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Frank–Kamenetskii Viscosity

Updated 9 July 2026
  • Frank–Kamenetskii viscosity is a linearized, temperature-dependent law derived from the Arrhenius formulation, encapsulating temperature sensitivity in a constant parameter Θ.
  • It simplifies convection analysis by enabling clear classification of mobile, sluggish, and stagnant lid regimes through controlled viscosity contrast.
  • The law is pivotal for scaling studies, influencing Nusselt–Rayleigh relationships and thermal boundary layer stability in both laboratory and geophysical flows.

Frank–Kamenetskii viscosity is the temperature-dependent viscosity law obtained by linearizing an Arrhenius-type dependence about a reference temperature and then nondimensionalizing with the viscosity at the top surface. In the formulation used for internally heated steady thermal convection, the nondimensional law is

η(T)=η0exp(ΘT),\eta(T)=\eta_0\exp(-\Theta T),

with nondimensional temperature T=θphys/ΔTT=\theta_{\mathrm{phys}}/\Delta T and nondimensional Frank–Kamenetskii parameter

ΘEaΔTRTref2.\Theta\equiv \frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}.

In the cited study, Θ\Theta is denoted by γ\gamma, and the law is used to analyze steady two-dimensional convective solutions, lid-regime classification, viscosity contrast, and Nusselt–Rayleigh scaling under homogeneous internal heating (Okuda et al., 22 Aug 2025).

1. Mathematical formulation

The starting point is an Arrhenius-type temperature dependence,

ηphys(Tphys)=ηrefexp ⁣[EaR(1Tphys1Tref)].\eta_{\mathrm{phys}}(T_{\mathrm{phys}})=\eta_{\mathrm{ref}}\exp\!\left[\frac{E_a}{R}\left(\frac{1}{T_{\mathrm{phys}}}-\frac{1}{T_{\mathrm{ref}}}\right)\right].

Expanding about a reference temperature TrefT_{\mathrm{ref}} and introducing a temperature scale ΔT\Delta T produces, to leading order, the Frank–Kamenetskii form

ηphysηrefexp ⁣[EaΔTRTref2θphys].\eta_{\mathrm{phys}}\simeq \eta_{\mathrm{ref}}\exp\!\left[-\frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}\,\theta_{\mathrm{phys}}\right].

Upon nondimensionalization with η0=η\eta_0=\eta at the top surface and T=θphys/ΔTT=\theta_{\mathrm{phys}}/\Delta T0, the viscosity law becomes

T=θphys/ΔTT=\theta_{\mathrm{phys}}/\Delta T1

where

T=θphys/ΔTT=\theta_{\mathrm{phys}}/\Delta T2

The paper denotes T=θphys/ΔTT=\theta_{\mathrm{phys}}/\Delta T3 by T=θphys/ΔTT=\theta_{\mathrm{phys}}/\Delta T4 (Okuda et al., 22 Aug 2025).

In this representation, the key structural feature is that the temperature sensitivity is controlled by a constant nondimensional parameter. This distinguishes the Frank–Kamenetskii law from the full Arrhenius form, whose effective sensitivity varies with temperature. A plausible implication is that the Frank–Kamenetskii law is especially convenient when regime structure and scaling are the primary targets, because the temperature dependence is compressed into a single constant parameter.

2. Derivation and nondimensionalization

The governing scales are specified as follows: the length scale is the layer thickness T=θphys/ΔTT=\theta_{\mathrm{phys}}/\Delta T5; the temperature scale is T=θphys/ΔTT=\theta_{\mathrm{phys}}/\Delta T6 with uniform internal heating T=θphys/ΔTT=\theta_{\mathrm{phys}}/\Delta T7 and thermal conductivity T=θphys/ΔTT=\theta_{\mathrm{phys}}/\Delta T8; the time scale is the thermal diffusion time T=θphys/ΔTT=\theta_{\mathrm{phys}}/\Delta T9 with thermal diffusivity ΘEaΔTRTref2.\Theta\equiv \frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}.0; and the viscosity scale is ΘEaΔTRTref2.\Theta\equiv \frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}.1, the viscosity at the top surface (Okuda et al., 22 Aug 2025).

Starting from

ΘEaΔTRTref2.\Theta\equiv \frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}.2

one writes ΘEaΔTRTref2.\Theta\equiv \frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}.3, assumes ΘEaΔTRTref2.\Theta\equiv \frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}.4, and expands

ΘEaΔTRTref2.\Theta\equiv \frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}.5

This gives

ΘEaΔTRTref2.\Theta\equiv \frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}.6

Defining ΘEaΔTRTref2.\Theta\equiv \frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}.7 and ΘEaΔTRTref2.\Theta\equiv \frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}.8 then yields

ΘEaΔTRTref2.\Theta\equiv \frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}.9

The approximation Θ\Theta0 is identified as the Frank–Kamenetskii approximation; it neglects higher-order curvature of the true Arrhenius dependence. This fixes the precise mathematical status of the law: it is not an independent constitutive ansatz in the cited treatment, but a leading-order approximation to Arrhenius rheology under a small-perturbation expansion.

3. Viscosity contrast and parameter interpretation

If the local nondimensional temperature varies between Θ\Theta1 at the top and Θ\Theta2 at the bottom of the convective layer, the viscosity contrast is

Θ\Theta3

In the paper, Θ\Theta4 is the mean bottom temperature, and Θ\Theta5 measures how many orders of magnitude Θ\Theta6 changes over the layer (Okuda et al., 22 Aug 2025).

The parameter Θ\Theta7 measures the sensitivity of viscosity to temperature change per unit of the chosen Θ\Theta8. Large Θ\Theta9 corresponds to strong temperature dependence, and small γ\gamma0 to weak temperature dependence. The reported ranges are γ\gamma1 to γ\gamma2 in lab-fluids and engineering flows, while mantle convection applications are described by γ\gamma3–γ\gamma4, γ\gamma5, and γ\gamma6, giving γ\gamma7–γ\gamma8. These are also the values explored in the paper, with γ\gamma9 from ηphys(Tphys)=ηrefexp ⁣[EaR(1Tphys1Tref)].\eta_{\mathrm{phys}}(T_{\mathrm{phys}})=\eta_{\mathrm{ref}}\exp\!\left[\frac{E_a}{R}\left(\frac{1}{T_{\mathrm{phys}}}-\frac{1}{T_{\mathrm{ref}}}\right)\right].0 up to ηphys(Tphys)=ηrefexp ⁣[EaR(1Tphys1Tref)].\eta_{\mathrm{phys}}(T_{\mathrm{phys}})=\eta_{\mathrm{ref}}\exp\!\left[\frac{E_a}{R}\left(\frac{1}{T_{\mathrm{phys}}}-\frac{1}{T_{\mathrm{ref}}}\right)\right].1 (Okuda et al., 22 Aug 2025).

This parameterization makes viscosity contrast an exponentially amplified function of the thermal state. A plausible implication is that relatively modest changes in ηphys(Tphys)=ηrefexp ⁣[EaR(1Tphys1Tref)].\eta_{\mathrm{phys}}(T_{\mathrm{phys}})=\eta_{\mathrm{ref}}\exp\!\left[\frac{E_a}{R}\left(\frac{1}{T_{\mathrm{phys}}}-\frac{1}{T_{\mathrm{ref}}}\right)\right].2 or in bottom temperature can reorganize the convective regime even when other control parameters remain fixed.

4. Relation to the Arrhenius-law formulation

The paper also implements the full Arrhenius law in nondimensional form as

ηphys(Tphys)=ηrefexp ⁣[EaR(1Tphys1Tref)].\eta_{\mathrm{phys}}(T_{\mathrm{phys}})=\eta_{\mathrm{ref}}\exp\!\left[\frac{E_a}{R}\left(\frac{1}{T_{\mathrm{phys}}}-\frac{1}{T_{\mathrm{ref}}}\right)\right].3

with ηphys(Tphys)=ηrefexp ⁣[EaR(1Tphys1Tref)].\eta_{\mathrm{phys}}(T_{\mathrm{phys}})=\eta_{\mathrm{ref}}\exp\!\left[\frac{E_a}{R}\left(\frac{1}{T_{\mathrm{phys}}}-\frac{1}{T_{\mathrm{ref}}}\right)\right].4 the offset and ηphys(Tphys)=ηrefexp ⁣[EaR(1Tphys1Tref)].\eta_{\mathrm{phys}}(T_{\mathrm{phys}})=\eta_{\mathrm{ref}}\exp\!\left[\frac{E_a}{R}\left(\frac{1}{T_{\mathrm{phys}}}-\frac{1}{T_{\mathrm{ref}}}\right)\right].5 the dimensionless activation energy (Okuda et al., 22 Aug 2025).

A local Frank–Kamenetskii-parameter analog may be defined as

ηphys(Tphys)=ηrefexp ⁣[EaR(1Tphys1Tref)].\eta_{\mathrm{phys}}(T_{\mathrm{phys}})=\eta_{\mathrm{ref}}\exp\!\left[\frac{E_a}{R}\left(\frac{1}{T_{\mathrm{phys}}}-\frac{1}{T_{\mathrm{ref}}}\right)\right].6

which depends on ηphys(Tphys)=ηrefexp ⁣[EaR(1Tphys1Tref)].\eta_{\mathrm{phys}}(T_{\mathrm{phys}})=\eta_{\mathrm{ref}}\exp\!\left[\frac{E_a}{R}\left(\frac{1}{T_{\mathrm{phys}}}-\frac{1}{T_{\mathrm{ref}}}\right)\right].7, whereas the Frank–Kamenetskii version uses constant ηphys(Tphys)=ηrefexp ⁣[EaR(1Tphys1Tref)].\eta_{\mathrm{phys}}(T_{\mathrm{phys}})=\eta_{\mathrm{ref}}\exp\!\left[\frac{E_a}{R}\left(\frac{1}{T_{\mathrm{phys}}}-\frac{1}{T_{\mathrm{ref}}}\right)\right].8. In practice, the Frank–Kamenetskii law, ηphys(Tphys)=ηrefexp ⁣[EaR(1Tphys1Tref)].\eta_{\mathrm{phys}}(T_{\mathrm{phys}})=\eta_{\mathrm{ref}}\exp\!\left[\frac{E_a}{R}\left(\frac{1}{T_{\mathrm{phys}}}-\frac{1}{T_{\mathrm{ref}}}\right)\right].9, is the linearization of the Arrhenius law about TrefT_{\mathrm{ref}}0. The paper reports that regime boundaries between mobile, sluggish, and stagnant lid are only mildly shifted under the full Arrhenius law with modest TrefT_{\mathrm{ref}}1, and that mapping TrefT_{\mathrm{ref}}2 brings the two formulations into almost quantitative agreement (Okuda et al., 22 Aug 2025).

The comparison indicates that constant-TrefT_{\mathrm{ref}}3 rheology captures the essential three-regime behavior while simplifying the temperature dependence. This suggests that the main discrepancy between the two formulations lies not in the existence of the regimes themselves, but in slight shifts of regime-boundary location.

5. Role in convective regime classification

In the cited study, two-dimensional steady-state convective solutions with the Frank–Kamenetskii viscosity are obtained by the Newton method for different values of the Rayleigh number and of the strength of the dependence of the viscosity on temperature. Lid-regime classification is based on the surface-velocity mobility TrefT_{\mathrm{ref}}4, with the thresholds

  • TrefT_{\mathrm{ref}}5: mobile lid,
  • TrefT_{\mathrm{ref}}6: sluggish lid,
  • TrefT_{\mathrm{ref}}7: stagnant lid (Okuda et al., 22 Aug 2025).

As TrefT_{\mathrm{ref}}8 increases, or as the basal Rayleigh number TrefT_{\mathrm{ref}}9 decreases, the sequence is mobile regime ΔT\Delta T0 sluggish lid ΔT\Delta T1 stagnant lid. The sluggish lid regime is found between the mobile and stagnant lid regimes. It is characterized by a large viscosity contrast through the boundary layer below the conductive lid, rapid changes of lid thickness and Nusselt number with ΔT\Delta T2 at almost constant ΔT\Delta T3, and a peak in the effective viscosity contrast across the boundary layer. The summary further states that this regime is promoted by the stress-free top boundary and disappears under a rigid-top condition (Okuda et al., 22 Aug 2025).

Within this classification, Frank–Kamenetskii viscosity acts as the mechanism that sets how abruptly rheological resistance increases toward the cold upper boundary. A plausible implication is that the sluggish lid regime is not merely intermediate by definition, but is associated with a distinct boundary-layer structure rather than a smooth interpolation between mobile and stagnant limits.

6. Scaling behavior and instability

The Nusselt–Rayleigh scaling depends on both ΔT\Delta T4 and ΔT\Delta T5. At moderate ΔT\Delta T6 and moderate ΔT\Delta T7, corresponding to a weak lid, classical scaling ΔT\Delta T8 emerges, approximately the isoviscous limit. At high ΔT\Delta T9 or strong viscosity contrast, thin strong plumes dominate and one finds ηphysηrefexp ⁣[EaΔTRTref2θphys].\eta_{\mathrm{phys}}\simeq \eta_{\mathrm{ref}}\exp\!\left[-\frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}\,\theta_{\mathrm{phys}}\right].0 in both mobile and stagnant-lid regimes when rescaled by the convective-layer thickness. For most solutions in the mobile and stagnant lid regimes, the Nusselt number is proportional to the ηphysηrefexp ⁣[EaΔTRTref2θphys].\eta_{\mathrm{phys}}\simeq \eta_{\mathrm{ref}}\exp\!\left[-\frac{E_a\Delta T}{R\,T_{\mathrm{ref}}^2}\,\theta_{\mathrm{phys}}\right].1 power of the Rayleigh number, and the paper states that this can be derived by taking into account the effect of thin and strong downwelling plumes (Okuda et al., 22 Aug 2025).

Time-evolution calculations show that the steady solutions become unstable for large Rayleigh numbers, where additional downward plumes grow on the background convective flows. The stated explanation is that the timescale of the Rayleigh–Taylor instability for the thermal boundary layer between the conductive lid and the convective core becomes shorter than the timescale of horizontal advection by the background flow (Okuda et al., 22 Aug 2025).

These results place Frank–Kamenetskii viscosity at the center of both steady scaling and loss of steadiness. In the steady problem it determines whether boundary layers remain thick and symmetric or become thin with focused plumes; in the unsteady transition it conditions the thermal-boundary-layer structure on which plume-forming instability develops.

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