Modeling of Oscillating Flow Past a Vertical Plate Spyros A. Kinnas, Yi-Hsiang Yu, Hanseong Lee, Karan Kakar Ocean Engineering Group, Department of Civil.

Slides:



Advertisements
Similar presentations
Instructor: André Bakker
Advertisements

Wind Flow Over Forested Hills: Mean Flow and Turbulence Characteristics CEsA - Centre for Wind Energy and Atmospheric Flows, Portugal J. Lopes da Costa,
CFD II w/Dr. Farouk By: Travis Peyton7/18/2015 Modifications to the SIMPLE Method for Non-Orthogonal, Non-Staggered Grids in k- E Turbulence Flow Model.
13.42 Lecture: Vortex Induced Vibrations
Direct Forcing Immersed Boundary (DFIB) Method for Mixed Heat Transfer
Aero-Hydrodynamic Characteristics
1 Pressure-based Solver for Incompressible and Compressible Flows with Cavitation Sunho Park 1, Shin Hyung Rhee 1, and Byeong Rog Shin 2 1 Seoul National.
University of Western Ontario
FPSO Roll Prediction and Mitigation
Pharos University ME 352 Fluid Mechanics II
Basic bluff-body aerodynamics I
External Flows.
Ye.A. Gayev ( ) (Institute of Hydromechanics of NASU, Kyiv, Ukraine) S.Z. Shikhaliev ( ) (Institute.
Third Graduate Student Symposium UW Math Department (Batmunkh. Ts) 1 Constantin-Lax-Majda Model Equation (1-Dimension) Blow Up Problem  Blow Up.
UNSTEADY VISCOUS FLOW Viscous effects confined to within some finite area near the boundary → boundary layer In unsteady viscous flows at low Re the boundary.
Basic Governing Differential Equations
D A C B z = 20m z=4m Homework Problem A cylindrical vessel of height H = 20 m is filled with water of density to a height of 4m. What is the pressure at:
HYDRODYNAMIC EVOLUTION OF IFE CHAMBERS WITH DIFFERENT PROTECTIVE GASES AND PRE-IGNITION CONDITIONS Zoran Dragojlovic and Farrokh Najmabadi University of.
Jordanian-German Winter Academy 2006 NATURAL CONVECTION Prepared by : FAHED ABU-DHAIM Ph.D student UNIVERSITY OF JORDAN MECHANICAL ENGINEERING DEPARTMENT.
CHE/ME 109 Heat Transfer in Electronics
Fluid Mechanics Wrap Up CEE 331 June 27, 2015 CEE 331 June 27, 2015 
DETAILED TURBULENCE CALCULATIONS FOR OPEN CHANNEL FLOW
Boundary Layer Correction of Viscous Flow Through 2 D Turbine Cascades
Analysis of Physical Intuition … P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Two-dimensional Boundary Layer Flows.
An Ultimate Combination of Physical Intuition with Experiments… P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Boundary Layer.
Fluid mechanics 3.1 – key points
Juan Carlos Ortiz Royero Ph.D.
Motivation  Movie  Game  Engineering Introduction  Ideally  Looks good  Fast simulation  Looks good?  Look plausible  Doesn’t need to be exactly.
Computational Modelling of Unsteady Rotor Effects Duncan McNae – PhD candidate Professor J Michael R Graham.
Conservation Laws for Continua
SNAME H-8 Panel Meeting No. 124 Oct. 18, 2004 NSWC-CD Research Update from UT Austin Ocean Engineering Group Department of Civil Engineering The University.
Wind Modeling Studies by Dr. Xu at Tennessee State University
A. Spentzos 1, G. Barakos 1, K. Badcock 1 P. Wernert 2, S. Schreck 3 & M. Raffel 4 1 CFD Laboratory, University of Glasgow, UK 2 Institute de Recherche.
Lecture Objectives: -Define turbulence –Solve turbulent flow example –Define average and instantaneous velocities -Define Reynolds Averaged Navier Stokes.
Recent and Future Research for Bird-like Flapping MAVs of NPU Prof. B.F.Song Aeronautics School of Northwestern Polytechnical University.
C M C C Centro Euro-Mediterraneo per i Cambiamenti Climatici COSMO General Meeting - September 8th, 2009 COSMO WG 2 - CDC 1 An implicit solver based on.
Wind Energy Program School of Aerospace Engineering Georgia Institute of Technology Computational Studies of Horizontal Axis Wind Turbines PRINCIPAL INVESTIGATOR:
Global Analysis of Floating Structures – M.H. Kim
Cylinder loading in transient motion representing flow under a wave group by T. Stallard, P.H. Taylor, C.H.K. Williamson, and A.G.L. Borthwick Proceedings.
Numerical investigation on the upstream flow condition of the air flow meter in the air intake assembly of a passenger car Zoltán Kórik Supervisor: Dr.
Historically the First Fluid Flow Solution …. P M V Subbarao Professor Mechanical Engineering Department I I T Delhi Second Class of Simple Flows.
Mass Transfer Coefficient
Sedimentation of a polydisperse non- Brownian suspension Krzysztof Sadlej IFT UW IPPT PAN, May 16 th 2007.
Integrating CFD and Experiments. 8-9 Sept. 2003, Glasgow.. NUMERICAL SIMULATION OF FLUID- STRUCTURE INTERACTIONS ON LONG BODIES Mike Graham, Tim Kendon.
Unit 1: Fluid Dynamics An Introduction to Mechanical Engineering: Part Two Fluid dynamics Learning summary By the end of this chapter you should have learnt.
A RANS Based Prediction Method of Ship Roll Damping Moment Kumar Bappaditya Salui Supervisors of study: Professor Dracos Vassalos and Dr. Vladimir Shigunov.
1 Reduced-Order Modeling in the Frequency Domain for Actuated Flows Guy Ben-Dov* and Arne J. Pearlstein Department of Mechanical Science and Engineering.
BOUNDARY LAYERS Viscous effects confined to within some finite area near the boundary → boundary layer In unsteady viscous flows at low Re (impulsively.
Title: SHAPE OPTIMIZATION OF AXISYMMETRIC CAVITATOR IN PARTIALY CAVITATING FLOW Department of Mechanical Engineering Ferdowsi University of Mashhad Presented.
CMP Modeling – Current Status Goal is to develop a comprehensive CMP model that complements experimental program Begin with hydrodynamic slurry flow model.
1 Fluidic Load Control for Wind Turbine Blades C.S. Boeije, H. de Vries, I. Cleine, E. van Emden, G.G.M Zwart, H. Stobbe, A. Hirschberg, H.W.M. Hoeijmakers.
Modeling of the Unsteady Separated Flow over Bilge Keels of FPSO Hulls under Heave or Roll Motions Yi-Hsiang Yu 09/23/04 Copies of movies/papers and today’s.
Challenges in Wind Turbine Flows
CE 1501 Flow Over Immersed Bodies Reading: Munson, et al., Chapter 9.
MECH 221 FLUID MECHANICS (Fall 06/07) Chapter 8: BOUNDARY LAYER FLOWS
A Numerical Solution to the Flow Near an Infinite Rotating Disk White, Section MAE 5130: Viscous Flows December 12, 2006 Adam Linsenbardt.
CFD Study of the Development of Vortices on a Ring Wing
Stokes Solutions to Low Reynolds Number Flows
Dynamics of a Gas Bubble in an Inclined Channel at Finite Reynolds Number Catherine Norman Michael J. Miksis Northwestern University.
Wind Energy Program School of Aerospace Engineering Georgia Institute of Technology Computational Studies of Horizontal Axis Wind Turbines PRINCIPAL INVESTIGATOR:
Lecture 6 The boundary-layer equations
School of Aerospace Engineering MITE Numerical Simulation of Centrifugal Compressor Stall and Surge Saeid NiaziAlex SteinLakshmi N. Sankar School of Aerospace.
Chapter 10 Approximate Solutions of the Navier-Stokes Equation
Application of Compact- Reconstruction WENO Schemes to the Navier-Stokes Equations Alfred Gessow Rotorcraft Center Aerospace Engineering Department University.
Indian Institute of Space Science and Technology STUDY OF EFFECT OF GAS INJECTION OVER A TORPEDO ON FLOW-FIELD USING CFD.
A V&V Overview of the 31st Symposium on Naval Hydrodynamics
Ship Hydrodynamics - Resistance
Numerical Investigation of Turbulent Flows Using k-epsilon
Date of download: 10/24/2017 Copyright © ASME. All rights reserved.
VALIDATION OF A HELICOIDAL VORTEX MODEL WITH THE NREL UNSTEADY AERODYNAMIC EXPERIMENT James M. Hallissy and Jean-Jacques Chattot University of California.
Presentation transcript:

Modeling of Oscillating Flow Past a Vertical Plate Spyros A. Kinnas, Yi-Hsiang Yu, Hanseong Lee, Karan Kakar Ocean Engineering Group, Department of Civil Engineering The University of Texas at Austin, Austin, TX, USA The 13th International Offshore and Polar Engineering Conference ISOPE-2003, Hawaii, May25-30, 2003

Overview Introduction Governing Equations, Boundary Conditions and Numerical Formulation. Comparison of results from the 2D unsteady Euler, Navier-Stokes Solvers with measurements. Visualization of separated flow field. Summary and future work.

Introduction Motivation & Objectives  Develop and validate a method for the prediction of the effects of bilge keels on FPSO Hull motion.  Understand the physics of the unsteady separated flow about the bilge keels of a hull subject to roll motions, and predict the corresponding hydrodynamic coefficients.

Motivation & Objectives In this work, we apply and validate our model to a bilge keel (vertical plate) subject to horizontal sinusoidal inflow.

Literature Review Numerical Work: - - Gentaz et al Korpus and Falzarano Vassalos et al Yeung et al. 1992, 1996, 1998, 2000, 2002 Experiments on Vertical Plate: -Keulegan and Carpenter Sarpkaya and O’Keefe 1995

Numerical Formulation Governing Equation Non-Dimensional Navier-Stokes equations KC: Keulegan-Carpenter number, Re: Reynolds number,

Numerical Method Finite Volume Method Ni’s Lax-Wendroff Method for time Artificial dissipation (viscosity) ~ only in the case of Euler solver SIMPLE Method for pressure correction

Euler and Navier-Stokes Solver Choi & Kinnas 2000, Choi PhD thesis Development of Euler Solver and Navier-Stokes solver. Kakar MS thesis FPSO hull motion - Application of unsteady 2D Euler solver of flow over bilge keels for FPSO hull motion. artificial viscosity  Euler Solver ~ Applied artificial viscosity  Navier-Stokes Solver ~ Viscous terms

Force Calculation on the plate Morison’s equation as follows [Sarpkaya and O’Keefe (1995)]

Results Convergence Study At KC=1

Convergence Study At KC=1

Force History comparison

Drag coefficient for a range of KC (0.5 < KC < 10)

Inertia coefficient for a range of KC (0.5 < KC < 10)

Streamline & vorticity contour at 0*T/4 for KC=1 Streamline & vorticity contour at 1*T/4 for KC=1 ESNS ESNS

Streamline & vorticity contour at 2*T/4 for KC=1 Streamline & vorticity contour at 3*T/4 for KC=1 ES NS ESNS

KC=1

KC=10

Summary  A finite volume method was applied to the solution of oscillating flow around a vertical flat plate. The same plate and tunnel dimensions as in the experiment of Sarpkaya and O'Keefe have been used.  It was found, that either the Euler or the Navier- Stokes solver produced force coefficients and separated flow fields which were close to each other and also close to the measurements, especially for lower values of the Keulegan- Carpenter number.

Summary  For higher KC numbers, the viscous terms start to be more important, and the effects of turbulence may need to be taken into account.  The Euler solver has already been extended in the case of FPSO hull sections, with and without bilge keels, and some preliminary results have been presented in Kinnas, et al., 12th Offshore Symposium, Texas section of the SNAME, 2003.

Future Work Further investigations with different Re numbers and KC numbers. Continue with the extension in the case of FPSO hull sections to study the effects of bilge keels.

The End