Combustion and Reactions Chapter 7: Multiphase Combustion and Pollutant Formation

This chapter develops the modeling framework for multiphase combustion systems involving liquid sprays, coal particles, evaporation, devolatilization, heterogeneous reactions, and pollutant formation. The central challenge is coupling particle dynamics, turbulence, chemistry, heat transfer, and radiation inside reacting flows. The chapter introduces Discrete Phase Modeling (DPM), spray combustion physics, coal combustion mechanisms, NOx formation pathways, and selective catalytic reduction (SCR) systems used for emission control.

 

Context and Motivation

Many industrial combustion systems involve:

  • Liquid droplets

  • Solid particles

  • Coal dust

  • Fuel sprays

  • Ash and soot

  • Pollutant formation

Examples include:

  • Diesel engines

  • Coal-fired power plants

  • Gas turbines

  • Industrial furnaces

  • SCR aftertreatment systems

Unlike single-phase gaseous combustion:

  • Fuel exists initially as discrete particles or droplets

  • Additional processes appear:

    • Injection

    • Atomization

    • Evaporation

    • Devolatilization

    • Char oxidation

    • Particle heating

    • Radiation coupling

The combustion process therefore becomes a strongly coupled multiphysics problem.


1. Discrete Phase Modeling (DPM)

Core Philosophy

The most important framework for dilute particle flows is:

  • Discrete Phase Modeling (DPM)

In DPM:

  • Gas phase solved in Eulerian framework

  • Particles tracked individually in Lagrangian framework

This creates:

  • Eulerian–Lagrangian coupling

Continuous vs Dispersed Phase

Two phases coexist:

Continuous Phase

  • Gas flow

  • Solved on mesh

Discrete Phase

  • Particles or droplets

  • Tracked as trajectories

Particles exchange:

  • Mass

  • Momentum

  • Energy

with the surrounding gas.

Why DPM Works

DPM assumes:

  • Particle volume fraction is relatively low

  • Particle–particle interaction negligible

Typically:

  • Volume loading below roughly 10%

Physically:

  • Particles “feel” the flow

  • But particles do not strongly interfere with each other

One-Way vs Two-Way Coupling

One-Way Coupling

  • Gas affects particles

  • Particles do not affect gas

Valid when:

  • Particle loading small

Two-Way Coupling

Particles also modify:

  • Flow momentum

  • Temperature

  • Species concentrations

Required when:

  • Heat release significant

  • Evaporation important

  • Mass loading large

This is essential for realistic combustion simulations.


2. Particle Dynamics and Life Cycle

Particle Motion

Particle trajectories are determined by:

  • Drag

  • Gravity

  • Pressure-gradient forces

  • Turbulent dispersion

  • Additional body forces

Particles continuously evolve as they travel.

Particle Life Cycle

A combusting particle typically undergoes:

  1. Injection

  2. Heating

  3. Evaporation or devolatilization

  4. Chemical reaction

  5. Burnout or escape

The particle state changes continuously:

  • Diameter

  • Temperature

  • Velocity

  • Composition

Turbulent Dispersion

Particles entering turbulent eddies experience:

  • Random lateral dispersion

  • Stochastic trajectory fluctuations

This strongly affects:

  • Mixing

  • Residence time

  • Combustion distribution

Discrete Random Walk Model

One common approach:

  • Particles interact statistically with turbulent eddies

Physically:

  • Simulates random turbulent scattering

Important insight:

  • Too few stochastic samples produce noisy source terms and convergence problems


3. Spray Combustion

Spray Physics

Liquid fuel combustion begins with:

  • Injection through nozzle

  • Atomization into droplets

Droplets then:

  • Heat up

  • Evaporate

  • Mix with oxidizer

  • Ignite

Combustion therefore depends heavily on:

  • Spray quality

  • Droplet size distribution

  • Injection velocity

  • Turbulence

Atomization

The liquid jet breaks into droplets due to:

  • Aerodynamic instabilities

  • Surface tension effects

  • Turbulent stresses

Smaller droplets:

  • Evaporate faster

  • Mix faster

  • Burn more efficiently

Droplet Heating and Evaporation

The droplet receives heat from surrounding gases.

This energy:

  • Raises droplet temperature

  • Eventually causes phase change

Evaporation rate depends strongly on:

  • Temperature

  • Relative velocity

  • Surface area

Spray Combustion in Engines

The ECN Spray A diesel case illustrates the full process:

  • High-pressure liquid injection

  • Spray penetration

  • Evaporation

  • Autoignition

  • Turbulent combustion

Important physical insight:
→ Ignition delay depends strongly on:

  • Ambient temperature

  • Mixing rate

  • Detailed chemical kinetics

Chemistry Complexity

Detailed diesel chemistry may involve:

  • Hundreds of species

  • Hundreds of reactions

This creates:

  • Severe numerical stiffness

Acceleration methods such as:

  • ISAT

  • Dynamic mechanism reduction

become necessary


4. Coal Combustion

Coal Flame Structure

Coal combustion is fundamentally multiphase.

The fuel particle undergoes multiple stages:

  1. Heating

  2. Drying

  3. Devolatilization

  4. Char combustion

The volatile gases burn in the gas phase, while remaining solid carbon burns heterogeneously

Devolatilization

As coal heats:

  • Volatile compounds are released

These gases:

  • Mix with air

  • Burn similarly to gaseous flames

The remaining particle becomes:

  • Char

Char Combustion

Char burns at the particle surface through heterogeneous reactions.

The reaction rate depends on:

  • Oxygen diffusion

  • Surface kinetics

  • Temperature

At high temperatures:

  • Diffusion often limits the process

Swirl-Stabilized Coal Burners

Industrial coal burners often use:

  • Strong swirl

Swirl creates:

  • Central recirculation zones

These zones:

  • Trap hot gases

  • Improve ignition

  • Stabilize combustion

Coal Combustion Modeling

Important submodels include:

  • Devolatilization model

  • Char oxidation model

  • Radiation model

  • Turbulence–chemistry interaction

Several devolatilization approaches exist:

  • Constant rate

  • Single-rate kinetics

  • Competing-rate models

  • CPD models

Sequential Solution Strategy

Coal combustion simulations are numerically difficult.

A stable workflow usually proceeds gradually:

  1. Cold flow

  2. Reactive flow

  3. Radiation

  4. Particle radiation

This improves convergence robustness


5. Radiation in Combustion

Why Radiation Matters

Combustion temperatures are high enough that:

  • Radiative heat transfer becomes dominant

In furnaces:

  • Radiation may dominate over convection

Participating Media

Important radiating species:

  • CO2

  • H2O

  • Soot

  • Coal particles

Particles strongly modify:

  • Temperature distribution

  • Heat fluxes

  • Flame stability

Particle Radiation

Coal particles:

  • Emit

  • Absorb

  • Scatter radiation

Ignoring this effect can significantly distort:

  • Furnace temperatures

  • Heat transfer prediction


6. Pollutant Formation

Importance of Pollutants

Combustion generates:

  • NOx

  • CO

  • Unburned hydrocarbons

  • Soot

NOx is one of the most important pollutants because:

  • Strongly regulated

  • Harmful to health

  • Contributes to smog and acid rain


7. NOx Formation Mechanisms

Several pathways produce NOx.

Thermal NOx

Produced at:

  • High temperatures

Mechanism:

  • Nitrogen from air reacts with oxygen radicals

Strong temperature dependence:

  • Small temperature increase → huge NO increase

This is why:

  • Peak flame temperature is critical

Prompt NOx

Occurs in:

  • Fuel-rich regions

Forms rapidly through:

  • Hydrocarbon radical chemistry

Usually important near:

  • Flame fronts

Fuel NOx

Occurs when:

  • Fuel itself contains nitrogen

Very important in:

  • Coal combustion

Fuel nitrogen converts into:

  • HCN

  • NH3

  • NO

N2O Mechanism

Relevant mainly for:

  • Lean flames

  • High-pressure systems

Usually smaller contribution in conventional flames.


8. Pollutant Modeling Philosophy

Postprocessing Assumption

Pollutant concentrations are usually:

  • Much smaller than main species

Therefore:

  • Pollutants assumed not to significantly alter main flow field

This allows:
→ Pollutant calculations using frozen combustion fields

This greatly reduces computational cost.

Sensitivity to Temperature

NOx prediction is extremely temperature-sensitive.

Even small temperature errors may produce:

  • Large NO prediction errors

Therefore:

  • Radiation

  • Turbulence

  • Chemistry

  • Boundary conditions

must all be reasonably accurate.

Engineering Reality

Absolute NOx prediction is difficult.

However:

  • CFD is extremely valuable for:

    • Parametric studies

    • Design optimization

    • Trend analysis


9. Selective Catalytic Reduction (SCR)

Purpose

SCR systems reduce NOx emissions after combustion.

Widely used in:

  • Diesel engines

  • Power plants

  • Industrial exhaust systems

Operating Principle

A reducing agent (typically ammonia or urea) reacts with NOx over a catalyst surface:

  • NOx converted into:

    • Nitrogen

    • Water

SCR Process Stages

Typical sequence:

  1. Urea injection

  2. Atomization

  3. Evaporation

  4. Thermal decomposition

  5. Mixing with exhaust

  6. Catalytic reduction

Importance of Mixing

Uniform ammonia distribution before catalyst is critical.

Poor mixing causes:

  • Low NOx conversion

  • Ammonia slip

  • Catalyst inefficiency

Porous Catalyst Modeling

The catalyst is usually represented as:

  • Porous medium

This captures:

  • Pressure loss

  • Flow redistribution

  • Species conversion

without resolving tiny catalyst channels directly.


10. Numerical and CFD Aspects

Mesh Requirements

Critical regions:

  • Injection zone

  • Flame stabilization region

  • Shear layers

  • Near-wall heat transfer

  • Catalyst regions

Sprays often require:

  • Strong local refinement

Tracking Parameters

Particle tracking depends on:

  • Time step

  • Step length

  • Maximum tracking steps

Too large time steps:

  • Inaccurate trajectories

  • Poor evaporation prediction

Boundary Conditions

Particles reaching walls may:

  • Escape

  • Reflect

  • Trap

  • Form liquid film

Wall interaction models become important in:

  • Engine sprays

  • Fuel impingement

  • SCR systems

Steady vs Unsteady Tracking

Steady tracking:

  • Lower computational cost

Unsteady tracking:

  • Required for:

    • Spray breakup

    • Transient combustion

    • Pulsed injection

Double Precision

Combustion problems often require:

  • Double precision

Especially for:

  • High temperature gradients

  • Stiff chemistry

  • Complex geometries




Physical Interpretation and Engineering Intuition

Combustion Efficiency Depends on Mixing

Whether in sprays, coal flames, or SCR systems:
→ Mixing controls performance.

Particle Size Is Critical

Smaller particles:

  • Heat faster

  • Evaporate faster

  • Burn faster

Large particles:

  • Longer residence times

  • Incomplete combustion risk

Swirl Is Primarily a Stabilization Tool

Swirl generates:

  • Internal recirculation

This:

  • Increases residence time

  • Recirculates hot products

  • Stabilizes flames

Radiation Cannot Be Ignored

At furnace temperatures:

  • Radiation strongly modifies temperature fields

Ignoring it:

  • Produces unrealistic flame behavior

Pollutants Are Extremely Sensitive

NOx formation depends on:

  • Local temperature

  • Oxygen availability

  • Residence time

Very small modeling errors may strongly affect emissions prediction.


Applications

  • Diesel engine combustion

  • Coal-fired power plants

  • Industrial furnaces

  • Gas turbines

  • SCR aftertreatment systems

  • Spray combustors

  • Biomass combustion


Limitations and Assumptions

DPM

  • Assumes dilute dispersed phase

  • Limited particle–particle interaction

Spray Models

  • Sensitive to breakup assumptions

  • Initial droplet distribution uncertain

Coal Models

  • Coal properties highly variable

  • Devolatilization models approximate

NOx Models

  • Extremely temperature sensitive

  • Strong dependence on combustion accuracy

SCR Models

  • Catalyst chemistry simplified

  • Mixing assumptions important


Study Priorities

If short on time:

  1. DPM philosophy (Eulerian–Lagrangian coupling)

  2. One-way vs two-way coupling

  3. Spray evaporation process

  4. Coal devolatilization and char combustion

  5. Swirl stabilization

  6. Radiation importance

  7. Thermal vs prompt vs fuel NOx

  8. SCR operating principle


Key Takeaways

  • Multiphase combustion couples particle physics with reacting flow dynamics.

  • DPM tracks particles individually while solving gas flow in Eulerian form.

  • Spray combustion depends heavily on atomization and evaporation.

  • Coal combustion involves devolatilization followed by char oxidation.

  • Swirl stabilizes flames through recirculation zones.

  • Radiation becomes dominant in high-temperature furnaces.

  • NOx formation is extremely sensitive to local flame temperature.

  • SCR systems reduce NOx through catalytic reactions using ammonia or urea injection.

  • Accurate multiphase combustion CFD requires careful coupling of turbulence, chemistry, radiation, and particle dynamics.

Next
Next

Combustion and Reactions Chapter 6: Turbulent PREMIXED Combustion