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Conjugate Scalar Transport

Updated 22 January 2026
  • Conjugate scalar transport is the modeling of scalar fields across fluid and solid phases with prescribed discontinuities at sharp interfaces.
  • It employs a volume penalization method with diffuse-interface representations to seamlessly integrate advection–diffusion in fluids and pure diffusion in solids.
  • Validation studies show that the method captures both scalar and flux jumps with relative errors below 3%, ensuring reliable simulations in complex geometries.

Conjugate scalar transport governs the coupled evolution of a scalar field—such as temperature or concentration—in multiphase domains, typically involving both fluid and solid regions separated by a sharp interface. This phenomenon is central to a wide range of thermal and chemical processes wherein the scalar and its normal flux may exhibit prescribed discontinuities (“jump conditions”) across the interface. Mathematical and computational treatments of conjugate scalar transport must systematically unify advection–diffusion equations with diverse interfacial boundary conditions over complex geometries (Liu et al., 15 Jan 2026).

1. Governing Equations for Multiphase Domains

Given a domain Ωe=ΩfΩs\Omega_e = \Omega_f \cup \Omega_s partitioned into fluid (Ωf\Omega_f) and solid (Ωs\Omega_s), distinct scalar fields cfc_f and csc_s are defined for each phase. The canonical governing equations are:

  • In the fluid (advection–diffusion):

tcf+ucf=(Dfcf)\partial_t c_f + \mathbf{u} \cdot \nabla c_f = \nabla \cdot (D_f \nabla c_f)

  • In the solid (pure diffusion):

tcs=(Dscs)\partial_t c_s = \nabla \cdot (D_s \nabla c_s)

where u\mathbf{u} is the velocity, and DfD_f, DsD_s are the molecular diffusivities in each region.

At the sharp interface Ωf\Omega_f0, the following generalized interfacial boundary conditions are imposed:

Ωf\Omega_f1

Ωf\Omega_f2

where Ωf\Omega_f3 is the outward unit normal from solid to fluid and Ωf\Omega_f4, Ωf\Omega_f5 are prescribed jumps in scalar and normal flux, respectively.

2. Diffuse-Interface Representation and Penalization Methodology

Simulations of conjugate scalar transport involving arbitrary interface geometry are computationally challenging, particularly when accommodating jump conditions. The volume penalization method (VPM), an immersed boundary approach, provides a framework for unifying the treatment of disparate subdomains and enforcing interfacial jump conditions (Liu et al., 15 Jan 2026).

A signed-distance level-set function Ωf\Omega_f6 encodes the interface: Ωf\Omega_f7 on Ωf\Omega_f8, Ωf\Omega_f9 in Ωs\Omega_s0, Ωs\Omega_s1 in Ωs\Omega_s2. A smoothed phase indicator Ωs\Omega_s3 transitions from Ωs\Omega_s4 (fluid) to Ωs\Omega_s5 (solid) over a thickness Ωs\Omega_s6, defined as

Ωs\Omega_s7

The unit normal is given by Ωs\Omega_s8.

For problems with a flux jump Ωs\Omega_s9 (pure Neumann), the penalization introduces a source confined to the interfacial region:

cfc_f0

This source asymptotically approaches a Dirac delta at cfc_f1 as cfc_f2, enforcing the required flux jump in the integral sense.

3. Unified Penalized Equation and Extension to Scalar Jumps

The volume penalization approach enables the solution of a unified equation across cfc_f3, with space-dependent coefficients:

cfc_f4

where

cfc_f5

If both scalar and flux jumps exist (cfc_f6, cfc_f7), an equivalent scalar field cfc_f8 is defined, with

cfc_f9

such that csc_s0 on csc_s1. The effective interfacial flux jump is

csc_s2

and the final penalized system becomes

csc_s3

Recovery of csc_s4 is achieved via csc_s5 (Liu et al., 15 Jan 2026).

4. Discretization and Computational Implementation

The VPM for conjugate scalar transport utilizes a finite-volume discretization on a Cartesian mesh. Second-order central differences are employed for both advection and diffusion operators. Time integration is handled by the fully implicit Euler scheme (first order in time). The interface mask, including the phase indicator and unit normal, is computed from the analytic or reinitialized level-set csc_s6; typically, csc_s7 with csc_s8 (where csc_s9 is the grid spacing). Adaptive mesh refinement (AMR) can be activated in regions where tcf+ucf=(Dfcf)\partial_t c_f + \mathbf{u} \cdot \nabla c_f = \nabla \cdot (D_f \nabla c_f)0 to ensure an adequate number of cells across the interface.

Outline of the VPM Algorithm

u\mathbf{u}4

5. Validation, Error Analysis, and Comparison

The VPM has been verified in several canonical test problems:

  • 1D diffusion with pure Neumann boundary: For tcf+ucf=(Dfcf)\partial_t c_f + \mathbf{u} \cdot \nabla c_f = \nabla \cdot (D_f \nabla c_f)1, analytical solution tcf+ucf=(Dfcf)\partial_t c_f + \mathbf{u} \cdot \nabla c_f = \nabla \cdot (D_f \nabla c_f)2 is recovered with first-order grid convergence. Average relative error is approximately tcf+ucf=(Dfcf)\partial_t c_f + \mathbf{u} \cdot \nabla c_f = \nabla \cdot (D_f \nabla c_f)3 for tcf+ucf=(Dfcf)\partial_t c_f + \mathbf{u} \cdot \nabla c_f = \nabla \cdot (D_f \nabla c_f)4, improving over the previous method (Brown-Dymkoski et al. 2014) which incurred up to tcf+ucf=(Dfcf)\partial_t c_f + \mathbf{u} \cdot \nabla c_f = \nabla \cdot (D_f \nabla c_f)5 error and exhibited nonphysical tcf+ucf=(Dfcf)\partial_t c_f + \mathbf{u} \cdot \nabla c_f = \nabla \cdot (D_f \nabla c_f)6 in the solid.
  • 2D fluid–solid coupled diffusion: For a cylindrical geometry (tcf+ucf=(Dfcf)\partial_t c_f + \mathbf{u} \cdot \nabla c_f = \nabla \cdot (D_f \nabla c_f)7 in tcf+ucf=(Dfcf)\partial_t c_f + \mathbf{u} \cdot \nabla c_f = \nabla \cdot (D_f \nabla c_f)8), four cases with varying tcf+ucf=(Dfcf)\partial_t c_f + \mathbf{u} \cdot \nabla c_f = \nabla \cdot (D_f \nabla c_f)9 closely match reference body-fitted mesh (BFM) simulations; all relative deviations along tcs=(Dscs)\partial_t c_s = \nabla \cdot (D_s \nabla c_s)0 are below tcs=(Dscs)\partial_t c_s = \nabla \cdot (D_s \nabla c_s)1 (mean tcs=(Dscs)\partial_t c_s = \nabla \cdot (D_s \nabla c_s)2). Mesh convergence on Cartesian grids with AMR achieves less than tcs=(Dscs)\partial_t c_s = \nabla \cdot (D_s \nabla c_s)3 change for tcs=(Dscs)\partial_t c_s = \nabla \cdot (D_s \nabla c_s)4 cells.
  • 2D advection–diffusion: At tcs=(Dscs)\partial_t c_s = \nabla \cdot (D_s \nabla c_s)5, tcs=(Dscs)\partial_t c_s = \nabla \cdot (D_s \nabla c_s)6, tcs=(Dscs)\partial_t c_s = \nabla \cdot (D_s \nabla c_s)7, tcs=(Dscs)\partial_t c_s = \nabla \cdot (D_s \nabla c_s)8, tcs=(Dscs)\partial_t c_s = \nabla \cdot (D_s \nabla c_s)9 on a cylinder of u\mathbf{u}0 in u\mathbf{u}1, the VPM achieves a relative deviation of approximately u\mathbf{u}2 versus BFM (chtMultiRegionFoam). Both scalar and flux jumps are captured.

In all test cases, the VPM enforces the interfacial jump in an integral sense while confining the penalization source to the narrow interfacial band, thereby avoiding pollution of the solid region (Liu et al., 15 Jan 2026).

6. Advantages, Limitations, and Interpretations

The VPM presented provides a unified diffuse-interface formulation for fluid–solid conjugate scalar transport, accommodating arbitrary jumps in scalar and its flux. It eliminates the need for explicitly body-fitted grids, simplifies mesh generation for complex geometries, and enables application of standard finite-volume tools. Relative errors typically remain below u\mathbf{u}3 in challenging multiphase test cases.

A plausible implication is that this approach facilitates accurate and efficient simulation in cases with complex interface geometry and general jump conditions, which are prevalent in thermal and chemical engineering contexts. However, grid convergence is first-order rather than second-order in the vicinity of the interface, due to the diffuse treatment; this may limit its use in applications where higher-order interface capturing is essential (Liu et al., 15 Jan 2026).

The VPM methodology constitutes a significant development for simulating conjugate transport across multiphase domains with nontrivial boundary conditions. Its validation against reference body-fitted mesh methods, as well as its compact divergence-form source for interfacial jumps, position it as a promising approach for complex engineering scenarios without requiring elaborate mesh construction. The method’s utility for cases with both scalar and flux jumps, combined with robust error characteristics and absence of nonphysical interior contamination, underscores its practical value in computational studies of multiphase transport phenomena (Liu et al., 15 Jan 2026).

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