOBER 2002 The influence of developed cavitation on the flow of a turbulent shear layer Claudia O. Iyer and Steven L. Ceccio Department of Mechanical Engineering,

More information

Flow Induced Noise Generation By Partial Cavities

Flow Induced Noise Generation By Partial Cavities Flow Induced Noise Generation By Partial Cavities Harish Ganesh, Juliana Wu and Steven L. Ceccio University of Michigan, Ann Arbor USA 2nd FLINOVIA Symposium Penn-State University, State College, PA Sponsor:

More information

THE EFFECT OF SAMPLE SIZE, TURBULENCE INTENSITY AND THE VELOCITY FIELD ON THE EXPERIMENTAL ACCURACY OF ENSEMBLE AVERAGED PIV MEASUREMENTS

THE EFFECT OF SAMPLE SIZE, TURBULENCE INTENSITY AND THE VELOCITY FIELD ON THE EXPERIMENTAL ACCURACY OF ENSEMBLE AVERAGED PIV MEASUREMENTS 4th International Symposium on Particle Image Velocimetry Göttingen, Germany, September 7-9, 00 PIV 0 Paper 096 THE EFFECT OF SAMPLE SIZE, TURBULECE ITESITY AD THE VELOCITY FIELD O THE EXPERIMETAL ACCURACY

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

Cavitation Inception and Dynamics in Vortical Flows

Cavitation Inception and Dynamics in Vortical Flows Cavitation Inception and Dynamics in Vortical Flows Steve L. Ceccio Mechanical Engineering Naval Architecture & Marine Engineering University of Michigan Ann Arbor, MI, 48109 American Physical Society

More information

Vortex-induced vibrations and lock-in phenomenon of bellows structure subjected to fluid flow

Vortex-induced vibrations and lock-in phenomenon of bellows structure subjected to fluid flow Fluid Structure Interaction and Moving Boundary Problems 225 Vortex-induced vibrations and lock-in phenomenon of bellows structure subjected to fluid flow M. Watanabe & M. Oyama Department of Mechanical

More information

Time Resolved PIV Measurements Elucidate the Feedback Mechanism that Causes Low-Frequency Undulation in an Open Cavity Shear Layer

Time Resolved PIV Measurements Elucidate the Feedback Mechanism that Causes Low-Frequency Undulation in an Open Cavity Shear Layer 9TH INTERNATIONAL SYMPOSIUM ON PARTICLE IMAGE VELOCIMETRY PIV 11 Kobe, Japan, July 21-23, 2011 Time Resolved PIV Measurements Elucidate the Feedback Mechanism that Causes Low-Frequency Undulation in an

More information

Viscous potential flow analysis of stress induced cavitation in an aperture flow

Viscous potential flow analysis of stress induced cavitation in an aperture flow cavitation-july9.tex Viscous potential flow analysis of stress induced cavitation in an aperture flow T. Funada, J. Wang and D. D. Joseph Department of Digital Engineering, Numazu College of Technology,

More information

Part 3. Stability and Transition

Part 3. Stability and Transition Part 3 Stability and Transition 281 Overview T. Cebeci 1 Recent interest in the reduction of drag of underwater vehicles and aircraft components has rekindled research in the area of stability and transition.

More information

Topics in Other Lectures Droplet Groups and Array Instability of Injected Liquid Liquid Fuel-Films

Topics in Other Lectures Droplet Groups and Array Instability of Injected Liquid Liquid Fuel-Films Lecture Topics Transient Droplet Vaporization Convective Vaporization Liquid Circulation Transcritical Thermodynamics Droplet Drag and Motion Spray Computations Turbulence Effects Topics in Other Lectures

More information

Numerical investigation of cavitation-regimes in a converging-diverging nozzle

Numerical investigation of cavitation-regimes in a converging-diverging nozzle Numerical investigation of cavitation-regimes in a converging-diverging nozzle 1 Polina Gorkh, 1 Steffen J. Schmidt, and 1 Nikolaus A. Adams 1 Institute of Aerodynamics and Fluid Mechanics, Department

More information

Experimental Investigation of the Aerodynamic Forces and Pressures on Dome Roofs: Reynolds Number Effects

Experimental Investigation of the Aerodynamic Forces and Pressures on Dome Roofs: Reynolds Number Effects Experimental Investigation of the Aerodynamic Forces and Pressures on Dome Roofs: Reynolds Number Effects *Ying Sun 1), Ning Su 2), Yue Wu 3) and Qiu Jin 4) 1), 2), 3), 4) Key Lab of Structures Dynamic

More information

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

Studies on the Transition of the Flow Oscillations over an Axisymmetric Open Cavity Model Advances in Aerospace Science and Applications. ISSN 2277-3223 Volume 3, Number 2 (2013), pp. 83-90 Research India Publications http://www.ripublication.com/aasa.htm Studies on the Transition of the Flow

More information

International Conference on Methods of Aerophysical Research, ICMAR 2008

International Conference on Methods of Aerophysical Research, ICMAR 2008 International Conference on Methods of Aerophysical Research, ICMAR 8 EXPERIMENTAL STUDY OF UNSTEADY EFFECTS IN SHOCK WAVE / TURBULENT BOUNDARY LAYER INTERACTION P.A. Polivanov, А.А. Sidorenko, A.A. Maslov

More information

Global Structure of Buffeting Flow on Transonic Airfoils

Global Structure of Buffeting Flow on Transonic Airfoils Global Structure of Buffeting Flow on Transonic Airfoils J.D. Crouch, A. Garbaruk, D. Magidov, and L. Jacquin Abstract The flow field associated with transonic airfoil buffet is investigated using a combination

More information

Comparative study of RANS and LES in simulating cavitating flows

Comparative study of RANS and LES in simulating cavitating flows 31st Symposium on Naval Hydrodynamics California, USA, September 11-16, 2016 Comparative study of RANS and LES in simulating cavitating flows Aswin Gnanaskandan and Krishnan Mahesh (University of Minnesota,

More information

Effects of tip-gap size on the tip-leakage flow in a turbomachinery cascade

Effects of tip-gap size on the tip-leakage flow in a turbomachinery cascade PHYSICS OF FLUIDS 18, 105102 2006 Effects of tip-gap size on the tip-leakage flow in a turbomachinery cascade Donghyun You a Center for Turbulence Research, Stanford University, Stanford, California 94305

More information

NUMERICAL SIMULATION OF UNSTEADY CAVITATING FLOWS

NUMERICAL SIMULATION OF UNSTEADY CAVITATING FLOWS NUMERICAL SIMULATION OF UNSTEADY CAVITATING FLOWS Charles C.S. Song and Qiao Qin St. Anthony Falls Laboratory, University of Minnesota Mississippi River at 3 rd Ave. SE, Minneapolis, MN 55414, USA ABSTRACT

More information

Physics and Control of Cavitation

Physics and Control of Cavitation Jean-Pierre FRANC University of Grenoble LEGI BP 53 38041 Grenoble Cedex 9 FRANCE Jean-Pierre.Franc@hmg.inpg.fr ABSTRACT The objective of the present chapter 1 is to provide the basic concepts and tools

More information

Shock induced boundary layer separation and associated unsteadiness

Shock induced boundary layer separation and associated unsteadiness Shock induced boundary layer separation and associated unsteadiness Pierre Dupont thanks to J.P. Dussauge, J.F. Debiève, L. Larchevêque, S. Piponniau Summary Low frequency unsteadiness in turbulent Shock

More information

A numerical study on the effects of cavitation on orifice flow

A numerical study on the effects of cavitation on orifice flow PHSICS OF FLUIDS, A numerical study on the effects of cavitation on orifice flow S. Dabiri, W. A. Sirignano, and D. D. Joseph, University of California, Irvine, California 9697, USA University of Minnesota,

More information

Proe. Indian Acad. Sci., Vol. C 2, Pt. 2, May 1979, pp

Proe. Indian Acad. Sci., Vol. C 2, Pt. 2, May 1979, pp Proe. Indian Acad. Sci., Vol. C 2, Pt. 2, May 1979, pp. 149-177. 9 Printed in India. Cavitation inception VIJAY H ARAKERI Department of Mechanical Engineering, Indian Institute of Science, Bangalore 560

More information

Visualizations of Leading Edge Cavitation in an Inducer at Different Temperatures

Visualizations of Leading Edge Cavitation in an Inducer at Different Temperatures Visualizations of Leading Edge Cavitation in an Inducer at Different Temperatures J.P. Franc*, E. Janson**, P. Morel***, C. Rebattet**, M. Riondet* * Laboratoire des Ecoulements Géophysiques et Industriels,

More information

Dynamic Pressure Characterization of a Dual-Mode Scramjet

Dynamic Pressure Characterization of a Dual-Mode Scramjet 26 th ICDERS July 30 th August 4 th, 2017 Boston, MA, USA Dynamic Pressure Characterization of a Dual-Mode Scramjet Camilo Aguilera, Amardip Ghosh, Kyung-Hoon Shin, Kenneth H. Yu Department of Aerospace

More information

AN ABSTRACT OF THE DISSERTATION OF

AN ABSTRACT OF THE DISSERTATION OF AN ABSTRACT OF THE DISSERTATION OF Ehsan Shams Sobhani for the degree of Doctor of Philosophy in Mechanical Engineering presented on November 13, 2009. Title: Numerical Simulation of Cavitating Bubble-Laden

More information

SOME TRANSITION AND CA VIT AT ION INCEPTION OBSERVATIONS ON A 1. 5 CAL OGIVE. V. H. Arakeri and A. J. Acosta California Institute of Technology

SOME TRANSITION AND CA VIT AT ION INCEPTION OBSERVATIONS ON A 1. 5 CAL OGIVE. V. H. Arakeri and A. J. Acosta California Institute of Technology 233 SOME TRANSITION AND CA VIT AT ION INCEPTION OBSERVATIONS ON A 1. 5 CAL OGIVE by V. H. Arakeri and A. J. Acosta California Institute of Technology for presentation to the Seventeenth Meeting of the

More information

Numerical study of the effects of trailing-edge bluntness on highly turbulent hydro-foil flows

Numerical study of the effects of trailing-edge bluntness on highly turbulent hydro-foil flows Numerical study of the effects of trailing-edge bluntness on highly turbulent hydro-foil flows T. Do L. Chen J. Tu B. Anderson 7 November 2005 Abstract Flow-induced noise from fully submerged lifting bodies

More information

Active Control of Separated Cascade Flow

Active Control of Separated Cascade Flow Chapter 5 Active Control of Separated Cascade Flow In this chapter, the possibility of active control using a synthetic jet applied to an unconventional axial stator-rotor arrangement is investigated.

More information

RECONSTRUCTION OF TURBULENT FLUCTUATIONS FOR HYBRID RANS/LES SIMULATIONS USING A SYNTHETIC-EDDY METHOD

RECONSTRUCTION OF TURBULENT FLUCTUATIONS FOR HYBRID RANS/LES SIMULATIONS USING A SYNTHETIC-EDDY METHOD RECONSTRUCTION OF TURBULENT FLUCTUATIONS FOR HYBRID RANS/LES SIMULATIONS USING A SYNTHETIC-EDDY METHOD N. Jarrin 1, A. Revell 1, R. Prosser 1 and D. Laurence 1,2 1 School of MACE, the University of Manchester,

More information

VISUALIZATION OF PRESSURE WAVE GENERATED BY COLLAPSE OF CAVITATION CLOUD USING FRAME DIFFERENCE METHOD

VISUALIZATION OF PRESSURE WAVE GENERATED BY COLLAPSE OF CAVITATION CLOUD USING FRAME DIFFERENCE METHOD ISFV3-3 th International Symposium on Flow Visualization FLUVISU2-2 th French Congress on Visualization in Fluid Mechanics July -4, 28, Nice, France VISUALIZATION OF PRESSURE WAVE GENERATED BY COLLAPSE

More information

INFLUENCE OF ACOUSTIC EXCITATION ON AIRFOIL PERFORMANCE AT LOW REYNOLDS NUMBERS

INFLUENCE OF ACOUSTIC EXCITATION ON AIRFOIL PERFORMANCE AT LOW REYNOLDS NUMBERS ICAS 2002 CONGRESS INFLUENCE OF ACOUSTIC EXCITATION ON AIRFOIL PERFORMANCE AT LOW REYNOLDS NUMBERS S. Yarusevych*, J.G. Kawall** and P. Sullivan* *Department of Mechanical and Industrial Engineering, University

More information

VORTICITY FIELD EVOLUTION IN A FORCED WAKE. Richard K. Cohn Air Force Research Laboratory Edwards Air Force Base, CA 92524

VORTICITY FIELD EVOLUTION IN A FORCED WAKE. Richard K. Cohn Air Force Research Laboratory Edwards Air Force Base, CA 92524 Proceedings of the st International Symposium on Turbulence and Shear Flow Phenomena, Santa Barbara, CA, Sep. 5, 999, Eds. Banerjee, S. and Eaton, J. K., pp. 9-96. VORTICITY FIELD EVOLUTION IN A FORCED

More information

Vortex Induced Vibrations

Vortex Induced Vibrations Vortex Induced Vibrations By: Abhiroop Jayanthi Indian Institute of Technology, Delhi Some Questions! What is VIV? What are the details of a steady approach flow past a stationary cylinder? How and why

More information

Direct Numerical Simulations of Transitional Flow in Turbomachinery

Direct Numerical Simulations of Transitional Flow in Turbomachinery Direct Numerical Simulations of Transitional Flow in Turbomachinery J.G. Wissink and W. Rodi Institute for Hydromechanics University of Karlsruhe Unsteady transitional flow over turbine blades Periodic

More information

THE RELATION BETWEEN THE NUCLEI POPULATION AND THE CAVITATION EVENT RATE FOR CAVITATION ON A SCHIEBE BODY

THE RELATION BETWEEN THE NUCLEI POPULATION AND THE CAVITATION EVENT RATE FOR CAVITATION ON A SCHIEBE BODY THE RELATION BETWEEN THE NUCLEI POPULATION AND THE CAVITATION EVENT RATE FOR CAVITATION ON A SCHIEBE BODY FED-Val. 190, Cavitation and Gas-Liquid Flow in Fluid Machinery and Devices ASME 1994 Zhenhuan

More information

1) the intermittence of the vortex-shedding regime at the critical angle of incidence in smooth flow; ) the inversion of the lift coefficient slope at

1) the intermittence of the vortex-shedding regime at the critical angle of incidence in smooth flow; ) the inversion of the lift coefficient slope at The Seventh International Colloquium on Bluff Body Aerodynamics and Applications (BBAA7) Shanghai, China; September -6, 01 Experimental investigation on the aerodynamic behavior of square cylinders with

More information

inter.noise 2000 The 29th International Congress and Exhibition on Noise Control Engineering August 2000, Nice, FRANCE

inter.noise 2000 The 29th International Congress and Exhibition on Noise Control Engineering August 2000, Nice, FRANCE Copyright SFA - InterNoise 2000 1 inter.noise 2000 The 29th International Congress and Exhibition on Noise Control Engineering 27-30 August 2000, Nice, FRANCE I-INCE Classification: 1.0 NOZZLE DESIGN EFFECT

More information

CAVITATION EFFECTS ON FLUID STRUCTURE INTERACTION IN THE CASE OF A 2D HYDROFOIL

CAVITATION EFFECTS ON FLUID STRUCTURE INTERACTION IN THE CASE OF A 2D HYDROFOIL Proceedings of ASME FEDSM2005 2005 ASME Fluids Engineering Division Summer Conference Houston, TX, June 19-23, 2005 FEDSM2005-77477 CAVITATION EFFECTS ON FLUID STRUCTURE INTERACTION IN THE CASE OF A 2D

More information

SC AD-A BUBBLY CAVITATION FLOWS AUG Final Report. E. Brennen California Institute of Technology Pasadena, California 91125

SC AD-A BUBBLY CAVITATION FLOWS AUG Final Report. E. Brennen California Institute of Technology Pasadena, California 91125 AD-A239 722 SC. AUG 16 1991 Final Report BUBBLY CAVITATION FLOWS E. Brennen California Institute of Technology Pasadena, California 91125 1. INTRODUCTION This constitutes the final report on the research

More information

Fluid Mechanics II 3 credit hour. External flows. Course teacher Dr. M. Mahbubur Razzaque Professor Department of Mechanical Engineering BUET 1

Fluid Mechanics II 3 credit hour. External flows. Course teacher Dr. M. Mahbubur Razzaque Professor Department of Mechanical Engineering BUET 1 COURSE NUMBER: ME 323 Fluid Mechanics II 3 credit hour External flows Course teacher Dr. M. Mahbubur Razzaque Professor Department of Mechanical Engineering BUET 1 External flows The study of external

More information

Cavitation Instabilities

Cavitation Instabilities Cavitation Instabilities Yoshinobu Tsujimoto Engineering Science, Osaka University, 1-3 Toyonaka, Machikaneyama, Osaka, 560-8531, Japan tujimoto@me.es.osaka-u.ac.jp Introduction It is well known that cavitating

More information

Aerodynamic characteristics of two-dimensional sharp-edged objects in tandem arrangement )

Aerodynamic characteristics of two-dimensional sharp-edged objects in tandem arrangement ) Arch. Mech., 60, 6, pp. 475 490, Warszawa 2008 SIXTY YEARS OF THE ARCHIVES OF MECHANICS Aerodynamic characteristics of two-dimensional sharp-edged objects in tandem arrangement ) R. GNATOWSKA Institute

More information

SURGE INSTABILITY ON A CAVITATING PROPELLER

SURGE INSTABILITY ON A CAVITATING PROPELLER CAV2001:sessionB8.003 1 SURGE INSTABILITY ON A CAVITATING PROPELLER Mark E. Duttweiler 1 and Christopher E. Brennen California Institute of Technology, Pasadena, CA 91125 Abstract This study details experiments

More information

Vortex cavitation and oscillation in a doublesuction

Vortex cavitation and oscillation in a doublesuction IOP Conference Series: Earth and Environmental Science Vortex cavitation and oscillation in a doublesuction volute pump To cite this article: T Sato et al 2010 IOP Conf. Ser.: Earth Environ. Sci. 12 012019

More information

On self-sustained oscillations in two-dimensional compressible flow over rectangular cavities

On self-sustained oscillations in two-dimensional compressible flow over rectangular cavities J. Fluid Mech. (22), vol. 455, pp. 315 346. c 22 Cambridge University Press DOI: 1.117/S2211217534 Printed in the United Kingdom 315 On self-sustained oscillations in two-dimensional compressible flow

More information

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

Experimental investigation of flow control devices for the reduction of transonic buffeting on rocket afterbodies Experimental investigation of flow control devices for the reduction of transonic buffeting on rocket afterbodies F.F.J. Schrijer 1, A. Sciacchitano 1, F. Scarano 1 1: Faculty of Aerospace Engineering,

More information

Journal of Fluid Science and Technology

Journal of Fluid Science and Technology Bulletin of the JSME Vol.9, No.3, 24 Journal of Fluid Science and Technology Re-evaluating wake width in turbulent shear flow behind an axisymmetric cylinder by means of higher order turbulence statistics

More information

Numerical Studies of Supersonic Jet Impingement on a Flat Plate

Numerical Studies of Supersonic Jet Impingement on a Flat Plate Numerical Studies of Supersonic Jet Impingement on a Flat Plate Overset Grid Symposium Dayton, OH Michael R. Brown Principal Engineer, Kratos/Digital Fusion Solutions Inc., Huntsville, AL. October 18,

More information

FEDSM AIR ENTRAINMENT BY TWO-DIMENSIONAL PLUNGING JETS : THE IMPINGEMENT REGION AND THE VERY-NEAR FLOW FIELD

FEDSM AIR ENTRAINMENT BY TWO-DIMENSIONAL PLUNGING JETS : THE IMPINGEMENT REGION AND THE VERY-NEAR FLOW FIELD Proceedings of FEDSM'98: 1998 ASME Fluids Engineering Division Summer Meeting June 21-25, 1998, Washington, DC FEDSM98-486 AIR ENTRAINMENT BY TWO-DIMENSIONAL PLUNGING JETS : THE IMPINGEMENT REGION AND

More information

VOF Simulations Of Hydrodynamic Cavitation Using The Asymptotic And Classical Rayleigh-Plesset Models

VOF Simulations Of Hydrodynamic Cavitation Using The Asymptotic And Classical Rayleigh-Plesset Models Fifth International Symposium on Marine Propulsion smp 17, Espoo, Finland, June 2017 VOF Simulations Of Hydrodynamic Cavitation Using The Asymptotic And Classical Rayleigh-Plesset Models Samir Muzaferija

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

Thermoacoustic Instabilities Research

Thermoacoustic Instabilities Research Chapter 3 Thermoacoustic Instabilities Research In this chapter, relevant literature survey of thermoacoustic instabilities research is included. An introduction to the phenomena of thermoacoustic instability

More information

Partial Cavity Instabilities and Re-Entrant Jet

Partial Cavity Instabilities and Re-Entrant Jet CAV1:lecture. Partial Cavity Instabilities and Re-Entrant Jet J.P. Franc Laboratoire des Ecoulements Géophysiques et Industriels, BP 53, 3841 GRENOBLE Cedex 9, France Abstract The purpose of this talk

More information

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

Module 3: Velocity Measurement Lecture 15: Processing velocity vectors. The Lecture Contains: Data Analysis from Velocity Vectors The Lecture Contains: Data Analysis from Velocity Vectors Velocity Differentials Vorticity and Circulation RMS Velocity Drag Coefficient Streamlines Turbulent Kinetic Energy Budget file:///g /optical_measurement/lecture15/15_1.htm[5/7/2012

More information

UNIVERSITY OF MINNESOTA. Travis Jon Schauer. Name of Faculty Adviser(s) Signature of Faculty Adviser(s) Date GRADUATE SCHOOL

UNIVERSITY OF MINNESOTA. Travis Jon Schauer. Name of Faculty Adviser(s) Signature of Faculty Adviser(s) Date GRADUATE SCHOOL UNIVERSITY OF MINNESOTA This is to certify that I have examined this copy of a master s thesis by Travis Jon Schauer and have found that it is complete and satisfactory in all respects, and that any and

More information

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

UWE has obtained warranties from all depositors as to their title in the material deposited and as to their right to deposit such material. Yao, Y., Fang, J., Zheltovodov, A. A. and Lu, L. (2014) Direct numerical simulation of supersonic flows passing a backward step. In: UK Turbulence Consortium Workshop, Imperial College, London, 22-23 September

More information

On the aeroacoustic tonal noise generation mechanism of a sharp-edged. plate

On the aeroacoustic tonal noise generation mechanism of a sharp-edged. plate On the aeroacoustic tonal noise generation mechanism of a sharp-edged plate Danielle J. Moreau, Laura A. Brooks and Con J. Doolan School of Mechanical Engineering, The University of Adelaide, South Australia,

More information

Günter Schewe DLR Institut für Aeroelastik Göttingen, Germany

Günter Schewe DLR Institut für Aeroelastik Göttingen, Germany EACWE 5 Florence, Italy 19 th 23 rd July 2009 Flying Sphere image Museo Ideale L. Da Vinci Reynolds-Number-Effects in Flow around a rectangular Cylinder with Aspect Ratio 1:5 Günter Schewe DLR Institut

More information

Numerical Investigation of Vortex Induced Vibration of Two Cylinders in Side by Side Arrangement

Numerical Investigation of Vortex Induced Vibration of Two Cylinders in Side by Side Arrangement Numerical Investigation of Vortex Induced Vibration of Two Cylinders in Side by Side Arrangement Sourav Kumar Kar a, 1,, Harshit Mishra a, 2, Rishitosh Ranjan b, 3 Undergraduate Student a, Assitant Proffessor

More information

Experimental Investigation of Cavitating Herschel Venturi- Tube Configuration

Experimental Investigation of Cavitating Herschel Venturi- Tube Configuration Experimental Investigation of Cavitating Herschel Venturi- Tube Configuration Abstract S. Brinkhorst 1, E. von Lavante 1, D. Güler 1, G. Wendt 2 1 Chair of Fluidmechanics, University of Duisburg-Essen,

More information

NEW TYPES OF CAVITATION INSTABILITIES IN INDUCERS

NEW TYPES OF CAVITATION INSTABILITIES IN INDUCERS 4 th International Conference on Launcher Technology "Space Launcher Liquid Propulsion" NEW TYPES OF CAVITATION INSTABILITIES IN INDUCERS Yoshinobu TSUJIMOTO, Yury A.SEMENOV * Osaka University Graduate

More information

Structure of Periodic Cavitation Clouds in Submerged Impinging Water-Jet Issued from Horn-Type Nozzle

Structure of Periodic Cavitation Clouds in Submerged Impinging Water-Jet Issued from Horn-Type Nozzle 9th Pacific Rim International Conference on Water Jetting Technology Structure of Periodic Cavitation Clouds in Submerged Impinging Water-Jet Issued from Horn-Type Nole Keiichi SATO a*, Yasuhiro SUGIMOTO

More information

Forcing the shear layer of a backward-facing step flow

Forcing the shear layer of a backward-facing step flow Forcing the shear layer of a backward-facing step flow using DBD plasma actuator J.-L. Aider* T. Duriez* J. E. Wesfreid* G. Artana *Laboratoire PMMH UMR7636 CNRS ESPCI - France Laboratorio de FluidoDynamica

More information

Vortex shedding from slender surface mounted pyramids

Vortex shedding from slender surface mounted pyramids Vortex shedding from slender surface mounted pyramids M. J. Morrison 1, R. J. Martinuzzi 3, E. Savory 1, G. A. Kopp 2 1 Department of Mechanical and Materials Engineering, University of Western Ontario,

More information

Aerodynamic noise produced in flow around an automobile bonnet

Aerodynamic noise produced in flow around an automobile bonnet Aerodynamic noise produced in flow around an automobile bonnet Hiroshi Yokoyama 1, Takahiro Nakajima 2, Taishi Shinohara 3, Masashi Miyazawa 4 and Akiyoshi Iida 5 1,2,3,5 Department of Mechanical Engineering,

More information

Application of two turbulence models for computation of cavitating flows in a centrifugal pump

Application of two turbulence models for computation of cavitating flows in a centrifugal pump IOP Conference Series: Materials Science and Engineering OPEN ACCESS Application of two turbulence models for computation of cavitating flows in a centrifugal pump To cite this article: M He et al 2013

More information

REYNOLDS NUMBER EFFECTS ON HEMISPHERICAL DOMES IN SMOOTH FLOW

REYNOLDS NUMBER EFFECTS ON HEMISPHERICAL DOMES IN SMOOTH FLOW The Seventh Asia-Pacific Conference on Wind Engineering, November 8-2, 29, Taipei, Taiwan ABSTRACT REYNOLDS NUMBER EFFECTS ON HEMISPHERICAL DOMES IN SMOOTH FLOW C. M. Cheng C. L. Fu 2 Director, Wind Engineering

More information

SIMULATION OF THREE-DIMENSIONAL INCOMPRESSIBLE CAVITY FLOWS

SIMULATION OF THREE-DIMENSIONAL INCOMPRESSIBLE CAVITY FLOWS ICAS 2000 CONGRESS SIMULATION OF THREE-DIMENSIONAL INCOMPRESSIBLE CAVITY FLOWS H Yao, R K Cooper, and S Raghunathan School of Aeronautical Engineering The Queen s University of Belfast, Belfast BT7 1NN,

More information

Experimental Analysis of Strains and Vibratory Response of a Flexible Foil

Experimental Analysis of Strains and Vibratory Response of a Flexible Foil Fourth International Symposium on Marine Propulsors SMP 15, Austin, Texas, USA, June 2015 Experimental Analysis of Strains and Vibratory Response of a Flexible Foil Alexandra Lelong 1, Jacques-André Astolfi

More information

*Fluid Dynamics Laboratory, Technische Universiteit Eindhoven, The Netherlands

*Fluid Dynamics Laboratory, Technische Universiteit Eindhoven, The Netherlands Rapports internes du LaMSID P. TESTUD P. MOUSSOU A. HIRSCHBERG* Y. AUREGAN** Noise generated by cavitating single-hole and multi-hole orifices in a water pipe RI-B3-N 005 Avril 2007 *Fluid Dynamics Laboratory,

More information

Investigation of Reynolds Number Scale Effects on Propeller Tip Vortex Cavitation and Propeller-Induced Hull Pressure Fluctuations

Investigation of Reynolds Number Scale Effects on Propeller Tip Vortex Cavitation and Propeller-Induced Hull Pressure Fluctuations th International Symposium on Cavitation CAV28 Baltimore, Maryland, USA, 4 6 May 28 Investigation of Reynolds Number Scale Effects on Propeller Tip Vortex Cavitation and Propeller-Induced Hull Pressure

More information

ACTIVE SEPARATION CONTROL PROCESS OVER A SHARP EDGE RAMP

ACTIVE SEPARATION CONTROL PROCESS OVER A SHARP EDGE RAMP June 30 - July 3, 2015 Melbourne, Australia 9 3D-1 ACTIVE SEPARATION CONTROL PROCESS OVER A SHARP EDGE RAMP Antoine Debien 8 rue Léonard de Vinci antoine.debien@univ-orleans.fr Sandrine Aubrun sandrine.aubrun@univ-orleans.fr

More information

Computations of unsteady cavitating flow on wing profiles using a volume fraction method and mass transfer models

Computations of unsteady cavitating flow on wing profiles using a volume fraction method and mass transfer models Computations of unsteady cavitating flow on wing profiles using a volume fraction method and mass transfer models Tobias Huuva *, Aurelia Cure, Göran Bark * and Håkan Nilsson * Chalmers University of Technology,

More information

CLOUD CAVITATION ON AN OSCILLATING HYDROFOIL

CLOUD CAVITATION ON AN OSCILLATING HYDROFOIL CLOUD CAVITATION ON AN OSCILLATING HYDROFOIL G. E. Reisman, E. A. McKenney, and C. E. Brennen California Institute of Technology Pasadena, CA Presented at: The Twentieth Symposium on Naval Hydrodynamics

More information

Response of base suction and vortex shedding from rectangular prisms to transverse forcing

Response of base suction and vortex shedding from rectangular prisms to transverse forcing J. Fluid Mech. (2002), vol. 461, pp. 25 49. c 2002 Cambridge University Press DOI: 10.1017/S0022112002008534 Printed in the United Kingdom 25 Response of base suction and vortex shedding from rectangular

More information

An Experimental Analysis of the Structural Response of Flexible Lightweight Hydrofoils in Various Flow Conditions

An Experimental Analysis of the Structural Response of Flexible Lightweight Hydrofoils in Various Flow Conditions An Experimental Analysis of the Structural Response of Flexible Lightweight Hydrofoils in Various Flow Conditions Alexandra Lelong,Pierre Guiffant, Jacques André Astolfi * SYMPOSIA ON ROTATING MACHINERY

More information

Time-Varying Flow Investigation of Synthetic Jet Effects on a Separating Boundary Layer

Time-Varying Flow Investigation of Synthetic Jet Effects on a Separating Boundary Layer Time-Varying Flow Investigation of Synthetic Jet Effects on a Separating Boundary Layer FRANCESCA SATTA, DANIELE SIMONI, MARINA UBALDI, PIETRO ZUNINO Department of Fluid Machines, Energy Systems, and Transportation

More information

Direct Numerical Simulation of Pressure Fluctuations Induced by Supersonic Turbulent Boundary Layers

Direct Numerical Simulation of Pressure Fluctuations Induced by Supersonic Turbulent Boundary Layers Direct Numerical Simulation of Pressure Fluctuations Induced by Supersonic Turbulent Boundary Layers PI: Lian Duan --- NSF PRAC 1640865- --- Missouri U. of S&T Project Members: Chao Zhang, Junji Huang,

More information

Surge Instability on a Cavitating Propeller

Surge Instability on a Cavitating Propeller Under consideration for publication in J. Fluid Mech. 1 Surge Instability on a Cavitating Propeller By M. E. D U T T W E I L E R AND C. E. B R E N N E N Division of Engineering and Applied Science, California

More information

ST. ANTHONY FALLS HYDRAULIC LABORATORY

ST. ANTHONY FALLS HYDRAULIC LABORATORY UNIVERSITY Of MINNESOTA ST. ANTHONY FALLS HYDRAULIC LABORATORY Project Report No. 248 THE ROLE OF "NUCLEI" IN TIP VORTEX CAVITATION INCEPTION by Vijay H. Arakeri and Roger E. A. Arndt Sponsored by DAVID

More information

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

Applied Thermal and Fluid Engineering. Energy Engineering (Thermal Engineering Laboratory) Applied Thermal and Fluid Engineering Energy Engineering (Thermal Engineering Laboratory) Professor Assoc. Professor Hajime Nakamura Shunsuke Yamada Outline of Research In our laboratory, we have been

More information

Divergence free synthetic eddy method for embedded LES inflow boundary condition

Divergence free synthetic eddy method for embedded LES inflow boundary condition R. Poletto*, A. Revell, T. Craft, N. Jarrin for embedded LES inflow boundary condition University TSFP Ottawa 28-31/07/2011 *email: ruggero.poletto@postgrad.manchester.ac.uk 1 / 19 SLIDES OVERVIEW 1 Introduction

More information

Cavitation instabilities in hydraulic machines

Cavitation instabilities in hydraulic machines IOP Conference Series: Materials Science and Engineering OPEN ACCESS Cavitation instabilities in hydraulic machines To cite this article: Y Tsujimoto 2013 IOP Conf. Ser.: Mater. Sci. Eng. 52 012005 View

More information

Aerodynamic Rotor Model for Unsteady Flow and Wake Impact

Aerodynamic Rotor Model for Unsteady Flow and Wake Impact Aerodynamic Rotor Model for Unsteady Flow and Wake Impact N. Bampalas, J. M. R. Graham Department of Aeronautics, Imperial College London, Prince Consort Road, London, SW7 2AZ June 28 1 (Steady Kutta condition)

More information

Effect of Liquid Viscosity on Sloshing in A Rectangular Tank

Effect of Liquid Viscosity on Sloshing in A Rectangular Tank International Journal of Research in Engineering and Science (IJRES) ISSN (Online): 2320-9364, ISSN (Print): 2320-9356 Volume 5 Issue 8 ǁ August. 2017 ǁ PP. 32-39 Effect of Liquid Viscosity on Sloshing

More information

Transactions on Engineering Sciences vol 9, 1996 WIT Press, ISSN

Transactions on Engineering Sciences vol 9, 1996 WIT Press,   ISSN The analysis of bubble cavitation inception in turbulent flow around a hydrofoil L. Wilczynski Ship Propeller Department, Institute of Fluid Flow Machinery of the Polish Academy ofsciences, Fiszera 14,

More information

INTERNATIONAL OIML D 25 DOCUMENT. Vortex meters used in measuring systems for fluids ORGANISATION INTERNATIONALE INTERNATIONAL ORGANIZATION

INTERNATIONAL OIML D 25 DOCUMENT. Vortex meters used in measuring systems for fluids ORGANISATION INTERNATIONALE INTERNATIONAL ORGANIZATION INTERNATIONAL OIML D 25 DOCUMENT Edition 1996 (E) Vortex meters used in measuring systems for fluids Compteurs à vortex utilisés dans les ensembles de mesurage de fluides OIML D 25 Edition 1996 (E) ORGANISATION

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

Wind Loads for Utility Scale Photovoltaic Power Plants

Wind Loads for Utility Scale Photovoltaic Power Plants Wind Loads for Utility Scale Photovoltaic Power Plants September 9, 2015 Joe Cain, P.E. David Banks, PhD, P.Eng. In Scope or Out of Scope? In scope for this study: Image curtesy of hbr.org Utility scale

More information

Untersuchungen an einer abgelösten Triebwerksgondel bei gestörter Zuströmung

Untersuchungen an einer abgelösten Triebwerksgondel bei gestörter Zuströmung Fachtagung Lasermethoden in der Strömungsmesstechnik 9. 11. September 2014, Karlsruhe Untersuchungen an einer abgelösten Triebwerksgondel bei gestörter Zuströmung Investigations in a Stalling Nacelle Inlet

More information

Understanding of the Flow Behaviour on a Helmholtz Resonator Excited by Grazing Flow

Understanding of the Flow Behaviour on a Helmholtz Resonator Excited by Grazing Flow Understanding of the Flow Behaviour on a Helmholtz Resonator Excited by Grazing Flow Abstract Grazing flow passing over the quiescent fluid inside the cavity of a Helmholtz resonator can excite the resonator.

More information

SECTIONAL AERODYNAMIC FORCES AND THEIR LONGITUDINAL CORRELATION ON A VIBRATING 5:1 RECTANGULAR CYLINDER

SECTIONAL AERODYNAMIC FORCES AND THEIR LONGITUDINAL CORRELATION ON A VIBRATING 5:1 RECTANGULAR CYLINDER BBAA VI International Colloquium on: Bluff Bodies Aerodynamics & Applications Milano, Italy, July, -4 8 SECTIONAL AERODYNAMIC FORCES AND THEIR LONGITUDINAL CORRELATION ON A VIBRATING 5:1 RECTANGULAR CYLINDER

More information

NUMERICAL INVESTIGATION OF PERFORMANCE OF KAPLAN TURBINE WITH DRAFT TUBE

NUMERICAL INVESTIGATION OF PERFORMANCE OF KAPLAN TURBINE WITH DRAFT TUBE NUMERICAL INVESTIGATION OF PERFORMANCE OF KAPLAN TURBINE WITH DRAFT TUBE Mohamed Adel and Nabil H. Mostafa ABSTRACT Mechanical Power Engineering Department, Engineering Faculty Zagazig University, Zagazig,

More information

RANS COMPUTATIONS OF A CAVITATING VORTEX ROPE AT FULL LOAD

RANS COMPUTATIONS OF A CAVITATING VORTEX ROPE AT FULL LOAD 6 th IAHR International Meeting of the Workgroup on Cavitation and Dynamic Problems in Hydraulic Machinery and Systems, September 9-11, 2015, Ljubljana, Slovenia RANS COMPUTATIONS OF A CAVITATING VORTEX

More information

Multiphase Science and Technology, Vol. 16, Nos. 1-4, pp. 1-20, 2005

Multiphase Science and Technology, Vol. 16, Nos. 1-4, pp. 1-20, 2005 Multiphase Science and Technology, Vol. 16, Nos. 1-4, pp. 1-2, 25 EXPERIMENTS ON THE TURBULENT STRUCTURE AND THE VOID FRACTION DISTRIBUTION IN THE TAYLOR BUBBLE WAKE L. Shemer, A. Gulitski and D. Barnea

More information

EFFECT OF CAVITATION ON THE STRUCTURE OF THE BOUNDARY LAYER IN THE WAKE OF A PARTIAL CAVITY

EFFECT OF CAVITATION ON THE STRUCTURE OF THE BOUNDARY LAYER IN THE WAKE OF A PARTIAL CAVITY Sixth International Symposium on Cavitation CAV6, Wageningen, The Netherlands, September 6 EFFECT OF CAVITATION ON THE STRUCTURE OF THE BOUNDARY LAYER IN THE WAKE OF A PARTIAL CAVITY Sarraf Christophe

More information

Experimental investigation of separated shear layer from a leading edge subjected to various angles of attack with tail flap deflections

Experimental investigation of separated shear layer from a leading edge subjected to various angles of attack with tail flap deflections Sādhanā Vol. 40, Part 3, May 2015, pp. 803 817. c Indian Academy of Sciences Experimental investigation of separated shear layer from a leading edge subjected to various angles of attack with tail flap

More information