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Dust Resuspension Modeling
Paul W. Humrickhouse and Brad J. Merrill
Fusion Safety Program
2nd IAEA RCM on Dust in Fusion Devices,21-23 June 2010
Overview
• Motivation and Objective• Aerosol deposition vs Resuspension• Particle-surface interactions• Resuspension model evolution• Model theory and description
- VZFG- RRH / Rock n’ Roll
• Numerical Implementation• Code and Model Comparison• Summary and Future Work
Introduction
• Radioactive/Toxic/Reactive dust presents a variety ofsafety issues
• Present work seeks to assess the extent of resuspensionand subsequent transport in an accident, e.g. LOVA
• MELCOR is a systems code that solves thermal hydraulicsand other things, including aerosols
- Developed at Sandia National Lab for LWR severe accidentmodeling
- Modified by INL for fusion applications and qualified forITER safety analysis
• MELCOR will deposit aerosols on surfaces, but has nomodel or mechanism to resuspend them
Deposition vs Resuspension
• This shortcoming is not limited to MELCOR• Deposition does not really treat particle surface interactions
- Body forces on particles steer them toward a surface
∂n∂ t
= u ·∇n = D∇2n−∇ ·vn
- They are simply assumed to stick
• Resuspension requires modeling interactions between theparticle, surface, and boundary layer flow
Particle-surface interaction
• Assumed that particles adhere to surfaces due to Van derWaals forces
F ∼ πγR
Resuspension as a static force balance
• The simplest picture of resuspension is that it occurs whendrag, or lift, forces exceed adhesive forces
• Particles are small: they reside in the viscous sublayer(u+ = y+), where u+ = u/u∗, y+ = ρyu∗/µ, andu∗ = (τw/ρ)1/2
• Drag on a sphere:
FD =12
ρU2p πR2CD =
πCDρ3u4∗R
4p
2µ2
• For CD = 24/Rep,FD = 3πρu2
∗R2p
• Force ratio (JKR, FA = 3πγRp):
FD
FA=
ρu2∗Rp
γ
Shortcomings of static force balance
• It’s an “all or nothing” approach:
- Zero resuspension occurs for FD/FA < 1- Complete resuspension for FD/FA > 1
• There is no time component to this...
- resuspension occurs completely and instantaneously
• Resuspension occurs when such a model predicts thereshould be none
Effects of turbulence
• The viscous sublayer is not really static, but affected byturbulent bursts
- These have a characteristic size and frequency,
`∼ ν
u∗
1t∼ u2
∗ν
• The latter was identified with a resuspension rate constant
Which forces are important?
• The above example considered only drag vs. adhesiveforces:
FD = 3πρu2∗R
2p
• The first models incorporating the turbulent burst idea usedlift forces:
FL ∼ µu3∗R
3p
• Thus, for small particles, drag is likely to dominate• It was later realized that drag was much more likely to
instigate movement by rolling due to the drag moment
- This approach has been adopted in both approches tofollow
Kinetic models
• The temporal character of resuspension was proposed tobe analagous to molecular desorption
- Resuspension rate constant given by an Arrenhius law:
p = f0exp(− Q
2〈PE〉
)• f0 is a “typical” frequency of particle/surface deformation
- Determined by experimental measurements of the lift forceenergy spectrum
f0 =
√〈 ˙f 2〉/〈f 2〉
2π≈ 0.00658
(u2∗
ν
)• Q/2〈PE〉= f (FD,FL,FA, ...) differs for each of two models
considered next
Vainshtein, Ziskind, Fichman, and Gutfinger (VZFG)
• Formulates Q/2〈PE〉 in terms of moments
- MA/MD turns out to be equivalent to Faτ/FD
• Forces are integrated to get potential and maximum energies
• Particle oscillates like a linear spring with stiffness χe:
χe =9
10 (6πγ)1/3 k2/3R2/3
VZFG (2)• Consideration of the particle equation of motion leads to
FD =χe
2R2 x3
• Integrating with respect to x gives PE ∼ x4, PE ∼ F4/3D
• Based on the maximum displacement from the JRK model,
Faτ = 9.3γ4/3R2/3
k1/3 , k =43
(1−ν2
1E1
+1−ν2
2E2
)• Drag on a stationary sphere on a plane in shear flow:
FD = 9.6µ2R2u2
∗ρ
Faτ
FD≈ ργ4/3
k1/3µ2R4/3u2∗
p = f0exp
(−(
Faτ
FD
)4/3)
Surface roughness
• In reality, particles do not adhere to smooth surfaces• They are presumed to rest on asperities, characterized by
their own radius of curvature ra
• Non-dimensionalform: r′a = ra/R
• Assumed r′a� R, sor′a should be used tocalculate adhesiveforce
• ra presumed to be lognormally distributed, with probabilitydensity ϕ(r′a):
ϕ(r′a)=
1
(2π)1/2
1r′a
1ln(σ ′a)
exp
(−(ln(r′a)− ln
(r̄′a))2
2(ln(σ ′a))2
)
VZFG Summary
Faτ
FD=
ργ4/3r2/3a
k1/3µ2R2u2∗
p = 0.0033(
u2∗
ν
)exp
(−(
Faτ
FD
)4/3)
ϕ(r′a)=
1
(2π)1/2
1r′a
1ln(σ ′a)
exp
(−(ln(r′a)− ln
(r̄′a))2
2(ln(σ ′a))2
)Fraction of partices remaining fR on a surface at time t:
fR (t) =∫
∞
0exp[−p(r′a)
t]
ϕ(r′a)
dr′a
Rock n’ Roll model (RNR)
• Based on prior RRH (Reeks, Reed, and Hall) model
- RRH originally proposed the Arrhenius law and energybalance
• Considers both drag and lift effects on rolling
• Primary differences between VZFG and RNR:
- RNR assumes a lognormal distribution of adhesive forces,rather than asperity radii used to calculate adhesive forces
- Considers both drag and lift effects on rolling- Treats contact with multiple asperities- Includes Gaussian distribution of drag forces- Spring oscillations are linear, in the direction of fluctuating
force
Rock n’ Roll (2)
Rock n’ Roll model (3)
p = f0exp
(−(fa−〈F〉)2
2〈f 2〉
)/12
[1+ erf
((fa−〈F〉)/
√2〈f 2〉
)]
• fa is the adhesive force, lognormally distributed:
ϕ(f ′a)=
1
(2π)1/2
1f ′a
1ln(σ ′a)
exp
(−(ln(f ′a)− ln
(f̄ ′a))2
2(ln(σ ′a))2
)
• 〈f 2〉 is the covariance of the fluctuating lift force f , givenexperimentally by √
〈f 2〉= 0.2〈F〉
• 〈F〉 is the mean aerodynamic force
Rock n’ Roll model (4)
• 〈F〉 contains both lift and drag contributions:
F(t) =12
FL +Ra
FD
• with the “geometric factor” R/a stated to be ~100• Mean lift and drag forces are given experimentally by
〈FL〉= 20.9ρf ν2f
(Ru∗νf
)2.31
〈FD〉= 32ρf ν2f
(Ru∗νf
)2
Numerical Implementation (1)
• Need to discretize in time and adhesive force (and particleradius)
- Force distribution evolves in time as loosely bound particlesare resuspended
∆Fn+1R,i −∆Fn
R,i
∆t=−p
(r′a)×(
θ ×∆Fn+1R,i +(1−θ)×∆Fn
R,i
)• Fortran code has been written to solve the problem
- Will be implemented as a MELCOR subroutine
• Structure is in place to do so
Numerical Implementation (2)
• Discretized MELCOR implementation will require:
- nr particle radius intervals- na adhesive force intervals- each for ns total surfaces
• nr×na×ns may present significant memory requirements• Possible solution: take all resuspending particles from one
bin
Size Distribution Approximation
x =lnr′a− lnr̄′a
lnσ ′a
VZFG implementation
0.0 2.0 4.0 6.0
Friction velocity (m/s)
0.0
0.2
0.4
0.6
0.8
Fraction remaining (FR)
Vainshtein's results
Approx. Eq. 18
Eq. 18
1.0
RNR implementation
0 1 10
Friction velocity (m/s)
0.0
0.2
0.4
0.6
0.8
Fraction remaining (FR)
Hall Data
Rock ‘n Roll R&H Rock 'n Roll Eq. 18
1.0
VZFG vs RNR
0.1 1 10
Friction velocity (m/s)
0.0
0.2
0.4
0.6
0.8
Fraction remaining
Rock'n Roll
Hall 10 data
Vainshtein
1.0
RnR - 20 micron, graphite particles
• Left: 23 µm alumina, σ ′a = 19, fred = 37• Right: 13 µm graphite, σ ′a = 19, fred = 1.55
Adhesion Distribution Measurements
• Reeks et al. take r′a = 1/37, σ ′a = 10.4 (i.e., from differentexperiments)
Influence of adhesion distribution
• Case 1: r′a = 1/37, σ ′a = 2.55• Case 2: r′a = 1/592, σ ′a = 49
Varying adhesion distributions in the RnR model
Time dependence• Prior experimental work has shown a resuspension rate∼ 1/t at long times
• Reeks et al. demonstrate this with RnR model• Our work shows similar behavior for the VZFG model
Adhesion distribution and time dependence• 1/t dependence occurs only for a sufficiently wide spread
in the lognormal distribution
“One bin at a time” approximation
• Agrees reasonably well with the “exact” solution for bothmodels
Influence of Gaussian Drag Force Distribution
p = f0exp
(−(fa−〈F〉)2
2〈f 2〉
)————————————————/
12
[1+ erf
((fa−〈F〉)/
√2〈f 2〉
)]
• Assumed by NRG code SPECTRA
Influence of particle size
• Alumina parameters (with σ ′a = 10.4, fred = 37), 10 µm and23 µm particles
Influence of Geometric Factor
• G = R/a, where a measures the distance betweenasperities
• Smaller a allows for easier rolling (i.e., more readilyresuspended by drag)
• Reeks et al. use G = 100, not abundantly clear why
Summary and Future Work
• Both VZFG and RNR resuspension models have beenimplemented numerically
• Results agree well with those published
• Outlook
- Models need to be implemented in MELCOR- Appropriateness of simplifying assumptions needs to be
verified for a broader range of flow parameters- Relative strenghts and weaknesses of competing models
need to be assessed
• Comparison to experimental data if available
• Biggest challenge: a quantitative result, given evolvingPFC characteristics