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91Ó°ÊÓ

Is there any limitation on the size of the time step \(\Delta t\) in the solution of transient heat conduction problems using (a) the explicit method and \((b)\) the implicit method?

Short Answer

Expert verified
Answer: In the explicit method, the time step size ∆t must follow the Courant-Friedrichs-Lewy (CFL) condition to maintain stability, which states that ∆t should not be greater than the ratio of the spatial step size squared (∆x²) to the thermal diffusivity (α): ∆t ≤ ∆x²/(4α). In the implicit method, there is no stability criterion or limit on the size of the time step ∆t, but an increased time step size may result in a loss of accuracy.

Step by step solution

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(a) Explicit method limitation

In the explicit method, the temperature at each point in the system is evaluated based on the temperatures of its neighboring points in the previous time step. The time step size in the explicit method has a stability criterion, often referred to as the Courant-Friedrichs-Lewy (CFL) condition. The CFL condition states that the time step size ∆t should not be greater than the ratio of the spatial step size squared (\(\Delta x^2\)) to the thermal diffusivity (\(\alpha\)): $$\Delta t \leq \frac{\Delta x^2}{4 \alpha}$$ If the time step size exceeds this limit, the explicit method may become unstable, leading to erroneous results.
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(b) Implicit method limitation

In the implicit method, the temperature at each point is updated simultaneously with the temperatures of its neighboring points. The implicit method is unconditionally stable, which means that there is no stability criterion or limit on the size of the time step ∆t for this method. However, increasing the time step size too much may lead to a loss in accuracy. Therefore, it is recommended to choose an appropriate value for the time step size depending on the specific problem and desired accuracy level.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Explicit Method
In the realm of transient heat conduction, the explicit method is often the straightforward approach. It calculates the temperature change at each point individually, relying on the known temperatures from the previous time step. This method is relatively simple to implement, making it attractive for educational purposes or straightforward problems.However, there's a catch known as the Courant-Friedrichs-Lewy (CFL) condition, which sets a limitation on the size of the time step (\( \Delta t \)). According to the CFL condition, for the explicit method to remain stable and produce correct results:
  • \(\Delta t \leq \frac{\Delta x^2}{4 \alpha}\)
Here, \(\Delta x\) is the spatial step size, and \(\alpha\) is the thermal diffusivity. When this condition is violated (i.e., when \(\Delta t\) exceeds this value), the results can become unstable or even erroneous. Thus, while using the explicit method, one must always ensure adherence to this stability requirement. It ensures that changes in temperature don't propagate too quickly, maintaining the fidelity of the simulation.
Implicit Method
The implicit method in transient heat conduction calculations takes a different approach. Unlike the explicit method, where calculations at each point rely heavily on information from the previous time step, the implicit method updates all points simultaneously. This method uses a form of the solution that considers future states, which inherently provides a distinct advantage in terms of stability.A standout feature of the implicit method is its unconditional stability. This means that:
  • There is no need for strict limitations on the size of \(\Delta t\).
Even if the time step is large, the implicit method can yield a stable solution. However, a large time step, while stable, can sometimes sacrifice accuracy. It's always a balancing act between computational speed (using larger time steps) and precision (keeping smaller time steps), especially in complex or precise simulations. Thus, for the implicit method, it is advised to opt for a time step that aligns with the accuracy needs of the problem at hand.
CFL Condition
The Courant-Friedrichs-Lewy (CFL) condition plays a vital role in ensuring stable and valid outcomes when using numerical methods such as the explicit method for transient heat conduction problems. It is essentially a convergence condition that relates the numerical stability of a method to the time step (\(\Delta t\)) and spatial step (\(\Delta x\)) sizes.This condition, quite famously expressed as:
  • \(\Delta t \leq \frac{\Delta x ^2}{4 \alpha}\)
guides the choice of \(\Delta t\) to prevent instability. If \(\Delta t\) becomes too large relative to \(\Delta x\), the numerical solution starts showing oscillations or incorrect behaviors, meaning the calculated temperatures don't accurately reflect the true heat conduction pattern.While primarily associated with the explicit method's stability, the CFL condition's core principle—that changes per time step should not be too abrupt—serves as a guideline even when constructing other numerical algorithms.
Stability Criterion
Numerical stability is crucial in simulations, particularly in transient heat conduction problems. The stability criterion provides a safety net, ensuring that computed results do not diverge over time, which occurs if calculations accumulate too much error at each step. For the explicit method, the stability criterion is intimately tied to the CFL condition, demanding smaller time steps to manage stability. A method is considered stable if, regardless of prolonged simulation duration, the errors do not grow uncontrollably. In the implicit method, though labelled as unconditionally stable, practical applications may still impose informal criteria. Excessively large time steps might lead to numerical errors that, while stable, can be inaccurate. Thus, achieving stability isn't merely about avoiding crashes or oscillations; it's about maintaining accuracy, working with realistic models, and achieving the desired precision over many iterations. Ultimately, the stability criterion ensures that we obtain a reliable map of how heat evolves within a material, enhancing our capability to predict and optimize real-world thermal processes.

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Most popular questions from this chapter

Explain how the finite difference form of a heat conduction problem is obtained by the energy balance method.

Starting with an energy balance on a volume element, obtain the two- dimensional transient explicit finite difference equation for a general interior node in rectangular coordinates for \(T(x, y, t)\) for the case of constant thermal conductivity and no heat generation.

Consider an aluminum alloy fin \((k=180 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) of triangular cross section whose length is \(L=5 \mathrm{~cm}\), base thickness is \(b=1 \mathrm{~cm}\), and width \(w\) in the direction normal to the plane of paper is very large. The base of the fin is maintained at a temperature of \(T_{0}=180^{\circ} \mathrm{C}\). The fin is losing heat by convection to the ambient air at \(T_{\infty}=25^{\circ} \mathrm{C}\) with a heat transfer coefficient of \(h=25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and by radiation to the surrounding surfaces at an average temperature of \(T_{\text {surr }}=290 \mathrm{~K}\). Using the finite difference method with six equally spaced nodes along the fin in the \(x\)-direction, determine \((a)\) the temperatures at the nodes and \((b)\) the rate of heat transfer from the fin for \(w=1 \mathrm{~m}\). Take the emissivity of the fin surface to be \(0.9\) and assume steady one-dimensional heat transfer in the fin.

Consider a long solid bar \((k=28 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) and \(\alpha=\) \(12 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}\) ) of square cross section that is initially at a uniform temperature of \(32^{\circ} \mathrm{C}\). The cross section of the bar is \(20 \mathrm{~cm} \times 20 \mathrm{~cm}\) in size, and heat is generated in it uniformly at a rate of \(\dot{e}=8 \times 10^{5} \mathrm{~W} / \mathrm{m}^{3}\). All four sides of the bar are subjected to convection to the ambient air at \(T_{\infty}=30^{\circ} \mathrm{C}\) with a heat transfer coefficient of \(h=45 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Using the explicit finite difference method with a mesh size of \(\Delta x=\Delta y=10 \mathrm{~cm}\), determine the centerline temperature of the bar \((a)\) after \(20 \mathrm{~min}\) and \((b)\) after steady conditions are established.

How does the finite difference formulation of a transient heat conduction problem differ from that of a steady heat conduction problem? What does the term \(\rho A \Delta x c_{p}\left(T_{m}^{i+1}-T_{m}^{i}\right) / \Delta t\) represent in the transient finite difference formulation?

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