Fourier number (Fo) — Dimensionless time for unsteady heat conduction

Category: 熱解析 > 非定常熱伝導 | 更新 2026-04-12
Fourier number Fo visualization showing dimensionless time evolution of transient heat conduction temperature profiles
フーリエ数 Fo の増加に伴う非定常温度分布の時間発展。Fo が大きくなるにつれ初期温度分布の影響が消え、平衡状態に近づく。

Theory and Physics

Definition and Physical Meaning of Fourier Number

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Professor, what does the Fourier number mean? The symbol Fo suddenly appeared in the textbook, and I don't really understand...

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Simply put, the Fourier number is a dimensionless time representing "how far unsteady heat conduction has progressed". The defining equation is:

$$ \mathrm{Fo} = \frac{\alpha \, t}{L^2} $$
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Here, $\alpha$ is the thermal diffusivity [m²/s], $t$ is the elapsed time [s], and $L$ is the characteristic length (e.g., half the plate thickness, cylinder radius) [m].

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Is thermal diffusivity $\alpha$ different from thermal conductivity $k$?

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Good question. Thermal diffusivity is thermal conductivity divided by density and specific heat:

$$ \alpha = \frac{k}{\rho \, c_p} \quad \text{[m}^2\text{/s]} $$
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While thermal conductivity $k$ indicates "how easily heat is conducted," thermal diffusivity $\alpha$ represents "how quickly temperature changes propagate". Copper has a large $k$, so it conducts heat easily, but its $\rho c_p$ is also quite large. On the other hand, aluminum has a larger $\alpha$ than copper, so temperature changes actually propagate faster in aluminum.

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I see! So, does a larger Fourier number mean "heat has sufficiently spread"?

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Exactly. To use an analogy, right after entering a bath, only the surface is warm (Fo is small), but after soaking for a while, the core becomes warm (Fo is large). The Fourier number is an indicator of "how uniformly the temperature has equalized throughout the object".

Governing Equation for Unsteady Heat Conduction and Nondimensionalization

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Where does the Fourier number come from in the governing equation?

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Let's look at the one-dimensional unsteady heat conduction equation (no internal heat generation, isotropic, constant properties):

$$ \frac{\partial T}{\partial t} = \alpha \frac{\partial^2 T}{\partial x^2} $$
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Now, introduce dimensionless variables. Define temperature as $\theta = (T - T_\infty)/(T_i - T_\infty)$, position as $\xi = x/L$, and time as $\tau = \alpha t / L^2$. Then the governing equation becomes:

$$ \frac{\partial \theta}{\partial \tau} = \frac{\partial^2 \theta}{\partial \xi^2} $$
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As you can see, the dimensionless time $\tau$ is precisely the Fourier number $\mathrm{Fo}$. After nondimensionalization, all parameters related to material properties and dimensions disappear, meaning for the same Fo and the same boundary conditions, the dimensionless temperature distribution $\theta(\xi, \mathrm{Fo})$ will be the same regardless of material or size. This is the essence of the similarity principle.

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Wait, so you mean a 10 cm aluminum plate and a 1 m iron plate will have the same temperature distribution pattern if Fo is the same?

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If the boundary conditions are matched with the same Bi (Biot number), yes. That's exactly the idea used to create scaled experimental models and why universal charts like the Heisler chart are valid.

One-Term Approximation and the Meaning of Fo > 0.2

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The textbook says "if Fo > 0.2, the one-term approximation can be used." What does that mean?

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The analytical solution for unsteady heat conduction is generally expressed as an infinite series. For example, for an infinite plate with initial temperature $T_i$ suddenly exposed to an environment at $T_\infty$, the dimensionless temperature at the center is:

$$ \theta^* = \sum_{n=1}^{\infty} C_n \exp\!\left(-\zeta_n^2 \, \mathrm{Fo}\right) \cos(\zeta_n \xi) $$
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Here, $\zeta_n$ are eigenvalues determined from the Biot number. The exponential function $\exp(-\zeta_n^2 \, \mathrm{Fo})$ decays more rapidly for larger $n$. When Fo exceeds 0.2, all terms with $n \geq 2$ become less than 2% and can be ignored. So, keeping only the first term gives sufficient accuracy:

$$ \theta^* \approx C_1 \exp\!\left(-\zeta_1^2 \, \mathrm{Fo}\right) \cos(\zeta_1 \xi) \quad (\mathrm{Fo} > 0.2) $$
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It also said in the textbook that Fo > 0.2 is a condition for using the Heisler chart. That's for the same reason!

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Exactly. The Heisler chart is a graphical representation of the one-term approximation results, so it cannot be used in the region Fo < 0.2. If the initial short-time region is needed, you must sum many terms of the series or use the semi-infinite body solution.

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Concretely, how long does it take for Fo to become > 0.2?

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For example, for steel ($\alpha \approx 1.2 \times 10^{-5}$ m²/s) with a plate thickness of 20mm ($L = 10$ mm = 0.01 m):

$$ t = \frac{\mathrm{Fo} \cdot L^2}{\alpha} = \frac{0.2 \times (0.01)^2}{1.2 \times 10^{-5}} \approx 1.7 \;\text{seconds} $$
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For a 20mm steel plate, the one-term approximation becomes usable after about 1.7 seconds. On the other hand, for a 200mm concrete wall ($\alpha \approx 5 \times 10^{-7}$ m²/s, $L = 0.1$ m), $t \approx 4000$ seconds = over 1 hour. It varies by orders of magnitude depending on material and dimensions.

Relationship with Biot Number and Selection of Analysis Method

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Are the Fourier number and Biot number used together as a set?

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Exactly. When deciding the analysis method for an unsteady heat conduction problem, the Biot number Bi and Fourier number Fo are considered as a pair. The Biot number is:

$$ \mathrm{Bi} = \frac{h L}{k} $$
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where $h$ is the surface heat transfer coefficient, $L$ is the characteristic length, and $k$ is the solid's thermal conductivity. Bi represents the ratio of "internal thermal resistance of the solid" to "convective thermal resistance at the surface".

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If Bi is small, the lumped capacitance method can be used, right?

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Yes. If Bi < 0.1, the temperature gradient inside the object is negligible, so the entire object can be treated as having a uniform temperature—this is the Lumped Capacitance Method. In this case, the temperature change follows a simple exponential decay:

$$ \frac{T(t) - T_\infty}{T_i - T_\infty} = \exp\!\left(-\mathrm{Bi} \cdot \mathrm{Fo}\right) = \exp\!\left(-\frac{hA_s}{\rho c_p V}t\right) $$
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The decision flow in practice can be summarized as follows:

ConditionApplicable MethodExample
Bi < 0.1Lumped Capacitance Method (ODE)Quenching cooling of small metal parts
Bi ≥ 0.1, Fo > 0.2One-term approximation, Heisler chartCooling process of steel plate (mid to late stage)
Bi ≥ 0.1, Fo < 0.2Series solution (multiple terms) or semi-infinite approximationInitial response to thermal shock
Complex shape/boundary conditionsFEM / FDM numerical analysisTransient temperature distribution in an engine block
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So just by checking Bi and Fo, you can decide which solution method to use. That's very clear!

Coffee Break Trivia Corner

Origin of the Name "Fourier Number"

The Fourier number is named after the French mathematician and physicist Jean-Baptiste Joseph Fourier (1768-1830). In his 1822 work 'Théorie analytique de la chaleur' (The Analytical Theory of Heat), he established the analytical method for heat conduction using Fourier series. Ironically, he himself was sensitive to cold and believed "warmth is good for health," preferring to dress warmly even after returning from the Egyptian expedition. Fourier transform, Fourier series, Fourier's law, and the Fourier number—there aren't many scientists whose names are attached to so many concepts.

Physical Meaning of Each Term (Components of the Fourier Number)
  • Thermal diffusivity $\alpha = k/(\rho c_p)$ [m²/s]: Represents the propagation speed of temperature changes. It increases when $k$ is large (good heat conductor) and when $\rho c_p$ is small (easy to heat up). Aluminum ($\alpha \approx 9.7 \times 10^{-5}$) is about 8 times that of steel ($\approx 1.2 \times 10^{-5}$), so temperature changes propagate faster.
  • Elapsed time $t$ [s]: Time during which thermal diffusion progresses. Fo is proportional to time, so doubling the time doubles Fo.
  • Characteristic length $L$ [m]: Distance over which heat must diffuse. Fo is inversely proportional to $L^2$, so if the thickness is doubled, it takes four times as long to reach the same Fo. This is why heat treatment of large parts takes a long time.
How to Choose the Characteristic Length $L$
  • Infinite plate: $L =$ half the plate thickness (from symmetry plane to surface)
  • Infinite cylinder: $L = r_0$ (radius)
  • Sphere: $L = r_0$ (radius)
  • Lumped capacitance method: $L_c = V / A_s$ (volume / surface area, characteristic length)
  • Note: Use the same definition of $L$ for calculating Bi and Fo. Mixing them up leads to incorrect judgments.
Thermal Diffusivity of Representative Materials
Material$\alpha$ [m²/s]$k$ [W/(m·K)]$\rho c_p$ [MJ/(m³·K)]
Copper$1.17 \times 10^{-4}$4013.42
Aluminum$9.7 \times 10^{-5}$2372.44
Carbon steel$1.2 \times 10^{-5}$514.25
Stainless steel (SUS304)$3.9 \times 10^{-6}$153.85
Glass$3.4 \times 10^{-7}$0.782.29
Concrete$5.0 \times 10^{-7}$1.02.0
Water$1.4 \times 10^{-7}$0.604.18

Numerical Methods and Implementation

Element Fourier Number and Stability Condition for Explicit Methods

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Professor, does the Fourier number also appear in FEM unsteady thermal analysis?

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It does. In numerical analysis, the element Fourier number (mesh Fourier number) becomes important. Instead of the characteristic length $L$, we use the element size $\Delta x$, and instead of time $t$, we use the time step $\Delta t$:

$$ \mathrm{Fo}_e = \frac{\alpha \, \Delta t}{\Delta x^2} $$
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When using an explicit method (forward Euler method, forward difference method), the solution diverges unless $\mathrm{Fo}_e \leq 0.5$ (1D). This is the famous CFL condition for heat conduction. For 2D, it becomes $\mathrm{Fo}_e \leq 0.25$, and for 3D, $\mathrm{Fo}_e \leq 1/6$.

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So if we refine the mesh, we have to make the time step extremely small?

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Yes, for explicit methods, $\Delta t \leq \mathrm{Fo}_{e,\max} \cdot \Delta x^2 / \alpha$, so if the mesh size $\Delta x$ is halved, the allowable time step becomes one-fourth. The number of calculation steps doubles, so the total computational cost balloons to 8 times. This is the biggest weakness of explicit methods.

Guidelines for Setting Time Steps

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So how do you decide the time step in practice?

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A Fourier number-based approach is convenient. First, estimate the overall time scale of the analysis:

  • Characteristic time $t_c = L^2 / \alpha$ — an estimate of the time for temperature changes to propagate throughout the object.
  • Analysis end time — until it approaches steady state (Fo $\approx$ 1~2) or until the time of interest.

Next, guidelines for the time step:

Time SchemeElement Fo GuidelineNotes
Explicit method (forward difference)Foe ≤ 0.5 (mandatory)Stability limit. Exceeding it causes solution divergence.
Implicit method (backward difference)Foe = 1~10Unconditionally stable, but accuracy degrades if too large.
Crank-Nicolson methodFoe = 1~5Second-order accuracy. Prone to oscillations, so caution needed.
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With implicit methods, can Foe be as large as you want?

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In terms of stability, yes, but accuracy suffers. If the time step is too large, you miss capturing transient temperature changes. Especially when looking at the initial response to thermal shock, "automatic time step control" is standard practice: use a small $\Delta t$ for the first few steps, then increase it once the temperature change becomes gradual.

Choosing Between Implicit and Explicit Methods

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So, which one should we use in the end?

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For general unsteady heat conduction, implicit methods are overwhelmingly advantageous. The reason is simple: heat conduction is a diffusion-type equation, so the time scale is long. Explicit methods force you to use a very small $\Delta t$ for stability, but physically, temperature changes are slow, so using a larger $\Delta t$ with an implicit method is more efficient.

However, there are exceptions:

  • Ultra-short-time local heating like laser heating or plasma irradiation → Explicit methods are
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