Compressible Flow Modeling Occurring in a Depressurization Process

Similar documents
Introduction to Aerodynamics. Dr. Guven Aerospace Engineer (P.hD)

Introduction to Fluid Mechanics. Chapter 13 Compressible Flow. Fox, Pritchard, & McDonald

DESIGN & COMPUTATIONAL FLUID DYNAMICS ANALYSES OF AN AXISYMMETRIC NOZZLE AT TRANSONIC FREE STREAM CONDITIONS

CHAPTER 7 SEVERAL FORMS OF THE EQUATIONS OF MOTION

Mass flow determination in flashing openings

CFD in COMSOL Multiphysics

Direct Modeling for Computational Fluid Dynamics

Introduction to Chemical Engineering Thermodynamics. Chapter 7. KFUPM Housam Binous CHE 303

Modeling of Humidification in Comsol Multiphysics 4.4

Transport equation cavitation models in an unstructured flow solver. Kilian Claramunt, Charles Hirsch

Differential relations for fluid flow

Lesson 6 Review of fundamentals: Fluid flow

Mechanical Engineering Science for Medical Engineers Level: 4 Credit value: 8 GLH: 62 TQT: 80

Detailed Outline, M E 320 Fluid Flow, Spring Semester 2015

Effect of Gas Flow Rate and Gas Composition in Ar/CH 4 Inductively Coupled Plasmas

CFD ANALYSIS OF CD NOZZLE AND EFFECT OF NOZZLE PRESSURE RATIO ON PRESSURE AND VELOCITY FOR SUDDENLY EXPANDED FLOWS. Kuala Lumpur, Malaysia

Reversibility, Irreversibility and Carnot cycle. Irreversible Processes. Reversible Processes. Carnot Cycle

AA214B: NUMERICAL METHODS FOR COMPRESSIBLE FLOWS

Multi-source Aeroacoustic Noise Prediction Method

On the Effect of Variable Opening Geometries, and Operating Conditions on High Pressure Hydrogen Releases: Ignition Risks

Helium two-phase flow in a thermosiphon open loop

3. FORMS OF GOVERNING EQUATIONS IN CFD

Biological Process Engineering An Analogical Approach to Fluid Flow, Heat Transfer, and Mass Transfer Applied to Biological Systems

Exercise 7 - Fluiddynamic Systems

FLOWS IN LIQUID FOAMS

Problem C3.5 Direct Numerical Simulation of the Taylor-Green Vortex at Re = 1600

1. INTRODUCTION TO CFD SPRING 2019

Chapter 1: Basic Concepts

dynamics of f luids in porous media

For example an empty bucket weighs 2.0kg. After 7 seconds of collecting water the bucket weighs 8.0kg, then:

AER1310: TURBULENCE MODELLING 1. Introduction to Turbulent Flows C. P. T. Groth c Oxford Dictionary: disturbance, commotion, varying irregularly

A Phase Field Approach to Model Laser Power Control in Spot Laser Welding

Fluid Mechanics - Course 123 COMPRESSIBLE FLOW

Contents. I Introduction 1. Preface. xiii

Three-dimensional simulation of cavitating flows in piping systems R. Klasinc, R. Reitbauer, H. Knoblauch

William В. Brower, Jr. A PRIMER IN FLUID MECHANICS. Dynamics of Flows in One Space Dimension. CRC Press Boca Raton London New York Washington, D.C.

Outlines. simple relations of fluid dynamics Boundary layer analysis. Important for basic understanding of convection heat transfer

Science. Circular Motion. Atomic Structure and Nuclear Chemistry. Kinematics; Motion in One and Two Dimensions

Dispersed Multiphase Flow Modeling using Lagrange Particle Tracking Methods Dr. Markus Braun Ansys Germany GmbH

Application of COMSOL Multiphysics in Transport Phenomena Educational Processes

V/ t = 0 p/ t = 0 ρ/ t = 0. V/ s = 0 p/ s = 0 ρ/ s = 0

Group #4 (Firko, Johnson)

Hervé Guillard, INRIA Projet Smash, B.P. 93, Sophia-Antipolis Cedex, France,

EFFECT OF LIQUID PHASE COMPRESSIBILITY ON MODELING OF GAS-LIQUID TWO-PHASE FLOWS USING TWO-FLUID MODEL

APPLIED FLUID DYNAMICS HANDBOOK

Physics Overview. High School Core Science Standards Physics

Contents. Preface... xvii

Computational Analysis of an Imploding Gas:

Influence of high temperature gradient on turbulence spectra

Fluid Mechanics Theory I

Further Applications of Newton s Laws - Friction Static and Kinetic Friction

Micro-scale modelling of internally

Understanding Transport Phenomena Concepts in Chemical Engineering with COMSOL Multiphysics

Comparison of Fluid Flow and Heat Transfer for 1D and 2D Models of an In-Line Pulse Tube Refrigerator

Modeling and Analysis of Dynamic Systems

A Discussion of Low Reynolds Number Flow for the Two-Dimensional Benchmark Test Case

.u= 0 ρ( u t +(u. )u)= ρ g p+.[µ( u+ t u)]

Calculating equation coefficients

KINETIC BOOKS PHYSICS CORRELATED TO SOUTH CAROLINA PHYSICS STANDARDS CORRELATION

Thermal Analysis of Fairchild Dornier 728Jet Wing/Fuselage Interface using MSC.Patran Thermal. Paper number D. Konopka, J. Hyer, A.

Boundary-Layer Theory

Model Studies on Slag-Metal Entrainment in Gas Stirred Ladles

1. INTRODUCTION TO CFD SPRING 2018

A drop forms when liquid is forced out of a small tube. The shape of the drop is determined by a balance of pressure, gravity, and surface tension

ENGINEERING FLUID MECHANICS. CHAPTER 1 Properties of Fluids

Assessment of Implicit Implementation of the AUSM + Method and the SST Model for Viscous High Speed Flow

A Plasma Torch Model

Analysis of Head Loss in Pipe System Components: Quasi-one-Dimensional Nozzle Flow

An Overview of Impellers, Velocity Profile and Reactor Design

Fluid Dynamics Exercises and questions for the course

Module 2 : Convection. Lecture 12 : Derivation of conservation of energy

Simulation of a Thermo-Acoustic Refrigerator

TAU Extensions for High Enthalpy Flows. Sebastian Karl AS-RF

Theoretical Gas Flow through Gaps in Screw-type Machines

CHAPTER 7 NUMERICAL MODELLING OF A SPIRAL HEAT EXCHANGER USING CFD TECHNIQUE

Table of Contents. Preface... xiii

vector H. If O is the point about which moments are desired, the angular moment about O is given:

Structure Formation and Particle Mixing in a Shear Flow Boundary Layer

Computational Engineering

Plasma Modeling with COMSOL Multiphysics

An Introduction to COMSOL Multiphysics v4.3b & Subsurface Flow Simulation. Ahsan Munir, PhD Tom Spirka, PhD

PTT 277/3 APPLIED THERMODYNAMICS SEM 1 (2013/2014)

SPC 407 Sheet 5 - Solution Compressible Flow Rayleigh Flow

Simplified Model of WWER-440 Fuel Assembly for ThermoHydraulic Analysis

DESIGN AND CFD ANALYSIS OF A CENTRIFUGAL PUMP

Flow Focusing Droplet Generation Using Linear Vibration

2. Conservation Equations for Turbulent Flows

Several forms of the equations of motion

Computational Astrophysics

S.E. (Mech.) (First Sem.) EXAMINATION, (Common to Mech/Sandwich) FLUID MECHANICS (2008 PATTERN) Time : Three Hours Maximum Marks : 100

CHAPTER 5 MASS AND ENERGY ANALYSIS OF CONTROL VOLUMES

2. FLUID-FLOW EQUATIONS SPRING 2019

An Overview of Fluid Animation. Christopher Batty March 11, 2014

Hydraulics Prof. Dr. Arup Kumar Sarma Department of Civil Engineering Indian Institute of Technology, Guwahati

Prediction of CO Burnout using a CHEMKIN based Network Tool

Soft Bodies. Good approximation for hard ones. approximation breaks when objects break, or deform. Generalization: soft (deformable) bodies

1. For an ideal gas, internal energy is considered to be a function of only. YOUR ANSWER: Temperature

Lecture23. Flowmeter Design.

Fundamentals of Fluid Mechanics

Investigation of an implicit solver for the simulation of bubble oscillations using Basilisk

Transcription:

Compressible Flow Modeling Occurring in a Depressurization Process Frédéric Viry 1, Vincent Bruyere 1, Thomas Paris 2, Patrick Namy 1 1 SIMTEC, 8 rue Duployé, Grenoble, 38100, France, +33 9 53 51 45 60 vincent.bruyere@simtecsolution.fr 2 CEA DAM, Valduc, Is-sur-Tille, 21120, France

SIMTEC www.simtecsolution.fr SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 2

SIMTEC www.simtecsolution.fr French company (founded in 2006) 4 Ph. D. Engineers SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 2

SIMTEC www.simtecsolution.fr French company (founded in 2006) 4 Ph. D. Engineers Experts in Modeling COMSOL Certified Consultants CFD Structural mechanics Electromagnetism Heat transfer Chemical engineering SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 2

SIMTEC www.simtecsolution.fr French company (founded in 2006) 4 Ph. D. Engineers Experts in Modeling COMSOL Certified Consultants CFD Structural mechanics Electromagnetism Heat transfer Chemical engineering Services Numerical modeling Custom-made training sessions Modeling assistance SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 2

SIMTEC www.simtecsolution.fr French company (founded in 2006) 4 Ph. D. Engineers Experts in Modeling COMSOL Certified Consultants CFD Structural mechanics Electromagnetism Heat transfer Chemical engineering Services Numerical modeling Custom-made training sessions Modeling assistance SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 2

Problem Statement SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 3

Problem Statement Gas particle High pressure tank (initially) Low pressure tank (initially) SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 3

Problem Statement Gas particle High pressure tank (initially) Low pressure tank (initially) SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 3

Problem Statement Gas particle High pressure tank (initially) Low pressure tank (initially) SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 3

Problem Statement Gas particle High pressure tank (initially) Low pressure tank (initially) SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 3

Problem Statement Gas particle High pressure tank (initially) Low pressure tank (initially) Model the flow to: Study the sensitivity to the dimensions of the system; Understand the behavior of the gas flow, the time to reach the equilibrium; Coupling with others physics: e.g. chemistry, etc SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 3

The Flow Study and its Issues SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 4

The Flow Study and its Issues Navier-Stokes Equations (Mass and momentum balances) Energy balance Precise description of the movement! Constitutive law SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 4

The Flow Study and its Issues Navier-Stokes Equations (Mass and momentum balances) Energy balance Precise description of the movement! Constitutive law Turbulent flow : difficult to capture numerically SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 4

The Flow Study and its Issues Navier-Stokes Equations (Mass and momentum balances) Energy balance Precise description of the movement! Constitutive law Turbulent flow : difficult to capture numerically Shockwaves appearing at the sound speed : it breaks the continuity hypothesis! SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 4

Overview 5

Overview Model derived from an existing 1D approach A Simplified Model for Real Gas Expansion Between Two Reservoirs Connected by a Thin Tube, S. Charton, V.Blet et J. P. Corriou, 1995 5

Overview Model derived from an existing 1D approach A Simplified Model for Real Gas Expansion Between Two Reservoirs Connected by a Thin Tube, S. Charton, V.Blet et J. P. Corriou, 1995 5

Overview Model derived from an existing 1D approach A Simplified Model for Real Gas Expansion Between Two Reservoirs Connected by a Thin Tube, S. Charton, V.Blet et J. P. Corriou, 1995 Tanks as points 5

Overview Model derived from an existing 1D approach A Simplified Model for Real Gas Expansion Between Two Reservoirs Connected by a Thin Tube, S. Charton, V.Blet et J. P. Corriou, 1995 Tanks as points Pipe modeled by a segment No turbulences to handle 5

Overview Model derived from an existing 1D approach A Simplified Model for Real Gas Expansion Between Two Reservoirs Connected by a Thin Tube, S. Charton, V.Blet et J. P. Corriou, 1995 Tanks as points Pipe modeled by a segment Location of the discontinuity given by a theoretical development No turbulences to handle Possibility to introduce the discontinuity 5

Overview Model derived from an existing 1D approach A Simplified Model for Real Gas Expansion Between Two Reservoirs Connected by a Thin Tube, S. Charton, V.Blet et J. P. Corriou, 1995 Tanks as points Pipe modeled by a segment Location of the discontinuity given by a theoretical development No turbulences to handle Possibility to introduce the discontinuity How to model the gas flow, the tanks and the discontinuity within COMSOL? 5

Gas Flow Within the Pipe 6

Gas Flow Within the Pipe Mass balance Mass variation 6

Gas Flow Within the Pipe Mass balance Mass variation Momentum balance Mass acceleration Friction forces (w/ viscosity) Pressure drop 6

Gas Flow Within the Pipe Mass balance Mass variation Momentum balance Mass acceleration Friction forces (w/ viscosity) Pressure drop Energy balance Internal energy variation Heat transfer by diffusion Friction forces work Pressure work 6

Gas Flow Within the Pipe Mass balance Mass variation Momentum balance Mass acceleration Friction forces (w/ viscosity) Pressure drop Energy balance Internal energy variation Heat transfer by diffusion Friction forces work Pressure work Constitutive law (ideal gas assumption) 6

Gas Flow Within the Pipe Mass balance Mass variation Momentum balance Mass acceleration Friction forces (w/ viscosity) Pressure drop Energy balance Internal energy variation Heat transfer by diffusion Friction forces work Pressure work Constitutive law (ideal gas assumption) ODE and PDE interfaces or Pipe Flow Module interfaces 6

Tanks as Points 7

Tanks as Points Exterior Tank in 0D Junction with the pipe 7

Tanks as Points Exterior 0D means a spatial uniformity of: pressure, temperature and density! Tank in 0D Junction with the pipe 7

Tanks as Points Exterior 0D means a spatial uniformity of: pressure, temperature and density! Tank in 0D Junction with the pipe Mass Balance Mass variation Mass flow at the junction 7

Tanks as Points Exterior 0D means a spatial uniformity of: pressure, temperature and density! Tank in 0D Junction with the pipe Mass Balance Energy balance Mass variation Mass flow at the junction Internal energy variation Heat transfer by convection Transfer of Heat exchanges with kinetic energy the exterior 7

Tanks as Points Exterior 0D means a spatial uniformity of: pressure, temperature and density! Tank in 0D Junction with the pipe Mass Balance Energy balance Mass variation Mass flow at the junction Internal energy variation Constitutive law (ideal gas assumption) Heat transfer by convection Transfer of Heat exchanges with kinetic energy the exterior 7

Tanks as Points Exterior 0D means a spatial uniformity of: pressure, temperature and density! Tank in 0D Junction with the pipe Mass Balance Energy balance Mass variation Mass flow at the junction Internal energy variation Constitutive law (ideal gas assumption) Heat transfer by convection Transfer of Heat exchanges with kinetic energy the exterior ODE interface 7

Handle the Discontinuity 8

Handle the Discontinuity Subsonic 8

Handle the Discontinuity Flow saturated to Mach 1 (second law of thermodynamics) Critical up Subsonic 8

Handle the Discontinuity Flow saturated to Mach 1 (second law of thermodynamics) Critical up Subsonic Sonic 8

Handle the Discontinuity Flow saturated to Mach 1 (second law of thermodynamics) Critical up Subsonic Sonic Critical down 8

Handle the Discontinuity Flow saturated to Mach 1 (second law of thermodynamics) Critical up Subsonic Sonic Critical down 8

Handle the Discontinuity Flow saturated to Mach 1 (second law of thermodynamics) Critical up Subsonic Sonic Critical down Conditions modified because of numerical issues 8

Handle the Discontinuity Flow saturated to Mach 1 (second law of thermodynamics) Critical up Subsonic Sonic Critical down Conditions modified because of numerical issues 8

Handle the Discontinuity Flow saturated to Mach 1 (second law of thermodynamics) Critical up Subsonic Sonic Critical down Conditions modified because of numerical issues 8

Handle the Discontinuity Flow saturated to Mach 1 (second law of thermodynamics) Critical up Subsonic Sonic Critical down Conditions modified because of numerical issues Events interface 8

Numerical Aspects 9

Numerical Aspects Space Discretization 9

Numerical Aspects Space Discretization Study of sensivity to the mesh At least homogeneous 1000 nodes Avoid numerical loss of mass during the discharge 9

Numerical Aspects Space Discretization Time Discretization Study of sensivity to the mesh At least homogeneous 1000 nodes Avoid numerical loss of mass during the discharge 9

Numerical Aspects Space Discretization Time Discretization Study of sensivity to the mesh Speed of sound reached very quickly At least homogeneous 1000 nodes Small timestep at the beginning of the simulation (about 10-7 s) Avoid numerical loss of mass during the discharge 9

Numerical Aspects Space Discretization Time Discretization Study of sensivity to the mesh Speed of sound reached very quickly At least homogeneous 1000 nodes Avoid numerical loss of mass during the discharge Small timestep at the beginning of the simulation (about 10-7 s) Gas less agitated after that: COMSOL chooses well its timestep automatically 9

Theoretical Validation SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 10

Theoretical Validation Theoretical results exist by neglecting the friction forces A. Lallemand, Ecoulements monodimensionnels des fluides compressibles, Techniques de l'ingénieur, 2014 SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 10

Theoretical Validation Theoretical results exist by neglecting the friction forces A. Lallemand, Ecoulements monodimensionnels des fluides compressibles, Techniques de l'ingénieur, 2014 SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 10

Theoretical Validation Theoretical results exist by neglecting the friction forces A. Lallemand, Ecoulements monodimensionnels des fluides compressibles, Techniques de l'ingénieur, 2014 SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 10

Theoretical Validation Theoretical results exist by neglecting the friction forces A. Lallemand, Ecoulements monodimensionnels des fluides compressibles, Techniques de l'ingénieur, 2014 SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 10

Theoretical Validation Theoretical results exist by neglecting the friction forces A. Lallemand, Ecoulements monodimensionnels des fluides compressibles, Techniques de l'ingénieur, 2014 The model respects the physics laws! SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 10

First Comparisons with Experiments SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 11

First Comparisons with Experiments SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 11

First Comparisons with Experiments The model does not reach the real equilibrium state SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 11

First Comparisons with Experiments Tracks to explain that Too reductive assumptions (e.g. ideal gas law...) The dimensions used to feed the model are not correct Some of the experimental results are not accurate enough The model does not reach the real equilibrium state A mix of them all SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 11

First Comparisons with Experiments Tracks to explain that Too reductive assumptions (e.g. ideal gas law...) The dimensions used to feed the model are not correct Some of the experimental results are not accurate enough The model does not reach the real equilibrium state A mix of them all SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 11

First Comparisons with Experiments Tracks to explain that Too reductive assumptions (e.g. ideal gas law...) The dimensions used to feed the model are not correct Some of the experimental results are not accurate enough The model does not reach the real equilibrium state A mix of them all SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 11

First Comparisons with Experiments Tracks to explain that Too reductive assumptions (e.g. ideal gas law...) The dimensions used to feed the model are not correct Some of the experimental results are not accurate enough The model does not reach the real equilibrium state A mix of them all SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 11

First Comparisons with Experiments Tracks to explain that Too reductive assumptions (e.g. ideal gas law...) The dimensions used to feed the model are not correct The model does not reach the real equilibrium state Some of the experimental results are not accurate enough Measurements of temperature A mix of them all SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 11

Simulation vs. (Corrected) Experimental SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 12

Simulation vs. (Corrected) Experimental Correction of the initial temperature in the tanks, regarding to the equilibrium SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 12

Simulation vs. (Corrected) Experimental Correction of the initial temperature in the tanks, regarding to the equilibrium SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 12

Simulation vs. (Corrected) Experimental Correction of the initial temperature in the tanks, regarding to the equilibrium SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 12

Simulation vs. (Corrected) Experimental Correction of the initial temperature in the tanks, regarding to the equilibrium The results of the model fits to the experiments in pressure! SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 12

Simulation vs. (Corrected) Experimental Correction of the initial temperature in the tanks, regarding to the equilibrium The results of the model fits to the experiments in pressure! Use of the model to detect experimental flaws SIMTEC INTRODUCTION FLOW MODELING VALIDATION CONCLUSIONS 12

Conclusions 13

Conclusions Numerical difficulties broken using a 1D approach General enough interfaces to implement it 13

Conclusions Numerical difficulties broken using a 1D approach General enough interfaces to implement it Validation of the model using theoretical and experimental results 13

Conclusions Numerical difficulties broken using a 1D approach General enough interfaces to implement it Validation of the model using theoretical and experimental results Some weaknesses on the thermal exchanges Inherent to the 0D simplification 13

Conclusions Numerical difficulties broken using a 1D approach General enough interfaces to implement it Validation of the model using theoretical and experimental results Some weaknesses on the thermal exchanges Inherent to the 0D simplification The degree of accuracy is satisfaying 13