All Study Guides Mathematical Fluid Dynamics Unit 10
💨 Mathematical Fluid Dynamics Unit 10 – Multiphase & Multicomponent FlowsMultiphase and multicomponent flows involve multiple phases or chemical species interacting within a system. These flows are ubiquitous in nature and industry, from oil pipelines to blood vessels. Understanding their behavior is crucial for designing efficient processes and predicting environmental impacts.
Key concepts include volume fractions, interfacial phenomena, and flow regimes. Fundamental equations describe mass, momentum, and energy conservation for each phase. Various modeling techniques, from Eulerian-Eulerian to interface tracking methods, are used to simulate these complex flows across diverse applications.
Key Concepts and Definitions
Multiphase flow involves the simultaneous presence of two or more phases (gas, liquid, or solid) in a system
Multicomponent flow consists of a mixture of different chemical species or components within a single phase
Phase refers to a distinct state of matter (gas, liquid, or solid) with homogeneous physical properties
Interface represents the boundary between two phases where properties change discontinuously
Volume fraction ( α k ) (\alpha_k) ( α k ) quantifies the proportion of each phase k k k in a given volume
Defined as the ratio of the volume occupied by phase k k k to the total volume
Satisfies the constraint ∑ k = 1 N α k = 1 \sum_{k=1}^N \alpha_k = 1 ∑ k = 1 N α k = 1 , where N N N is the total number of phases
Interfacial area concentration ( α i ) (\alpha_i) ( α i ) measures the amount of interfacial area per unit volume
Slip velocity ( v ⃗ s l i p ) (\vec{v}_{slip}) ( v s l i p ) represents the relative velocity between phases
Calculated as the difference between the phase velocities v ⃗ s l i p = v ⃗ 1 − v ⃗ 2 \vec{v}_{slip} = \vec{v}_1 - \vec{v}_2 v s l i p = v 1 − v 2
Interfacial transfer terms describe the exchange of mass, momentum, and energy between phases
Fundamental Equations
Conservation of mass (continuity equation) for each phase k k k :
∂ ( α k ρ k ) ∂ t + ∇ ⋅ ( α k ρ k v ⃗ k ) = Γ k \frac{\partial (\alpha_k \rho_k)}{\partial t} + \nabla \cdot (\alpha_k \rho_k \vec{v}_k) = \Gamma_k ∂ t ∂ ( α k ρ k ) + ∇ ⋅ ( α k ρ k v k ) = Γ k
ρ k \rho_k ρ k is the density of phase k k k , v ⃗ k \vec{v}_k v k is the velocity of phase k k k , and Γ k \Gamma_k Γ k represents mass transfer to phase k k k
Conservation of momentum for each phase k k k :
∂ ( α k ρ k v ⃗ k ) ∂ t + ∇ ⋅ ( α k ρ k v ⃗ k v ⃗ k ) = − α k ∇ p + ∇ ⋅ ( α k τ k ) + α k ρ k g ⃗ + M ⃗ k \frac{\partial (\alpha_k \rho_k \vec{v}_k)}{\partial t} + \nabla \cdot (\alpha_k \rho_k \vec{v}_k \vec{v}_k) = -\alpha_k \nabla p + \nabla \cdot (\alpha_k \tau_k) + \alpha_k \rho_k \vec{g} + \vec{M}_k ∂ t ∂ ( α k ρ k v k ) + ∇ ⋅ ( α k ρ k v k v k ) = − α k ∇ p + ∇ ⋅ ( α k τ k ) + α k ρ k g + M k
p p p is the pressure, τ k \tau_k τ k is the stress tensor of phase k k k , g ⃗ \vec{g} g is the gravitational acceleration, and M ⃗ k \vec{M}_k M k represents interfacial momentum transfer to phase k k k
Conservation of energy for each phase k k k :
∂ ( α k ρ k E k ) ∂ t + ∇ ⋅ ( α k ρ k H k v ⃗ k ) = − ∇ ⋅ ( α k q ⃗ k ) + α k D p D t + ∇ ⋅ ( α k τ k ⋅ v ⃗ k ) + α k ρ k g ⃗ ⋅ v ⃗ k + Q k \frac{\partial (\alpha_k \rho_k E_k)}{\partial t} + \nabla \cdot (\alpha_k \rho_k H_k \vec{v}_k) = -\nabla \cdot (\alpha_k \vec{q}_k) + \alpha_k \frac{Dp}{Dt} + \nabla \cdot (\alpha_k \tau_k \cdot \vec{v}_k) + \alpha_k \rho_k \vec{g} \cdot \vec{v}_k + Q_k ∂ t ∂ ( α k ρ k E k ) + ∇ ⋅ ( α k ρ k H k v k ) = − ∇ ⋅ ( α k q k ) + α k D t D p + ∇ ⋅ ( α k τ k ⋅ v k ) + α k ρ k g ⋅ v k + Q k
E k E_k E k is the total energy of phase k k k , H k H_k H k is the total enthalpy of phase k k k , q ⃗ k \vec{q}_k q k is the heat flux vector of phase k k k , and Q k Q_k Q k represents interfacial energy transfer to phase k k k
Closure relations are needed to model interfacial transfer terms, phase interactions, and constitutive equations
Classification of Multiphase Flows
Gas-liquid flows (bubbly flow, slug flow, churn flow, annular flow)
Gas-solid flows (pneumatic conveying, fluidized beds)
Liquid-liquid flows (immiscible liquids, emulsions)
Liquid-solid flows (slurry transport, sedimentation)
Three-phase flows (gas-liquid-solid systems)
Classified based on the state of the dispersed phase
Bubbly flows have gas bubbles dispersed in a continuous liquid phase
Droplet flows have liquid droplets dispersed in a continuous gas phase
Particulate flows have solid particles dispersed in a continuous gas or liquid phase
Flow patterns depend on factors such as phase properties, flow rates, and geometry
Horizontal pipes exhibit stratified, wavy, slug, and annular flow patterns
Vertical pipes display bubbly, slug, churn, and annular flow patterns
Interfacial Phenomena
Surface tension ( σ ) (\sigma) ( σ ) arises from the imbalance of molecular forces at the interface
Causes the interface to minimize its surface area and form spherical shapes (bubbles, droplets)
Quantified as the force per unit length acting tangentially to the interface
Capillary pressure ( Δ p c ) (\Delta p_c) ( Δ p c ) is the pressure difference across a curved interface
Related to surface tension and interface curvature by the Young-Laplace equation: Δ p c = σ ( 1 R 1 + 1 R 2 ) \Delta p_c = \sigma (\frac{1}{R_1} + \frac{1}{R_2}) Δ p c = σ ( R 1 1 + R 2 1 )
R 1 R_1 R 1 and R 2 R_2 R 2 are the principal radii of curvature
Marangoni effect refers to the mass transfer along an interface due to surface tension gradients
Caused by temperature or concentration gradients
Induces interfacial flow from regions of low surface tension to high surface tension
Wetting and contact angles describe the interaction between a liquid and a solid surface
Contact angle ( θ ) (\theta) ( θ ) is the angle formed by the liquid-vapor interface and the solid surface
Wetting occurs when θ < 9 0 ∘ \theta < 90^\circ θ < 9 0 ∘ , non-wetting when θ > 9 0 ∘ \theta > 90^\circ θ > 9 0 ∘
Interfacial instabilities (Rayleigh-Taylor, Kelvin-Helmholtz) can lead to the breakup of interfaces
Rayleigh-Taylor instability occurs when a denser fluid is above a lighter fluid
Kelvin-Helmholtz instability arises from velocity shear at the interface between two fluids
Flow Regimes and Patterns
Flow regimes characterize the spatial distribution of phases in a multiphase system
Determined by factors such as phase properties, flow rates, and geometry
Gas-liquid flow regimes in vertical pipes:
Bubbly flow: discrete gas bubbles dispersed in a continuous liquid phase
Slug flow: large bullet-shaped gas bubbles (Taylor bubbles) separated by liquid slugs
Churn flow: chaotic and oscillatory flow with irregular gas structures
Annular flow: gas flows in the core, and liquid flows as a film along the pipe wall
Gas-liquid flow regimes in horizontal pipes:
Stratified flow: gas and liquid flow separately with a smooth interface
Wavy flow: gas and liquid flow separately with a wavy interface
Slug flow: intermittent liquid slugs and elongated gas bubbles
Annular flow: similar to vertical annular flow
Flow pattern maps (Baker chart, Taitel-Dukler map) predict flow regimes based on dimensionless parameters
Dimensionless parameters include superficial velocities, density ratio, and viscosity ratio
Transition criteria between flow regimes based on stability analysis and empirical correlations
Modeling Techniques
Eulerian-Eulerian (two-fluid) model treats each phase as a separate continuum
Solves averaged conservation equations for each phase
Requires closure relations for interfacial transfer terms and phase interactions
Suitable for dispersed flows with high volume fractions
Eulerian-Lagrangian model treats the continuous phase as a continuum and the dispersed phase as discrete particles
Solves averaged conservation equations for the continuous phase
Tracks individual particles using Newton's second law of motion
Accounts for particle-fluid and particle-particle interactions
Suitable for dilute dispersed flows with low volume fractions
Mixture model considers the multiphase flow as a single fluid with averaged properties
Solves conservation equations for the mixture
Uses algebraic expressions to determine phase velocities and volume fractions
Applicable when the phases are strongly coupled and have similar velocities
Interface tracking methods (Volume of Fluid, Level Set) explicitly capture the interface between phases
Volume of Fluid (VOF) method uses a color function to represent the volume fraction of each phase in a cell
Level Set method defines the interface as a zero level set of a signed distance function
Accurately resolve interface geometry and topology changes
Averaging techniques (time averaging, volume averaging, ensemble averaging) derive macroscopic equations from microscopic descriptions
Time averaging is suitable for steady flows
Volume averaging is used for systems with spatial inhomogeneities
Ensemble averaging is employed for turbulent and stochastic flows
Numerical Methods and Simulations
Finite volume method (FVM) is widely used for multiphase flow simulations
Discretizes the computational domain into control volumes
Enforces conservation principles by balancing fluxes across control volume faces
Handles complex geometries and unstructured grids
Staggered grid arrangement stores velocity components at cell faces and scalar quantities at cell centers
Prevents checkerboard pressure oscillations
Facilitates the implementation of momentum interpolation schemes (QUICK, MUSCL)
Pressure-velocity coupling algorithms (SIMPLE, PISO) solve the coupled system of equations
SIMPLE (Semi-Implicit Method for Pressure-Linked Equations) is an iterative algorithm
PISO (Pressure Implicit with Splitting of Operators) is a non-iterative algorithm
Advection schemes (upwind, central differencing, TVD) discretize the convective terms in the governing equations
Upwind schemes are stable but prone to numerical diffusion
Central differencing schemes are second-order accurate but may introduce oscillations
TVD (Total Variation Diminishing) schemes combine the advantages of upwind and central differencing
Temporal discretization schemes (explicit, implicit, Crank-Nicolson) integrate the equations in time
Explicit schemes are straightforward to implement but have stability restrictions
Implicit schemes are unconditionally stable but require the solution of a linear system
Crank-Nicolson scheme is second-order accurate and unconditionally stable
Turbulence modeling (RANS, LES, DNS) captures the effects of turbulence on multiphase flows
RANS (Reynolds-Averaged Navier-Stokes) models solve for averaged quantities and model turbulence effects
LES (Large Eddy Simulation) resolves large-scale turbulent structures and models sub-grid scale effects
DNS (Direct Numerical Simulation) resolves all scales of turbulence but is computationally expensive
Applications and Case Studies
Oil and gas industry: multiphase flow in pipelines, separators, and wells
Predicting flow patterns and pressure drops in pipelines
Designing efficient separators for oil-water-gas mixtures
Modeling gas-liquid flow in wellbores and risers
Chemical and process engineering: reactors, heat exchangers, and distillation columns
Simulating gas-liquid reactors (bubble columns, airlift reactors) for mass transfer and reaction kinetics
Designing multi-phase heat exchangers for enhanced heat transfer
Modeling distillation columns for separation processes
Nuclear engineering: two-phase flow in boiling water reactors (BWRs) and pressurized water reactors (PWRs)
Predicting void fraction and critical heat flux in BWRs
Analyzing departure from nucleate boiling (DNB) in PWRs
Simulating two-phase flow instabilities and flow-induced vibrations
Environmental engineering: sediment transport, bubble plumes, and oil spills
Modeling sediment transport in rivers and coastal areas
Simulating bubble plumes for aeration and mixing in water bodies
Predicting the fate and transport of oil spills in marine environments
Biomedical engineering: blood flow, drug delivery, and microfluidic devices
Simulating blood flow as a multiphase mixture of plasma and blood cells
Modeling drug delivery systems with nanoparticles or microbubbles
Designing microfluidic devices for cell separation and analysis
Aerospace engineering: fuel injection, spray combustion, and icing
Simulating fuel injection and atomization in combustion chambers
Modeling spray combustion and pollutant formation
Predicting ice accretion on aircraft wings and engines
Geophysical flows: volcanic eruptions, geysers, and hydrothermal vents
Simulating gas-particle flows in volcanic plumes and pyroclastic density currents
Modeling geyser eruptions driven by two-phase flow in geothermal systems
Investigating multiphase flow in hydrothermal vents and black smokers