VTT TECHNICAL RESEARCH CENTRE OF FINLAND 1 Fluid-Structure Interaction Calculations of a Large-Break Loss-of-Coolant Accident Antti Timperi Kul-34.4551.

Slides:



Advertisements
Similar presentations
FE analysis with shell and axisymmetric elements E. Tarallo, G. Mastinu POLITECNICO DI MILANO, Dipartimento di Meccanica.
Advertisements

Nathan N. Lafferty, Martin L. deBertodano,
Flow Disturbance of Flow due to Bends and Obstacles, etc. Time Transients and Spatial Distribution of Fluid Force on Structure Surface FLAVOR-3D: 3-D Fluid.
Aero-Hydrodynamic Characteristics
By Paul Delgado. Motivation Flow-Deformation Equations Discretization Operator Splitting Multiphysics Coupling Fixed State Splitting Other Splitting Conclusions.
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.
SIEMENS, MUELHEIM 1 1 Fluid-Structure Interaction for Combustion Systems Artur Pozarlik Jim Kok FLUISTCOM SIEMENS, MUELHEIM, 14 JUNE 2006.
Modelling FSI problems in ANSYS Fluent via UDF
MAE 5130: VISCOUS FLOWS Introduction to Boundary Layers
ANALYSES OF STABILITY OF CAISSON BREAKWATERS ON RUBBLE FOUNDATION EXPOSED TO IMPULSIVE WAVE LOADS Burcharth, Andersen & Lykke Andersen ICCE 2008, Hamburg,
LECTURE SERIES on STRUCTURAL OPTIMIZATION Thanh X. Nguyen Structural Mechanics Division National University of Civil Engineering
October 25-27, th International QUENCH Workshop 1 Top Flooding Experiments and Modeling Estelle Brunet-Thibault (EDF), Serge Marguet (EDF)
An Introduction to Multiscale Modeling Scientific Computing and Numerical Analysis Seminar CAAM 699.
Coupling Continuum Model and Smoothed Particle Hydrodynamics Methods for Reactive Transport Yilin Fang, Timothy D Scheibe and Alexandre M Tartakovsky Pacific.
Coupled Fluid-Structural Solver CFD incompressible flow solver has been coupled with a FEA code to analyze dynamic fluid-structure coupling phenomena CFD.
Thermo-fluid Analysis of Helium cooling solutions for the HCCB TBM Presented By: Manmeet Narula Alice Ying, Manmeet Narula, Ryan Hunt and M. Abdou ITER.
3-D Large Eddy Simulation for Jet Noise Prediction A.Uzun, G. Blaisdell, A. Lyrintzis School of Aeronautics and Astronautics Purdue University Funded by.
Finite Element Method in Geotechnical Engineering
Fracture and Fragmentation of Thin-Shells Fehmi Cirak Michael Ortiz, Anna Pandolfi California Institute of Technology.
Image courtesy of National Optical Astronomy Observatory, operated by the Association of Universities for Research in Astronomy, under cooperative agreement.
MCE 561 Computational Methods in Solid Mechanics
© 2011 Autodesk Freely licensed for use by educational institutions. Reuse and changes require a note indicating that content has been modified from the.
FUNDAMENTAL EQUATIONS, CONCEPTS AND IMPLEMENTATION
The Finite Element Method
By Paul Delgado Advisor – Dr. Vinod Kumar Co-Advisor – Dr. Son Young Yi.
RF-Accelerating Structure: Cooling Circuit Modeling Riku Raatikainen

26-27 September 2005 Colloque GDR Intéraction Fluide-Structure, Sophia Antipolis 1 Fluid-Structure Interaction Modelling with Europlexus Fast Dynamics.
© 2011 Autodesk Freely licensed for use by educational institutions. Reuse and changes require a note indicating that content has been modified from the.
1 SIMULATION OF VIBROACOUSTIC PROBLEM USING COUPLED FE / FE FORMULATION AND MODAL ANALYSIS Ahlem ALIA presented by Nicolas AQUELET Laboratoire de Mécanique.
Haptics and Virtual Reality
Thermal Model of MEMS Thruster Apurva Varia Propulsion Branch Code 597.
Brookhaven Science Associates U.S. Department of Energy MUTAC Review April , 2004, LBNL Target Simulation Roman Samulyak, in collaboration with.
Fig.6 Next Generation Airplane ( ■ Design of Next Generation Airplanes - Lightweight airframe - High aspect ratio.
Global Analysis of Floating Structures – M.H. Kim
The Finite Element Method A Practical Course
A particle-gridless hybrid methods for incompressible flows
August 14 th, 2012 Comparison of compressible explicit density-based and implicit pressure-based CFD methods for the simulation of cavitating flows Romuald.
1 MICRO FLOWS: AN INTRODUCTION Michael Shusser. 2 SIZE RANGES OF MACRO, MICRO, AND NANO DEVICES.
1 © Dassault Systèmes Ι Confidential Information Effectiveness of Tetrahedral Finite Elements in Modeling Tread Patterns for Rolling Simulations Harish.
IAEA Meeting on INPRO Collaborative Project “Performance Assessment of Passive Gaseous Provisions (PGAP)” December, 2011, Vienna A.K. Nayak, PhD.
A STUDY OF THE DYNAMIC RESPONSE OF A FRACTURED TUNNEL TO PLANE WAVES Pei-cheng Xu SwRI, SanAntonio,Texas Sept. 7, 2000.
A RANS Based Prediction Method of Ship Roll Damping Moment Kumar Bappaditya Salui Supervisors of study: Professor Dracos Vassalos and Dr. Vladimir Shigunov.
Silesian University of Technology in Gliwice Inverse approach for identification of the shrinkage gap thermal resistance in continuous casting of metals.
Numerical Investigation of Hydrogen Release from Varying Diameter Exit
HEAT TRANSFER FINITE ELEMENT FORMULATION
Advanced Simulation Techniques for the coupled Fatigue and NVH Optimization of Engines. K+P Software, Schönbrunngasse 24, A Graz / Austria Tel.:
COMPUTER SIMULATION OF BLOOD FLOW WITH COMPLIANT WALLS  ITC Software All rights reserved.
STUDY OF THE AIR TEMPERATURE AND VELOCITY AROUND THE ATLAS MUON CHAMBERS Emma Vigo Castellvi ST/CV Design.
(*) CIMNE: International Center for Numerical Methods in Engineering, Barcelona, Spain Innovative Finite Element Methods For Aeroelastic Analysis Presented.
ERMSAR 2012, Cologne March 21 – 23, 2012 Experimental and computational studies of the coolability of heap-like and cylindrical debris beds E. Takasuo,
DEWEK 2004 Lecture by Aero Dynamik Consult GmbH, Dipl. Ing. Stefan Kleinhansl ADCoS – A Nonlinear Aeroelastic Code for the Complete Dynamic Simulation.
MODELLING OF THE HYDRO- ACOUSITC SIGNAL AS A TSUNAMI PRECURSOR F. Chierici (IRA-INAF) L. Pignagnoli (ISMAR-CNR) D. Embriaco (INGV) Nearest meeting, Berlin.
Institute of Safety Research Member Institution of the Scientific Association Gottfried Wilhelm Leibniz DYN3D/ATHLET AND ANSYS CFX CALCULATIONS OF THE.
Lecture Objectives: Review discretization methods for advection diffusion equation –Accuracy –Numerical Stability Unsteady-state CFD –Explicit vs. Implicit.
CFX Slide serial no 1 © 2003 ANSYS CFX CFX-5.6 Multiphase Course Free Surface Lecture 5 Free Surface Flow.
Heat Exchanger Design Cooler E-100 Heater E-108.
CAD and Finite Element Analysis Most ME CAD applications require a FEA in one or more areas: –Stress Analysis –Thermal Analysis –Structural Dynamics –Computational.
Universität Dortmund Fakultät für Mathematik IAM technische universität dortmund A numerical set-up for benchmarking and optimization of fluid-structure.
M. Khalili1, M. Larsson2, B. Müller1
Task2: Liquid Metal Target Thermo hydraulic and structural analysis of the Eurisol liquid metal target Ashrafi-Nik M. * C.E.R.N, AB Department, ATB Group.
CFD Simulation Investigation of Natural Gas Components through a Drilling Pipe RASEL A SULTAN HOUSSEMEDDINE LEULMI.
Panel Discussion: Discussion on Trends in Multi-Physics Simulation
CHAPTER 2 - EXPLICIT TRANSIENT DYNAMIC ANALYSYS
Finite Element Method in Geotechnical Engineering
Chamber Dynamic Response Modeling
Prepared BY: Helwan University Faculty Of Engineering
Data Structures for Efficient and Integrated Simulation of Multi-Physics Processes in Complex Geometries A.Smirnov MulPhys LLC github/mulphys
Modeling and experimental study of coupled porous/channel flow
Numerical Investigation of Hydrogen Release from Varying Diameter Exit
Presentation transcript:

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 1 Fluid-Structure Interaction Calculations of a Large-Break Loss-of-Coolant Accident Antti Timperi Kul Postgraduate Seminar in Fluid Mechanics

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 2 Introduction t Aim of the work has been to find practical tools for analyzing Fluid- Structure Interaction (FSI) problems found in nuclear and also other industries. t Large-Break Loss-Of-Coolant Accident (LBLOCA) is an important Design Basis Accident (DBA) situation. Rapid depressurization of the primary circuit causes loads on the reactor internals. t The motivation for studying more advanced simulation methods for analysis of DBA situations is to get more accurate, so-called ”best estimate”, analysis results. t LBLOCA in the VVER-440 type Pressurized Water Reactor (PWR) was used as a test case in earlier calculations. t Validation of LBLOCA calculations against the German HDR experiments is presented in the following.

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 3 HDR (Heißdampfreaktor) test facility vs. PWR p = 110bar T core = 308ºC T downcomer = 240ºC p = 125bar T hot leg = 295ºC T cold leg = 265ºC

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 4 HDR test facility vs. PWR (cont.) QuantityHDRPWR Pressure, MPa P 0 − P sat, MPa5.57 T core − T downc, °C0…5030 Break diameter, m Break opening time, ms1…2? Core barrel length, m Core barrel thickness, mm2350 Core barrel diameter, m Maximum stress, MPa Maximum displacement, mm24…5

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 5 Overview of the calculations Apros Boundary condition Star-CD Propagation of pressure transient MpCCI Wall position MpCCI Pressure loads Abaqus Stresses and deformation of structures t MpCCI (Mesh-based parallel Code Coupling Interface) is middleware that has been developed at the Fraunhofer Institute t Motion of the core barrel is taken into account in the CFD calculation of pressure.

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 6 Pressure at the break location, measured data and APROS calculations:

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 7 Star-CD CFD model t PISO (“Pressure Implicit with Splitting of Operators”) pressure correction algorithm. t Water is treated as compressible: t Crank-Nicholson method for temporal discretization and MARS/central/central- upwind differencing for spatial discretization. t Standard k-ε model and standard wall functions for modeling turbulence. ~ hex cells

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 8 ABAQUS structural model t Fully linear model with ~ node hexahedral elements. t Continuum shell and solid elements are used for matching geometry between CFD and FEM. t Implicit Newmark direct time integration. t Small amount of stiffness proportional damping was included to the RPV wall: 2 % of critical damping at frequency 1000 Hz.

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 9 CFD-FEM calculation t Explicit, sequential solution strategy, i.e. loose numerical coupling. Stable (usually) in LBLOCA calculations, but has been found unstable in certain other applications. t Interpolation is used for transferring the coupling quantities between the CFD and FEM meshes. t Coupling quantities local fluid pressure (CFD → FEM) and nodal coordinates (FEM → CFD). Data is exchanged in each time step (∆t = 10 μs). t Star-CD analysis has a moving mesh, internal CFD mesh is smoothed by mesh morpher of MpCCI.

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 10 CFD-FEM calculation (cont.) 1. Star-CD sends pressure load corresponding to initial conditions to ABAQUS. 2. ABAQUS simulation advances one time step. 3. ABAQUS sends new nodal coordinates to Star-CD. 4. Star-CD simulation advances one time step. 5. Star-CD sends new pressure load to ABAQUS. The sequence 2-5 is repeated for the duration of the simulation.

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 11 Acoustic-structural calculation t Models sound wave propagation and added mass effects, but effects of bulk flow, e.g. dynamic pressure, are neglected. Assumes small displacements. t Fluid is described as an acoustic medium (three-dimensional wave equation for pressure): t Linear constitutive behavior for the fluid (K is bulk modulus): t Reduces to Laplace equation for incompressible fluid (low- frequency structural motion):

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 12 Acoustic-structural calculation (cont.) t ”Volumetric drag” γ can be added to model bulk viscosity or resistive porous material: t Fluid pressure and structural displacement are coupled on the fluid-structure interface: t A single system of equations is solved, i.e. the fluid and structure domains are solved simultaneously:

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 13 Pressure in the reactor, CFD-FEM calculation: p [Pa] t = 5 ms10 ms15 ms20 ms25 ms

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 14 Stresses and deformations (x200), CFD-FEM calculation: s [Pa] t = 0 ms5 ms20 ms40 ms115 ms

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 15 Pressures, experiment vs. CFD-FEM: z = m,  = 90°z = m,  = 270° z = m (core) z = m,  = 90°

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 16 Displacements of the core barrel, experiment vs. CFD-FEM: z = m,  = 90°z = m,  = 270° z = m,  = 90°z = m,  = 90°

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 17 Pressures, experiment vs. acoustic model: z = m,  = 90°z = m,  = 90° z = m (core) z = m,  = 90°

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 18 Displacements of the core barrel, experiment vs. acoustic model: z = m,  = 90°z = m,  = 270° z = m,  = 90°z = m,  = 270°

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 19 Conclusions on CFD-FEM calculations t The calculated fluid and structural quantities were in fairly good agreement with the experiment. Especially the overall structural behavior of the core barrel was predicted well. t The most significant phenomena of the LBLOCA were well captured by the calculation during the first 100 ms, when the largest loads occurred. t Strong boiling increased pressure significantly after 120 ms, which caused deviation of measured and calculated pressures (single- phase CFD model was used).

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 20 Conclusions on acoustic-structural calculations t The results were in good agreement with the experiment and with the CFD-FEM calculation during the early phase of the simulation when the flow velocity was negligible. t Loads and structural effects were highly over-predicted in the later phase when the effect of bulk flow of water became significant. t The method is considerably more efficient and more robust compared to the CFD-FEM method. t May be considered as an alternative tool for comparison calculations in future work.

VTT TECHNICAL RESEARCH CENTRE OF FINLAND 21 General conclusions t Fairly coarse numerical meshes were sufficient for capturing the most important fluid transient and FSI phenomena. t The single-phase assumption used in the FSI calculations was adequate during the phase when the largest structural effects occurred, i.e. until ~ 100 ms. t The experiment had probably an unrealistically short break opening time, i.e. ~ 1 ms. Opening times of 15 ms and longer have been proposed in the literature.