nasa/cp—2004-213205/vol1 188 · nasa/cp—2004-213205/vol1 189. critical path roadmap zimpaired...
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NASA/CP—2004-213205/VOL1 187
https://ntrs.nasa.gov/search.jsp?R=20040142359 2018-06-09T09:24:46+00:00Z
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NASA/CP—2004-213205/VOL1 188
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Donald P. Gaver Anastacia M. Bilek
Sarina KayAnne-Marie Jacob
Kay C Dee
Department of Biomedical EngineeringTulane UniversityNew Orleans, LA
Investigations of Pulmonary Epithelial Cell Investigations of Pulmonary Epithelial Cell Damage Due to AirDamage Due to Air--Liquid Interfacial Stresses in Liquid Interfacial Stresses in a Microgravity Environmenta Microgravity Environment
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Critical Path RoadMapCritical Path RoadMap
Impaired Response due to Modified Orthostatic Mechanical Stress
Diminished Cardiac Function
Impaired Response to Exercise Stress
Cardiovascular Alterations Pulmonary Alterations
Airway Closure Becomes more Homogeneous
Potentially Impaired Pulmonary Function
Impaired Response to Exercise Stress
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Gravity Effects on Ventilation Gravity Effects on Ventilation DistributionDistribution
• (A) At FRC the lower region is less expanded, but more compliant
so it receives larger portion of ventilation
• (B) At RV the lower lung regions experience airway closure
Milic-Emili, J. Respiratory Physiology I, vol. 2, 1974
g
Airway Closure
ρgh
ρgh
A B
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Airway Closure in MicrogravityAirway Closure in MicrogravityAirways
Bifurcation
Alveolar Sac
Alveoli
AirwayClosure
MICROGRAVITY CAUSES:
•Regional Modification of Ventilation•Changes of Blood Perfusion•Variation in Lung Capacity
•‘Patchy’ regions of airway collapse
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Related Terrestrial SyndromesRelated Terrestrial Syndromes
•Infant Respiratory Distress Syndrome
•Acute Respiratory Distress Syndrome
•Ventilator-Induced Lung Injury
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Pulmonary Multiscale InteractionsPulmonary Multiscale Interactions
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MotivationMotivation
Our goal is to determine the cause of reopening-induced damage, and the surfactant properties and airway reopening strategies that will allow pulmonary airways to be opened with minimal damage to the lung.
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Stresses in Airway ReopeningStresses in Airway Reopening
Direction of Bubble Progression
Air Bubble Collapsed Airway
Gaver, Jensen, Halpern and Grotberg, J. Fluid Mech., 1996
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Luminal TransmembraneProteins
Cell-cellproteins Nuclear
Membrane
Focal AdhesionSites
Mechanisms of Cell Mechanisms of Cell Mechanotransduction and DamageMechanotransduction and Damage
Matrix
Nucleus
3-D Surface Topography Influences Stress Distribution
Force Transmission
Adapted from Davies,Physiol. Rev., 1995
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Cell Culture ExperimentsCell Culture Experiments
Lung epithelial cells were:• Cultured in an idealized model of small airways,• Exposed to a moving finger of air under reopening
conditions, • Examined for cellular trauma.
Occlusion Fluid(PBS or Infasurf)Air Bubble
Glass Plate
Pulmonary Epithelial CellsGlass Plate
U(~ 0.25 - 2.5 cm/s)
(L2 or A549)
0.16 cm
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Methods Methods –– Variable VelocityVariable VelocityLung epithelial cells (CRL-149, ATCC) cultured to
confluence on glass microscope slides.
The channel dimensions were 2.5 x 7.0 x 0.17 cm.
Two velocities (0.27 and 2.7 cm/s) were assessed.
Two occlusion fluids were assessed:– phosphate buffered saline (PBS) and– 1 mg/mL Infasurf (ONY, Inc., Buffalo, NY) in
PBS.
Cellular trauma was quantified using fluorescent staining (Live/Dead Kit, Molecular Probes).
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Stress Field Stress Field –– Rigid ChannelRigid Channel
Direction of Bubble Progression
Air Bubble Fluid Occlusion
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Injury by a Single Bubble ProgressionInjury by a Single Bubble Progression(L2 cells, Live/Dead Kit)(L2 cells, Live/Dead Kit)
Control 0.27 cm/s 2.7 cm/s
PBS
Infa
surf
Bubble Velocity
Occ
lusi
on F
luid
Occlusion Fluid(PBS or Infasurf)Air Bubble
Glass Plate
Pulmonary Epithelial CellsGlass Plate
U(~ 0.25 - 2.5 cm/s)
(L2 or A549)
0.16 cm
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Injury by a Single Bubble ProgressionInjury by a Single Bubble Progression(L2 cells, Live/Dead Kit)(L2 cells, Live/Dead Kit)
n = 5* p < 0.01
PBS Infasurf (1 mg/mL in PBS)
0
100
200
300
400
500
Control
Inju
red
Cel
ls [c
ells
/mm
2 ]
0.27 2.7
Bubble Velocity [cm/s]
**
* *
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Mechanisms of Cell Membrane Mechanisms of Cell Membrane WoundingWounding
Shear Stress
Shear Stress Gradient
Pressure
Pressure Gradient
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The Flow ModelThe Flow Model
Surface Tension, γeq Q = Constant
Newtonian Fluid, µ
2H
Steady Flow of a Semi-Infinite Bubble in a Channel
Governing Parameter:eq
UCaγµ=
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11.6443.817.5FastInfasurf
2.7893.47.9SlowInfasurf
6.017010.134.3FastSaline
1.43409.215.5SlowSaline
f (µm)
∆P(dyn/cm2)
∆τs(dyn/cm2)
τs(dyn/cm2)
SpeedFluid
PredictionsPredictions
Control 0.27 2.7Bubble Velocity [cm/s]
Cel
l Dam
age
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Predictions of Cell Normal StressesPredictions of Cell Normal Stresses
(x* – xmen*)/H
O c c lu s io nF lu id
A ir B u b b le
G la s s P la te
E p ith e lia l C e llsG la s s P la te
y =
y* /H
-1
0
1
C a = 0 .0 5C a = 0 .0 0 5C a = 0 .0 0 0 5
-1 0
Dim
ensi
onle
ss P
ress
ure,
(P* -P
* bub)/(
γγ γγ/H
)
-1
0
y =
y* /H
-1
0
1
C a = 0 .0 5C a = 0 .0 0 5C a = 0 .0 0 0 5
-1 0
Dim
ensi
onle
ss P
ress
ure,
(P* -P
* bub)/(
γγ γγ /H
)
-1
0
y =
y* /H
-1
0
1
C a = 0 .0 5C a = 0 .0 0 5C a = 0 .0 0 0 5
-1 0
Dim
ensi
onle
ss P
ress
ure,
(P* -P
* bub)/(
γγ γγ /H
)
-1
0
1. Film Thickness decreases with decreasing velocity
2. The pressure gradient on the cell surface increases with decreasing velocity
Decreasing Velocity
Decreasing Velocity
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Investigations of the Applied Stress Investigations of the Applied Stress Duration Duration
The variable velocity experiments induce stresses on cells that are not of constant duration.
Hypothesis:The slow velocity experiments may induce greater damage because of the increased exposure time.
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Methods Methods –– Constant VelocityConstant Velocity
Human Pulmonary Epithelial Cells (A549, ATCC) cultured to confluence on glass microscope slides.
The channel dimensions were 2.5 x 7.0 x 0.17 cm.
A single velocity (0.34 cm/s) was applied.
Two viscosities were used µ = µ = µ = µ = 8x10-3 g/(cm s) (PBS)µ = µ = µ = µ = 8x10-2 g/(cm s) (PBS + 14% Dextran)
Cellular trauma was quantified using fluorescent staining (Live/Dead Kit, Molecular Probes).
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TravelingTraveling--Wave BehaviorWave Behavior
Film Thickness Increasesas
Ca Increases
Lubrication Film
b Ca > 0Ca = 0
Ca = 0
P
xLwave
U
Pressure Field Near Contact Line
c
Ca > 0Pressure Gradient
Decreasesas Ca Increases
∆∆∆∆P = γ/Η= γ/Η= γ/Η= γ/Η
Contact Line
a U
γµUCa =
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TravelingTraveling--Wave BehaviorWave Behavior
Ca = 0
P
x
U
Ca > 0
γµUCa =
|dP/dx| Decreases as Ca Increases
∆∆∆∆P ~ γγγγ/H
LwaveIncreases as Ca Increases
29.071.0
29.0
exp γµ
UH
ULt wave ∝=∆
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0
10
20
30
40
Low ViscosityControl
HighViscosityControl
Low ViscosityExp
HighViscosity Exp
Inju
red
Cel
ls
(103 c
ells
/cm
2 )PBS
PBS/Dextran
Pressure Gradient, not Exposure Duration, Pressure Gradient, not Exposure Duration, Determines DamageDetermines Damage
Ca largeCa small
U = 0.34 cm/s, µµµµDextran = 10µµµµPBS
↑dxdP
↓dxdP ↑sτ
↓expt↓sτ
↑exptKay et al. , JAP, 2004
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Investigations of TopographyInvestigations of Topography
Our system is modeled to isolate the influence of epithelial topography on the following components of the stress cycle during airway reopening:– shear stress and shear stress gradient– normal stress and normal stress gradient
bubbleprogression
bubbleprogression
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Computational ModelComputational Model
x0
y -0
epithelial cell layer
2a
Q*
λλλλ
2H
constant surface tension, γγγγ
semi-infinite bubble
fluid occlusion
constant µµµµ, ρρρρ
Geometric Parameters: εεεε=a/H ΛΛΛΛ= λλλλ/H
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Computational ModelComputational Model
Stokes Flow
LubricationTheory
Boundary Element Method
Q* KinematicBoundary Condition
Interfacial Stress
∂∂Yt
n u n∗
∗
∗⋅ ⋅= ∇ = ∇∗ ∗P uµ 2
τ γ κ∗ ∗= n
Governing Parameter: Ca Q /2H/
Q =*
γ µ
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y
-1
0
1
x-3 -2 -1 0 1 2
ττ ττ n
-1
0εεεε = a/H = 0.00εεεε = a/H = 0.05εεεε = a/H = 0.10
increasingcell height
epithelial cell
bubble
Normal Stress Distribution Normal Stress Distribution λλ/H = 2, Ca = 0.01/H = 2, Ca = 0.01
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Normal Stress DistributionNormal Stress Distributiona/H = 0.1, a/H = 0.1, λλ/H = 2, Ca = 0.01/H = 2, Ca = 0.01
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y
-1
0
1
x-3 -2 -1 0 1 2
ττ ττ t
0.0
0.2εεεε = a/H = 0.00εεεε = a/H = 0.05εεεε = a/H = 0.10
increasingcell height
epithelial cell
bubble
Tangential Stress DistributionTangential Stress Distributionλλ/H = 2, Ca = 0.01/H = 2, Ca = 0.01
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Tangential Stress DistributionTangential Stress Distributiona/H = 0.1, a/H = 0.1, λλ/H = 2, Ca = 0.01/H = 2, Ca = 0.01
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εεεε/ΛΛΛΛ = a/λλλλ = 0.05εεεε/ΛΛΛΛ = a/λλλλ = 0.00
Tangential Stress
CaQ = [Q*/(2H)]/(γγγγ/µµµµ)
0.001 0.01 0.1
(dττττt/dx)max
1e-4
1e-1
1e+0
Tangential Stress Gradient
CaQ = [Q*/(2H)]/(γγγγ/µµµµ)
0.001 0.01 0.1
(ττττt)max
1e-4
1e-1
1e+0 increasing εεεε/ΛΛΛΛ
increasing εεεε/ΛΛΛΛ
CaCaQQ vs.vs. Tangential Stress and Tangential Stress and Stress GradientStress Gradient εε//ΛΛ = 0.05= 0.05
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CaCaQQ vs.vs. Normal Stress GradientNormal Stress Gradientεε//ΛΛ = 0.05= 0.05
increasing εεεε/ΛΛΛΛ
CaQ = [Q*/(2H)]/(γγγγ/µµµµ)0.001 0.01 0.1
(dττττn/dx)max
2e+0
3e+04e+0
1e-4 εεεε/ΛΛΛΛ = a/λλλλ = 0.05εεεε/ΛΛΛΛ = a/λλλλ = 0.00
Normal Stress Gradient
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Surfactant EffectsSurfactant Effects
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Equilibrium Equation of State (Infasurf)Equilibrium Equation of State (Infasurf)
Ghadiali, S. N. and D. P. Gaver, III (2000). J. Appl. Physiol. 88: 493-506.
0.1 1 100.010.0010.00010
10
20
30
40
50
60
70
80
Infasurf Concentration [mg/mL]
Sur
face
Ten
sion
[dyn
/cm
]
γγγγeq
CCBC
NA
SA/C
P—2004-213205/V
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0
10,000
20,000
30,000
40,000
50,000
0 0.01 0.1 1Infasurf Concentration [mg/mL]
Popu
latio
n In
jury
[cel
ls/c
m 2 ]
0.1 1 100.010.0010.00010
10
20
30
40
50
60
70
80
Infasurf Concentration [mg/mL]
Sur
face
Ten
sion
[dyn
/cm
]
CBC
γeq
Influence of Surfactant ConcentrationInfluence of Surfactant Concentration(A549 cells, Live/Dead Kit, 0.25 cm/s)(A549 cells, Live/Dead Kit, 0.25 cm/s)
CBC
NA
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Correlation of Stress and InjuryCorrelation of Stress and Injury
InfasurfSpeed Injury ττττs ∆τ∆τ∆τ∆τs ∆∆∆∆P(cells/cm2) (dyn/cm2) (dyn/cm2) (dyn/cm2)
0 0.25 ++ 13.1 4.8 163
0.01 0.25 ++ 12.8 4.6 154
0.1 0.25 ++ 7.1 1.9 48
1 0.25 - 6.7 1.8 44
(cm/s)(mg/mL)
?
NA
SA/C
P—2004-213205/V
OL
1224
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Influence of NonInfluence of Non--Equilibrium Behavior Equilibrium Behavior of Infasurfof Infasurf
M
Non-equilibrium behavior: produces dynamic surface tensions that are greater than the equilibrium surface tension,creates non-equilibrium surface tension that causes film-thinning.
NA
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P—2004-213205/V
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Dynamic Surface Tension of InfasurfDynamic Surface Tension of Infasurf
Ghadiali, S. N. and D. P. Gaver, III (2000). J. Appl. Physiol. 88: 493-506.
0.1 1 100.010.0010.00010
10
20
30
40
50
60
70
80
Infasurf Concentration [mg/mL]
Sur
face
Ten
sion
[dyn
/cm
]
γγγγeq
CCBC
γγγγdyn
NA
SA/C
P—2004-213205/V
OL
1226
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•Combined experiments and computational investigations allows us to estimate the mechanical stresses that damage epithelial cells during reopening
•The damaging effects from reopening are likely to be due to a large pressure gradient from the traveling air-liquid interface
•Topological effects can increase the magnitude of deleterious stresses.
Non-equilibrium surface-tension effects may increase damage unless concentrations are large.
ConclusionsConclusions
NASA: NAG3-2734 NIH: P20 EB001432NSF: BES-9978605
NA
SA/C
P—2004-213205/V
OL
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