ABALBERTO
BRAMBILA

MASTER'S THESIS · UNIVERSIDAD DE COLIMA · 2018

A CVD reactor,
understood through thermal physics.

From Reynolds, Grashof and Richardson numbers to a precursor-placement decision—and the microstructures grown inside the real reactor.

MY WORKFormulated and built the CFD study, designed the parameter sweeps, checked the underlying physics and connected the simulated flow structures with experimental synthesis outcomes.

Two families of convection cells along the complete tubular reactor
Long recirculation cells near the tube ends coexist with Bénard-type rolls in the heated center. These structures explain how material can grow differently only centimeters apart. Enlarge figure ↗

MASTER’S RESEARCH / FROM THERMAL MODEL TO SYNTHESIS

Explain where the material grows—and why.

The problem

The temperature and flow inside the synthesis tube could not be measured throughout the operating process. Precursor placement needed a physical basis.

My contribution

I built the CFD study around Reynolds, Grashof, Richardson and Nusselt numbers, isolated model effects and compared precursor positions.

The engineering link

The predicted circulation and thermal behavior were connected to experimental growth observations. The figures below follow that reasoning from model to synthesis.

This is the original academic research context, with collaborative synthesis and characterization. It is not a generic version of an industrial project in the professional log.

01 / THE PHYSICAL PROCESS

A thermal field that could not be measured during synthesis.

The engineering problem was not simply to obtain a temperature contour. It was to understand the transport mechanisms governing where ceramic fibers grow, without disturbing the reacting atmosphere.

Experimental CVD furnace, nitrogen supply, precursor and axial temperature profile
The experimental apparatus and measured thermal profile, reproduced from the thesis presentation; original process by Villavelázquez and collaborators. The diagram establishes the physical context, not a new CFD result. Enlarge figure ↗

Translate the experiment into a numerical question

A 1.2 m alumina tube has a 25 mm inner diameter and a central 450 mm section heated to 1300 °C. Nitrogen passes a porous Na₂SiF₆ precursor and a SiC preform; precursor decomposition supplies gaseous species for fiber growth.

The precursor position had been chosen empirically. Internal probes during synthesis would disturb the flow or compromise the atmosphere, so the temperature and circulation around the porous bodies had to be reconstructed numerically.

Two questions shaped the study: does injected nitrogen actually control the internal convection, and where should the precursor sit within that thermal-flow field?

The CFD contribution was the flow/heat-transfer model and its recommendation. The reactor, synthesis chemistry and material characterization belonged to a collaborative experimental program.

02 / THE CENTRAL ENGINEERING IDEA

Use dimensionless numbers to ask a more general question.

Re, Gr and Ri turn the operating conditions into competing physical mechanisms. Nusselt number then expresses the heat-transfer response, making the analysis useful beyond this one furnace.

Imposed flow

Re = UH / ν

Inertia relative to viscosity. The source reports Re ≈ 0.5 at the nominal process condition.

Buoyancy

Gr = gβΔTH³ / ν²

Thermal buoyancy relative to viscous forces. The source reports Gr ≈ 3.6 × 10⁶.

Competition

Ri = Gr / Re²

The reported process Ri ≈ 1.2 × 10⁷ places it deep in the buoyancy-dominated regime.

Thermal response

Nu = hH / k

Convective heat transfer relative to conduction across the characteristic length H.

A controlled numerical experiment

Hold Gr fixed and vary inlet flow to change Re: the Richardson sweep isolates the competition between natural and forced convection across Ri = 10³–10⁸.

This is the transferable method. Select a physical ratio, vary one mechanism systematically, and read the response through both integral quantities and the structures causing them.

At the actual process condition, small inlet-flow changes have little influence on temperature. A much wider sweep is needed before forced flow becomes competitive.

Preform and precursor temperature versus Richardson number
Six logarithmically spaced Richardson conditions. Black: preform temperature, left axis; blue: precursor temperature, right axis. Both axes are in °C. Enlarge figure ↗
Ri = 10³–10⁴

Forced flow competes

Bénard-type cells are absent in the reported low-Ri cases.

Ri ≈ 10⁵

Structures begin to recover

The central convection cells are only beginning to form.

Ri ≥ 10⁶

Buoyancy organizes the flow

The cells are developed; the nominal process lies within this regime.

Connect Nu to the local flow mechanism

The thesis analyzed Nusselt–Richardson behavior by axial region. Near the operating condition, the two end regions showed correlations of r = −0.81 and −0.72, while the porous-influenced center was weakly correlated (r = −0.1).

Know where a correlation stops being useful

Ri alone is a poor descriptor where porous bodies reshape the circulation. The engineering value is both the correlation and the recognition that a different local mechanism controls heat transfer in the central region.

Transferable reasoning: the same forced-versus-natural-convection question appears in heated enclosures, cooling passages, process equipment and HVAC flows. The dimensionless framework transfers; this reactor's fitted coefficients do not become universal design correlations.

03 / MODEL DEVELOPMENT AND VALIDATION

Add complexity only after its effect can be isolated.

Four incremental configurations separate the roles of buoyancy, imposed flow and the porous solids. Independent checks establish the two underlying physics before they are combined.

Four incremental reactor configurations and physical dimensions
Cases 1–4: open tube; add nitrogen flow; add the porous preform; add the precursor. The heated and adiabatic sections are retained in each configuration. Enlarge figure ↗

Build a model that answers the question

Steady laminar OpenFOAM simulations used ideal-gas density for buoyancy and homogeneous porous zones for the preform and precursor. A pore-scale Reynolds argument justified retaining the viscous Darcy resistance and neglecting the inertial Forchheimer term.

Hexahedral meshes were built in ANSYS Meshing. The open-tube and synthesis families used approximately 0.34 and 1.37 million nodes, with a centerline-temperature mesh-independence check before the parameter studies.

This was conduction/convection modeling. Radiation and reaction chemistry were outside the solved physics.

Temperature fields in the four progressively more complex reactor cases
A–D correspond to the four configurations above. Temperature in °C. The global thermal field changes little as flow and porous bodies are introduced. Enlarge figure ↗
Velocity magnitude in the four reactor configurations
Velocity magnitude in m/s. The porous bodies change local circulation even while the large-scale temperature field remains similar. All simulations used laminar models. Enlarge figure ↗

Read both fields together: a nearly unchanged temperature contour does not imply unchanged transport. The velocity field reveals the local disturbances that matter to precursor positioning and downstream growth.

OpenFOAM and Fluent porous-flow velocity fields and profiles
Cross-code verification of the porous-flow model. A separate tracer comparison at four locations gave errors within 5% for both codes. Enlarge figure ↗
Open-tube thermal prediction compared with five measurement campaigns
Thermocouple profiles versus axial position. The thesis reports approximately 5% average error against its reference campaign; the figure retains all original campaign labels. Enlarge figure ↗

These are independent checks of porous flow and buoyant heat transfer. The combined synthesis configuration was assessed through its physical implications and experimental outcomes, rather than instrumented internally during reaction.

04 / FROM ANALYSIS TO A PROCESS DECISION

The best position is not simply the hottest precursor.

Moving the precursor changes its temperature, the preform temperature and the circulation between them. The design choice has to serve the synthesis process as a whole.

Compare four positions, then interpret the trade-off

The sweep tested 24.8, 26.5, 28.7 and 30.9 cm from the inlet. Precursor temperature increased almost linearly with position, but preform temperature did not: the highest average and most uniform preform temperature occurred at 26.5 cm.

The thesis gives the precursor relation T = 49.47x − 770.84, with T in °C, x in cm and R² = 0.994. This is a fit within the tested positions, not an extrapolation rule.

At 26.5 cm, simulated precursor temperature was about 537 °C—within the independently reported 520–593 °C decomposition window. The preform was about 10 °C warmer than at the original position.

Preform and precursor temperatures at four precursor positions
Black: preform, left temperature axis; blue: precursor, right axis. Increasing precursor temperature alone would miss the preform optimum at 26.5 cm. Enlarge figure ↗
  1. Identify the mechanismBuoyancy controls the thermal field; porous placement alters local circulation.
  2. Test the design variableMove the precursor while retaining the other process conditions.
  3. Recommend a position26.5 cm balances precursor conditions and preform temperature.
  4. Check the physical outcomeCompare decomposition and SEM/EDS evidence from synthesis trials.

05 / THE MATERIAL OUTCOME

Close the loop between the flow field and what grew.

The numerical work becomes more persuasive when the predicted mechanism is connected to the physical reactor, the recovered material and its microscopic structure.

Tube, recovered growth and scanning-electron micrographs of fibers
Tube and material-growth observations with increasing magnification, from the source research presentation. SEM/EDS characterization: Laboratorio de Nanomateriales, Universidad de Colima. Enlarge figure ↗

A recommendation tested through synthesis

Experiments at fixed wall temperature, four-hour synthesis time, nitrogen supply and outlet condition compared the proposed positions. Measured precursor decomposition increased from 15.0% at 24.8 cm to 51.8% at 26.5 cm.

The source reports the densest Si₃N₄ fiber growth at the recommended position. Growth became sparser and more fragile at the more central positions, reinforcing that hotter precursor conditions alone do not define the best process.

Explain the location of growth

Recovery of Bénard-type cells downstream of the preform was linked to the face with the greatest fiber growth. A separate growth zone on the tube was interpreted through the interface between the two convection patterns.

These are experimentally observed outcomes interpreted using CFD—not reaction yields computed by the flow solver.

The Space Base, an SEM micrograph of NaF microstructures
“The Space Base” · Alberto Brambila Solórzano · Universidad de Colima. SEM image of NaF microstructures; image width 0.5 mm. Enlarge figure ↗

FIRST PLACE · NANOARTOGRAPHY 2017

Scientific observation,
communicated visually.

The Space Base captures cubic NaF microstructures from the CVD synthesis process. It received first place in the 2017 NanoArtography competition.

The micrograph connects this modeling project to the material world it investigated. It is NaF, distinct from the target Si₃N₄ fibers shown above.

View the official award record ↗

WHAT THIS WORK BRINGS TO ANOTHER PROJECT

A heat-transfer method that travels beyond materials synthesis.

The demonstrated capabilities are the reasoning, model construction and checks used to reach the recommendation.

Dimensionless heat-transfer analysis

Designed a fixed-Gr, variable-Re campaign and interpreted both Ri-dependent behavior and the regions where it breaks down.

Transfer: Mixed-convection assessment in enclosures, ducts, cooling passages and process equipment.

See the engineering evidence ↑

Physics-based model simplification

Built four incremental configurations and justified ideal-gas buoyancy and a Darcy porous resistance model.

Transfer: Choosing the required physical complexity in thermal systems and porous components.

See the engineering evidence ↑

Numerical and experimental validation

Used mesh sensitivity, a commercial-code comparison and independent physical measurements.

Transfer: Establishing confidence before using a CFD model for a design decision.

See the engineering evidence ↑

Simulation-to-experiment interpretation

Connected placement, thermal conditions, circulation and observed synthesis outcomes.

Transfer: Turning parameter sweeps into an engineering recommendation with a physical explanation.

See the engineering evidence ↑
Technical scope, source definitions and credits

All numerical results retain their thesis context. Reported Re, Gr and Ri are rounded values. The thesis source's compact Nu–Ri fit notation does not establish its axis normalization, so a raw-Ri fit is not reproduced here. The local/zone interpretation is retained.

The model excludes radiation and reaction chemistry and assumes steady laminar flow with homogeneous Darcy zones. The complete synthesis configuration was not directly validated by internal measurements. Implementation files are maintained privately.

CFD thesis: Alberto Brambila Solórzano, Universidad de Colima, 2018; supervisors Carlos I. Villavelázquez Mendoza and Carlos Escobar del Pozo. Apparatus, synthesis process and material characterization were collaborative. The award micrograph is credited to Alberto by the official competition record.

← Automated pump CFDFSI, rheology and particle transport →

Implementation files and detailed configurations are maintained privately. This page presents the engineering approach and selected evidence.