Title: Fluid Dynamics Issues in Synthesis of Nanotubes
1Fluid Dynamics Issues in Synthesis of Nanotubes
- By
- Dr. Alex Povitsky
- Department of Mechanical Engineering
- University of Akron
- E-mail povitsky_at_uakron.edu
2 3Carbon nanotube-polymer of pure carbon
- Stiffness-to-weight ratio forty times higher than
that of aluminum - Strength-to-weight ratio five hundred times
higher than that of aluminum - Thermal conductivity as high as diamond
- Electrical conductivity six orders-of-magnitude
higher than copper
4Nanotubes Properties Uses
- Conductive plastics
- Energy storage
- Molecular electronics
- Thermal materials
- Fibers and fabrics
- Catalyst supports
5Scope of the presentation
- Considered processes of synthesis of nanotubes
are decomposition of high-pressure carbon oxide
(HiPco), laser ablation (LA), and chemical vapor
deposition (CVD). - We discuss the required modeling tools including
combined Eulerian and Lagrangian approach and
Burnett equations for higher Kn number flow. - Based on modeling, we find a thermal regime of
catalyst particles that is critical for formation
of carbon nanotubes.
6Mathematical problems
- Classification of catalyst particles
trajectories. Trajectory-based optimal design of
the apparatus for synthesis of nano-tubes - Multi-scale modeling and interaction of molecular
dynamics and continuous aerodynamics. Examples
include solid-to-gas ablation (1 microsec) and
plume dynamics (1 millisec) Rigorous model is
needed to switch between MD, DSMC, and CGD - Use of micro-fluidic boundary conditions and
Burnett equations to obtain heat and mass
transfer coefficients between the feedstock gas
and a single nanotube for Kngt0.1. Example
synthesis of nano-tubes by chemical vapor
deposition.
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9HiPco reactor and showerhead
10Various mixing scenario
90O
30O
11Temperature of catalyst particles versus time
30O
30O
60O
60O
Hot-to-cold Mass ratio31
Hot-to-cold Mass ratio61
90O
90O
12Improved Showerhead of the HiPco Reactor
60O
13Temperature of catalyst particles along their
trajectories
- Basic configuration one cold and three hot jets
14Typical trajectories of catalyst particles for
high-incidence jet mixing
1-trajectory bends inwards 2-trajectory bends
outwards 3-particle rotates upstream of the jet
intersection point
Can we design a mixing device to achieve as much
trajectories (2) as possible?
15Random Walk model for turbulent flow
One central jet, 60 degrees
New design, 60 degrees
New design, 90 degrees
16Journal publications about CFD modeling of HiPco
- C. Scott, A. Povitsky, C. Dateo, T. Gokcen, P.
Willis and R.E. Smalley, Iron Catalyst Chemistry
in Modeling a High Pressure Carbon Monoxide
Nanotube Reactor, Journal of Nanoscience and
Nanotechnology, Vol. 3, No. 2, 2003, pp. 63-73. - A. Povitsky and M. Salas, Trajectory-based
Approach to Jet Mixing and Optimization of the
Reactor for Production of Carbon Nanotubes,
AIAA Journal , Vol. 41, No. 11, November 2003,
pp. 2130-2143 preliminary version ICASE Report
2001-04 - A. Povitsky, Improving Jet Reactor Configuration
for Production of Carbon Nanotubes, Computers and
Fluids, Vol. 31, No. 8, April 2002, preliminary
version ICASE Report 2000-18
17Laser-Ablation SWNT Process at NASA Johnson Space
Center
- Dual concentric quartz tubes
- Pulse laser at 532 nm wavelength and 5mm beam
diameter - Target graphite and catalyst (Ni and Co)
- Non-reacting surrounding argon flow at T1473 K
18Plume formation in laser ablation
19Ablation
20Evolution of plume and formation of nanotubes
212-D CONSERVATION LAWS Euler Equations
22Numerical discretization
- The second-order upwind scheme(MUSCL)
- Second-order explicit RK scheme integrates in
time - Minmod TVD limiter is used
- Relaxing TVD scheme is employed
- Kurganov Tadmor, J Comp. Physics, 160 241-282,
2000 - S. Jin and Z. Xin, The Relaxation Schemes for
Systems of Conservation Laws in Arbitrary Space
Dimensions, Comm. Pure Appl. Math., 1995, Vol.
48, pp. 235-276
23Validation of the code
2-D shock tube problem
24Sedov-Taylor analytical solutionL. I. Sedov,
Similarity and Dimensional Methods in Mechanics,
Academics Press, New York, 1959
25Effect of Injection Velocity on Plume Motion
26Propagation of plumeunder standard atmospheric
pressure
27Low chamber pressure (p0.01atm)
28Temperature of catalyst particles emerging with
the doubled plume
1
2
29Influence of injection velocity on multi-pulse
plume
3010th plume
31Geometry of the laser furnace
32Target is located in the middle section of the
bulb-shape furnace
30 µs
60 µs
pressure
90 µs
30 µs
33Effects of viscosity and turbulence
- For a single plume, effective viscous
length-scale can be defined as
For t200µsec, l100µ (typical figures for laser
ablation in production of carbon nanotubes). This
scale is two orders of magnitude smaller than
cross-section of the plume and two orders of
magnitude larger than the particle size.
For multiple plume injection, viscous effects may
be more important since the flow is more close to
continuous jet For turbulent surrounding flow,
the effective viscosity is much higher and
viscous effects are more prominent Viscous/turbule
nt effects are important for motion of catalyst
particles
34Multi-domain approach
- The multi-domain approach will be developed for
concurrent rendering of different areas of
computational domain by different models (MD,
DSMC, and CGD) and/or different time steps for
the same model. - For multiple plume ejection, the near-target area
will be rendered by MD or DSMC whereas the CGD
algorithm is employed to simulate plume dynamics
of previously ejected plumes apart of the target.
- The jet mixing occurs by formation of
Raleigh-Taylor instabilities at the plume-gas
interface due to interaction with reflected shock
waves, and the local fine grid should be used - For the first 180 time steps after ablation
CFL0.0001 and the time step is
35Adopting grid and shock wave interaction with
Vortical Density Inhomogeneity (VDI)
Povitsky Ofengeim, 1999
36Laser ablation conclusions
- Non-monotonic temperature of catalyst particles
is caused by (i) interaction of particles with
reflected shock waves and (ii) circular motion of
the particles caused by formation of vortical
zones, stagnation points, and slip-lines. While
both reasons are important for the standard
atmospheric pressure of furnace gas, the latter
reason plays the key role for near-vacuum ambient
pressure. - The plume propagation is much slower than that
of the leading shock wave especially for low
injection rate and/or low ambient pressure. For
the given pressure in a laser furnace, the
position of the front of the plume primarily
depends on the plume injection velocity. A
refined laser melting and vaporization model is
needed to determine the injection velocity.
37- The location of the carbon target in the middle
section of the bulb (semi-bulb furnace geometry)
produces relatively smooth temperature profile of
catalyst particles required for synthesis of
carbon nanotubes. - Modeling of multiple plume is important for
technological applications where laser hits
target many times. Behavior of catalyst particles
for multiple injected plumes shows substantial
difference in comparison to a single plume
model. - On one hand, the temperature of catalyst
particles for multi-plume injection has been
increased substantially in comparison to the
single and double pulse cases. On the other hand,
there is a broad spread of the temperature for
catalyst particles emerging from different zones
of the target.
38Related Journal Papers
- D. Lobao and A. Povitsky, Single and Multiple
Plume Dynamics in Laser Ablation for Nanotube
Synthesis, accepted for publication in AIAA
Journal, preliminary version AIAA Paper
2003-3923. - D. Lobao and A. Povitsky, Furnace Geometry
Effects on Plume Dynamics in Laser Ablation, to
appear in Mathematics Computers in Simulation
(Special Issue on Wave Propagation), short
version in Proceedings of ICCSA-2003, Lecture
Notes in Computer Science 2668, pp. 871-880, 2003.
39Chemical Vapor Deposition method (CVD) for
synthesis of nanotubes
Base growth model
40CFD modeling of CVD process
- Knudsen number is 0.1-1.0 (based on the nanotubes
diameter) - Slip/No-slip boundary conditions
- Navier-Stokes/Burnett equations
Purpose to compute mass transfer between the
feedstock gas and catalyst particles
41Slip boundary conditionsStocks Equations (low
Re, Knlt0.1)
Single Isolated Cylinder
For slip boundary conditions D ?0!
42Computational framework for CVD process
43Micro-fluids aspects of feedstock gas flow at
the nanotubes base
Slip boundary conditions
No-slip boundary conditions
44Conclusions and Future Research
- CFD modeling of nanotubes synthesis requires
multi-scale approach to combine - continuous mechanics of multi-species flow of
feedstock gas or plume - micro-fluidic flow model that is needed to find
heat and mass transfer coefficients about
isolated nanotubes - molecular dynamics of formation of plume in laser
ablation. The obtained distribution of plume
injection velocity will be used by continuous
model
45Collaboration with Prof. Zhigiley(U. of Virginia)
Proposal Title Combined mathematical model of
plume dynamics in laser ablation of nanosecond
to millisecond temporal scale During the first
nanoseconds, fast laser energy deposition leads
to overheating of the surface and ejection of
atoms, molecules, ions, and clusters. This
initial fast part of the ablation process is
followed by a slower expansion of the ablation
plume. The large disparity of the processes
occuring at different stages of laser ablation
does not allow one to describe this phenomenon
within a single computational approach
46Collaboration with Profs. Tsukerman (Akron) and
Friedman (Drexel)
Proposal Magnetically Driven Self-Assembly of
Nano- and Micro- particles in Fluids
During the last decade, substrates patterned with
many different chemical species or other
materials have found applications in
combinatorial chemistry, chemical sensors and
genetic testing (DNA chips). Fluid agitation by
impulsive flows can induce much more ordered
patterns of particles on the substrate. Flow
motion may be used to disperse undesirable chains
or clouds of particles.
47References