multiphase flows Application to evaporation phenomena Olivier Le - - PowerPoint PPT Presentation
multiphase flows Application to evaporation phenomena Olivier Le - - PowerPoint PPT Presentation
Dynamic relaxation processes in compressible multiphase flows Application to evaporation phenomena Olivier Le Mtayer Aix-Marseille University, Polytech Marseille UMR CNRS 7343 Some industrial applications where evaporation is crucial Fuel
Some industrial applications where evaporation is crucial
Fuel injectors at high pressure BLEVE phenomena (Security) : rapid depressurization of liquefied gas + combustion Cryogenic injection device in space launcher
Typical physical processes we are interested in
Low pressure chamber
- Liquid/vapor mixture (drops, bubbles,
pockets, ,…) Liquid flow from a high pressure chamber
- Drops evaporation and jet explosion
- « Flashing » (rapid depressurization)
generated by the initial pressure ratio Valve/diaphragm
- Cavitation created by geometric
singularities (strong rarefaction waves) Interface problems Two-velocities flow (inter-penetration) How can be solved the multiphase flow when the topology strongly varies ? A way is to consider relaxation effects
Plan
- Presentation of the relaxation effects
- Some multidimensional numerical results
- Description of the non-equilibrium multiphase flow model
Non-equilibrium multiphase compressible flow model
Multiphase compressible flow model
) u ( . t ) (
k k
k I k k
α P I P u u ρ . t ) u (
k I I k k
α . u P u P ρE . t ) E (
α . u t α
k I k
- Each phase has its own set of equations and associated variables
(velocity, pressure temperature, entropy,…) : + Equation of state :
) , P ( e
k k k
- Solved by the Discrete Equations Method (Abgrall & Saurel, JCP, 2003 ; Saurel & al.,
JFM, 2003 ; Chinnayya & al., JCP, 2004 ; Le Métayer & al., JCP, 2005 ; Saurel & al., IJNMF, 2007 ; Le Métayer & al., JCP, 2011)
- Initially proposed by (Baer & Nunziato,IJMF,1986) for two phases
Fixed control volume = sum of the sub-volumes filled with the fluids Each phase has a time-dependent sub-volume (volume fraction)
Discrete Equations Method : Godunov’s concept applied to multiphase cells
- DEM=averaging procedure by solving Riemann problems between pure fluids at each cells interface
Cell i Cell (i-1) Cell (i+1)
- Godunov’s method=averaging procedure by solving a single Riemann problem at each cells interface
Cell i Cell (i-1) Cell (i+1) Fixed control volume = volume filled with the fluid
Major contributions of DEM (1)
Discrete equations traducing the time evolution of phases and mixture variables are
- btained = Numerical scheme
When dealing with a two-phases bubbly flow, a continuous model has been obtained : All interface variables are determined !
x α P x P ρu t ) u (
1 I 1 2 1
1 2
u u λ
x α u t α
1 I 1
2 1
P P μ
x α u P x u P ρE t ) E (
1 I I 1 1
2 1 I
P P μP
1 2 I
u u λu
2 1 I
Z Z A
2 1 2 1 I
Z Z Z Z A
2 1 2 2 1 1 I
Z Z u Z u Z u
2 1 2 2 1 1 I
Z 1 Z 1 Z P Z P P
Interfacial area between phases
µ and λ express the rates at which pressure and velocity equilibrium are reached respectively
Major contributions of DEM (2)
- This non-equilibrium model is able to treat simultaneously :
- mixtures with several velocities, temperatures,…
- material interfaces (contact)
- permeable interfaces (interfaces separating a cloud of drops and a gas for example,…)
Evaporation effects
- This model is completed by heat and mass transfer source terms (evaporation,
condensation) at infinite rates (relaxations)
- They are particularly relevant when :
- the interfacial area and the flow topology are unknown,
- the Direct Numerical Simulation of interface problems is considered.
- Relaxation processes (at infinite rate) allow the obtention of solutions in limit cases
corresponding to reduced models.
Two-phase compressible flow model + relaxation terms
m
I
H ~ m
I
u ~ m
Pressure relaxation Velocity relaxation Mass transfer Heat transfer Hyperbolic
1 1
) u .( t ) (
1 2
u u λ
1 I I 1 1
α . u P u P ρE . t ) E (
2 1 I
P P P μ
1 2 I
u u . u λ
1 2 T
T T H
2 1 I
P P P μ
I
H ~ m
1 2 T
T T H ) g g ( ~ m
2 1 I
1 2
u u λ
1 2 I
u u . u λ
2 2
) u .( t ) (
1 I 2 2
α P I P u u ρ . t ) u (
1 I I 2 2
α . u P u P ρE . t ) E (
1 I 1 1
α P I P u u ρ . t ) u (
m
2 1
P P μ
I
u ~ m
I
~ m
1 I 1
α . u t
Relaxation coefficients
1 2
u u λ
1 2 T
T T H ) g g ( ~ m
2 1 I
2 1
P P μ
- µ and λ express the rate at which pressure and velocity equilibria are
reached respectively :
- HT expresses the rate at which temperature equilibrium is reached :
- ν expresses the rate at which Gibbs free energy equilibrium is reached :
Heat exchange between phases Mass transfer (evaporation/condensation process) Mechanical interactions (drags, compressibility ratio) between phases
μ , HT , ν → ∞
Instantaneous exchanges : relaxation effects
Relaxation effects at infinite rates
Hierarchy of compressible flow models : reduced models
Multi-velocity flow model Non-equilibrium flows (u1,u2,p1,p2,T1,T2,g1,g2) Single-velocity flow model Interface problems (u,p,T1,T2,g1,g2) Homogeneous Euler model Thermodynamic equilibrium flows (u,p,T,g)
Thermal relaxation (temperature) Mechanical relaxation (velocity and pressure) Chemical relaxation (Gibbs free energy)
Multi-species Euler mixture model Thermal equilibrium flows (u,p,T, g1,g2)
,
T
H
Velocity relaxation procedure : λ → ∞
t ) (
1
t ) u (
1
1 2
u u λ t α1
1 2 I
u u . u λ
t ) (
2
cst ) ( Y
1 1
cst ) ( Y
2 2
2 2 1 1 *
u Y u Y u ) u u ).( u u ( 2 1 e e
1 * 1 * 1 * 1
EOS of both phases are not used explicitly
) u u ).( u u ( 2 1 e e
2 * 2 * 2 * 2
cst
1
1 2
u u λ
-
t ) u (
2
1 2 I
u u . u λ
-
t ) E (
1
t ) E (
2
Momentum and energy conservation
Pressure relaxation procedure : μ → ∞
t ) (
1
t ) u (
1
t α1 cst ) ( Y
2 2
2 1 I
P P P μ
cst u1 cst u2
1 * 1 * 1 * 1
1 1 p e e
Use of EOS
) , p ( e
* 1 * * 1
2 1 I
P P P μ
t ) (
2
2 1
P P μ
t ) E (
1
t ) u (
2
t ) E (
2
cst ) ( Y
1 1
2 * 2 * 2 * 2
1 1 p e e
) , p ( e
* 2 * * 2
) p (
* * 1
) p (
* * 2
) p ( Y ) p ( Y 1
* * 2 2 * * 1 1
Function of the final relaxed pressure only When considering ideal gas or ‘Stiffened Gas’ EOS an analytical relation is available for the pressure Mass and energy conservation
Single-velocity flow model : Interface problems
Each phase has its own temperature and Gibbs free energy (Kapila & al., 2001; Saurel & al., 2008) Mechanical equilibrium Mixture variables : Asymptotic analysis of the full non-equilibrium model Wood sound speed :
10 100 1000 10000 0.2 0.4 0.6 0.8 1 Fraction volumique eau Vitesse du son de wood dans un melange eau/air (m/s)
2 1 2 1
) E ( ) E ( E ) ( ) ( p p p u u u
2 1 2 1
u ) p E ( . t ) E ( I p u u . t ) u ( u ) ( . t ) ( u ) ( . t ) ( u . c c ) c c ( . u t
2 2 1 1 2 2 2 2 1 2 1 1 2 1 1 2 2 2 1 1
2 2 2 2 2 1 1 1 2 wood
c c c 1
,
Pressure and temperature relaxation procedure : μ , HT → ∞
t ) (
1
t ) u (
1
t ) E (
1
t α1
t ) (
2
t ) u (
2
t ) E (
2
cst ) ( Y
1 1
cst ) ( Y
2 2
2 1 I
P P P μ
2 1
P P μ
2 1 I
P P P μ
cst u1 cst u2 cte Y Y 1
* 2 2 * 1 1
Mass and energy conservation
1 2 T
T T H
1 2 T
T T H
cte e Y e Y e
* 2 2 * 1 1
Use of EOS
) T , p (
* * * k
) T , p ( e
* * * k
) T , p ( Y ) T , p ( Y 1
* * * 2 2 * * * 1 1
When considering ideal gas or ‘Stiffened Gas’ EOS analytical relations are available for pressure and temperature
) T , p ( e Y ) T , p ( e Y e
* * * 2 2 * * * 1 1
Two-species Euler model
u ) p E ( . t E I p u u . t u u ) ( . t ) ( u ) ( . t ) (
2 2 1 1
Mixture variables :
u . u 2 / 1 e E
u ) p E ( . t E I p u u . t u ) u Y .( t Y ) u Y .( t Y
2 2 1 1
Mechanical and thermal equilibrium Asymptotic analysis of the full non-equilibrium model
T T T p p p u u u
2 1 2 1 2 1
T
H , ,
Each phase has its own Gibbs free energy
2 2 1 1
Y Y 1
2 2 1 1
e Y e Y e
Pressure, temperature and Gibbs free energy relaxation procedure : μ , HT , ν→ ∞
I
~ m
m
I
H ~ m
I
u ~ m
t ) (
1
t ) u (
1
t ) E (
1
t α1
t ) (
2
t ) u (
2
t ) E (
2
2 1 I
P P P μ
2 1
P P μ
2 1 I
P P P μ
Mass and energy conservation
1 2 T
T T H
1 2 T
T T H
Use of EOS
) T , p (
* * * k
) T , p ( e
* * * k
m
I
u ~ m
I
H ~ m
) g g ( ~ m
2 1 I
* 2 * 2 * 1 * 1
e Y e Y e
+ Gibbs free energy equality
) p ( T T
* sat * * 2 * 2 * 1 * 1
Y Y 1 ) p ( h ) p ( h p e ) p ( h Y
* * 1 * * 2 * * * 2 * 1
) p ( 1 ) p ( 1 1 ) p ( 1 Y
* * 1 * * 2 * * 2 * 1
Latent heat of vaporization
) p ( L
* V
Homogeneous Euler model
u ) p E ( . t E I p u u . t u ) u .( t
g g g T T T p p p u u u
2 1 2 1 2 1 2 1
Mechanical and thermodynamic equilibrium Closure relations :
u . u 2 / 1 e E
Equilibrium sound speed :
2 2 2 , p 2 2 1 1 , p 1 2 wood 2 eq
dp ds C Y dp ds C Y T c 1 c 1
wood eq
c c
Asymptotic analysis of the full non-equilibrium model
, H , ,
T
) p ( T T
sat
1 2 2 1
1 1 1 1 Y
2 2 1 1
e Y e Y e
For an arbitrary number of phases…
Multiphase compressible flow model
Pressure relaxation Velocity relaxation Temperature relaxation Hyperbolic
k k
) u ( . t ) (
k I k k
α P I P u u ρ . t ) u (
k I I k k
α . u P u P ρE . t ) E (
k I k
α . u t α
N , 1 l k l kl
) u u (
N , 1 l l k kl
) P P (
N , 1 l k l kl I
) u u ( . u
N , 1 l l k kl I
) P P ( P
N , 1 l k l kl , T
) T T ( H
Pressure, temperature relaxation and Gibbs free energy relaxation (liquid/vapor) : μkl → ∞, HT,kl → ∞, ν → ∞
m t ) (
1
I 1
u ~ m t ) u (
I N , 1 l l 1 l 1
~ m ) P P (
t α1
N , 1 l l 1 l 1 I
) P P ( P t ) E (
1 I N , 1 l 1 l l 1 , T
H ~ m ) T T ( H
m t ) (
2
I 2
u ~ m t ) u (
I N , 1 l l 2 l 2
~ m ) P P (
t α2
N , 1 l l 2 l 2 I
) P P ( P t ) E (
2 I N , 1 l 2 l l 2 , T
H ~ m ) T T ( H
t ) (
k
t ) u (
k
N , 1 l l k kl
) P P (
t αk
N , 1 l l k kl I
) P P ( P t ) E (
k
N , 1 l k l kl , T
) T T ( H
Phase k (inert) : Phase 1 (liquid) : Phase 2 (vapor) :
- pressure
- temperature
Relaxation : Relaxation :
- Gibbs free energy
- pressure
- temperature
) g g ( ~ m
2 1 I
- pressure
- temperature
Relaxation :
3 k
Pressure, temperature and Gibbs free energy (liquid/vapor) relaxation for an arbitrary number of phases
Mass and energy conservation Use of EOS
) T , p (
* * * k
) T , p ( e
* * * k
N , 3 k * k k * 2 * 2 * 1 * 1
e Y e Y e Y e
+ Gibbs free energy equality
) p ( T T
* sat *
N , 3 k * k k * 2 * 2 * 1 * 1
Y Y Y 1
) p ( h ) p ( h ) p ( h Y p e ) p ( h Y Y Y
* * 1 * * 2 N , 3 k * * k k * * * 2 2 1 * 1
) p ( 1 ) p ( 1 ) p ( Y 1 ) p ( Y Y Y
* * 1 * * 2 N , 3 k * * k k * * 2 2 1 * 1
1 Y Y Y
N , 3 k k * 2 * 1
) N , 3 k ( cst Y Y
k * k
Modification of the final thermodynamic state between the liquid and its vapor
One-dimensional examples
Shock tube (water, steam, air)
Bar P 1 Bar P 10
K 467 ) P ( T T
sat
4 Liq
10 . 5
Cloud of droplets in a gaz (air/steam) mixture
K 373 ) P ( T T
sat
2 .
Air
Mechanical equilibrium :
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Mass fraction Liq Vap Air 1 2 3 4 5 6 7 8 9 10 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Pressure(Bar) Liq Vap Air 50 100 150 200 250 300 350 400 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Velocity(m/s) Liq Vap Air 300 350 400 450 500 550 600 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Temperature(K) Liq Vap Air
,
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Mass fraction Liq Vap Air 1 2 3 4 5 6 7 8 9 10 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Pressure(Bar) Liq Vap Air 50 100 150 200 250 300 350 400 450 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Velocity(m/s) Liq Vap Air
No interaction between phases
300 350 400 450 500 550 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Temperature(K) Liq Vap Air
Mechanical equilibrium
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Mass fraction Liq Vap Air 1 2 3 4 5 6 7 8 9 10 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Pressure(Bar) Liq Vap Air 50 100 150 200 250 300 350 400 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Velocity(m/s) Liq Vap Air 300 350 400 450 500 550 600 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Temperature(K) Liq Vap Air
,
Mechanical/thermal equilibrium
T
H , ,
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Mass fraction Liq Vap Air 1 2 3 4 5 6 7 8 9 10 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Pressure(Bar) Liq Vap Air 50 100 150 200 250 300 350 400 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Velocity(m/s) Liq Vap Air 360 380 400 420 440 460 480 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Temperature(K) Liq Vap Air
Mechanical/thermodynamical equilibrium , H , ,
T
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Mass fraction Liq Vap Air 1 2 3 4 5 6 7 8 9 10 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Pressure(Bar) Liq Vap Air 50 100 150 200 250 300 350 400 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Velocity(m/s) Liq Vap Air 380 390 400 410 420 430 440 450 460 470 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Temperature(K) Liq Vap Air
Another possibility : heat exchanges between inert phases and liquid/vapor are absent
m t ) (
1
I 1
u ~ m t ) u (
I N , 1 l l 1 l 1
~ m ) P P (
t α1
N , 1 l l 1 l 1 I
) P P ( P t ) E (
1 I N , 1 l 1 l l 1 , T
H ~ m ) T T ( H
m t ) (
2
I 2
u ~ m t ) u (
I N , 1 l l 2 l 2
~ m ) P P (
t α2
N , 1 l l 2 l 2 I
) P P ( P t ) E (
2 I N , 1 l 2 l l 2 , T
H ~ m ) T T ( H
t ) (
k
t ) u (
k
N , 1 l l k kl
) P P (
t αk
N , 1 l l k kl I
) P P ( P t ) E (
k
N , 1 l k l kl , T
) T T ( H
Phase k (inert) : Phase 1 (liquid) : Phase 2 (vapor) :
- pressure
- temperature
Relaxation : Relaxation :
- Gibbs free energy
- pressure
- temperature
) g g ( ~ m
2 1 I
- pressure
- temperature
Relaxation :
3 k
Mechanical/thermodynamical equilibrium , H , ,
T
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Mass fraction Liq Vap Air 1 2 3 4 5 6 7 8 9 10 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Pressure(Bar) Liq Vap Air 50 100 150 200 250 300 350 400 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Velocity(m/s) Liq Vap Air 380 390 400 410 420 430 440 450 460 470 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Temperature(K) Liq Vap Air
Thermodynamical equilibrium between liquid and vapor only
0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Mass fraction Liq Vap Air 1 2 3 4 5 6 7 8 9 10 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Pressure(Bar) Liq Vap Air 50 100 150 200 250 300 350 400 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Velocity(m/s) Liq Vap Air 300 350 400 450 500 550 600 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1 X(m) Temperature(K) Liq Vap Air
Multi-dimensional examples
Cryogenic liquid and inert gas injections
Inert gas injection Tank
Bar 1 P
Tank filled with cryogenic liquid ~50000 tetrahedrons Inert gas
Bar 1 P
bar 20 p
Pressure and temperature equilibrium flow
Pressure, temperature and Gibbs free energy equilibrium flow
Vapor volume fraction evolution
Filling of cavity under gravity effect
Walls Connection to atmosphere Hot steam
Bar 1 P
Air
Bar 1 P
Cold water Gravity
Liquid volume fraction evolution : pressure relaxation
Pressure and temperature relaxation
Pressure, temperature and Gibbs free energy relaxation
Perspectives
- Exact steady solutions through converging-diverging nozzles should be
investigated under mechanical, thermal and Gibbs free energy equilibria for an arbitrary number of phases Reference solutions
- The knowledge of the interfacial area at each point of the flow must be strongly