Consider a stainless steel spoon \((k=15.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), \(\varepsilon=0.6\) ) that is partially immersed in boiling water at \(95^{\circ} \mathrm{C}\) in a kitchen at \(25^{\circ} \mathrm{C}\). The handle of the spoon has a cross section of about \(0.2 \mathrm{~cm} \times 1 \mathrm{~cm}\) and extends \(18 \mathrm{~cm}\) in the air from the free surface of the water. The spoon loses heat by convection to the ambient air with an average heat transfer coefficient of \(h=13 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) as well as by radiation to the surrounding surfaces at an average temperature of \(T_{\text {surr }}=\) \(295 \mathrm{~K}\). Assuming steady one- dimensional heat transfer along the spoon and taking the nodal spacing to be \(3 \mathrm{~cm}\), (a) obtain the finite difference formulation for all nodes, (b) determine the temperature of the tip of the spoon by solving those equations, and \((c)\) determine the rate of heat transfer from the exposed surfaces of the spoon.

Short Answer

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Answer: To find the temperature at the tip of the spoon and the rate of heat transfer, we first need to analyze the heat transfer along the stainless steel spoon, which is partially immersed in boiling water. The spoon loses heat through convection and radiation. Using the finite difference method to model the heat transfer and solving the system of equations, we can calculate the temperature at each node. The temperature at the tip of the spoon is the temperature at node 1 (T1). After calculating the temperatures, we can find the heat transfer rate from the exposed surfaces by summing up the conductive, convective, and radiative heat transfer components.

Step by step solution

01

Variables and Parameters

Define the variables and parameters for the problem, such as thermal conductivity (k), emissivity (ε), dimensions of the spoon, heat transfer coefficient (h), and the surrounding temperature (T_surr). - Thermal conductivity, k = 15.1 W/mK - Emissivity, ε = 0.6 - Cross-sectional area of the spoon handle, A = 0.2 cm * 1 cm = 0.2e-4 m² - Length of the spoon handle exposed to air, L = 18 cm = 0.18 m - Heat transfer coefficient, h = 13 W/m²K - Surrounding temperature, T_surr = 295 K
02

Finite Difference Formulation (Node Equations)

The heat transfer along the spoon handle can be solved using the finite difference method. Divide the handle into nodes with equal spacing of 3 cm. - Nodal spacing, Δx = 3 cm = 0.03 m For each node, we will write an energy balance, which gives us the finite difference equation. A general energy balance on the i-th node would look like: (Q_in)_i + (Q_out)_i = 0 The conductive heat transfer brings energy into the node and convective and radiative heat transfer removes energy. Write the energy balance on each node (from node 1 to node 6): - For node 1: `k * A * (T2-T1)/Δx - h * P * Δx * (T1-T_ambient) - ε * σ * A * (T1^4 - T_surr^4) = 0` - For nodes 2 to 5: `(Q_in)_i = k * A * (Ti-1 - Ti)/Δx` `(Q_out)_i = k * A * (Ti - Ti+1)/Δx + h * P * Δx * (Ti-T_ambient) + ε * σ * A * (Ti^4 - T_surr^4)` `(Q_in)_i + (Q_out)_i = 0` - For node 6 (in contact with boiling water): `(Q_in)_i = 0` `(Q_out)_i = k * A * (T6 - T5)/Δx + h * P * Δx * (T6-T_ambient) + ε * σ * A * (T6^4 - T_surr^4) + Q_bw` `(Q_in)_i + (Q_out)_i = 0` Where Q_bw is the heat transfer rate from the boiling water to node 6. Solve these equations to get the temperatures of each node.
03

Finding Temperatures at Nodes

We need to solve the system of equations from step 2 to find the temperatures at each node. This can be achieved using a variety of numerical methods, such as the Gauss-Seidel method or the Newton-Raphson method. The numerical method used should be able to deal with the non-linear nature of the radiative term (Ti^4 - T_surr^4). Once we have calculated the temperatures at all the nodes, we can determine the temperature at the tip of the spoon, which is the temperature at node 1 (T1).
04

Heat Transfer Rate

As we have the temperature of all nodes, we can use these values to compute the heat transfer rate from the exposed surfaces of the spoon. We will calculate conductive, convective, and radiative heat transfer components separately and then sum them. - Conductive heat transfer rate: `Q_cond = k * A * (T2 - T1)/Δx` - Convective heat transfer rate: `Q_conv = h * P * Δx * (T1 - T_ambient)` - Radiative heat transfer rate: `Q_rad = ε * σ * A * (T1^4 - T_surr^4)` Total Heat Transfer Rate (Q_total) = Q_cond + Q_conv + Q_rad We now have the temperature of the tip of the spoon (T1) and the rate of heat transfer from the exposed surfaces of the spoon (Q_total).

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Most popular questions from this chapter

The wall of a heat exchanger separates hot water at \(T_{A}=90^{\circ} \mathrm{C}\) from cold water at \(T_{B}=10^{\circ} \mathrm{C}\). To extend the heat transfer area, two-dimensional ridges are machined on the cold side of the wall, as shown in Fig. P5-76. This geometry causes non-uniform thermal stresses, which may become critical for crack initiation along the lines between two ridges. To predict thermal stresses, the temperature field inside the wall must be determined. Convection coefficients are high enough so that the surface temperature is equal to that of the water on each side of the wall. (a) Identify the smallest section of the wall that can be analyzed in order to find the temperature field in the whole wall. (b) For the domain found in part \((a)\), construct a twodimensional grid with \(\Delta x=\Delta y=5 \mathrm{~mm}\) and write the matrix equation \(A T=C\) (elements of matrices \(A\) and \(C\) must be numbers). Do not solve for \(T\). (c) A thermocouple mounted at point \(M\) reads \(46.9^{\circ} \mathrm{C}\). Determine the other unknown temperatures in the grid defined in part (b).

What causes the round-off error? What kind of calculations are most susceptible to round-off error?

A DC motor delivers mechanical power to a rotating stainless steel shaft ( \(k=15.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) with a length of \(25 \mathrm{~cm}\) and a diameter of \(25 \mathrm{~mm}\). The DC motor is in a surrounding with ambient air temperature of \(20^{\circ} \mathrm{C}\) and convection heat transfer coefficient of \(25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and the base temperature of the motor shaft is \(90^{\circ} \mathrm{C}\). Using a uniform nodal spacing of \(5 \mathrm{~cm}\) along the motor shaft, determine the finite difference equations and the nodal temperatures by solving those equations.

Consider one-dimensional transient heat conduction in a plane wall with variable heat generation and variable thermal conductivity. The nodal network of the medium consists of nodes 0,1 , and 2 with a uniform nodal spacing of \(\Delta x\). Using the energy balance approach, obtain the explicit finite difference formulation of this problem for the case of specified heat flux \(\dot{q}_{0}\) and convection at the left boundary (node 0 ) with a convection coefficient of \(h\) and ambient temperature of \(T_{\infty}\), and radiation at the right boundary (node 2 ) with an emissivity of \(\varepsilon\) and surrounding temperature of \(T_{\text {surr }}\).

Consider a nuclear fuel element \((k=57 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) that can be modeled as a plane wall with thickness of \(4 \mathrm{~cm}\). The fuel element generates \(3 \times 10^{7} \mathrm{~W} / \mathrm{m}^{3}\) of heat uniformly. Both side surfaces of the fuel element are cooled by liquid with temperature of \(80^{\circ} \mathrm{C}\) and convection heat transfer coefficient of \(8000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Using a uniform nodal spacing of \(8 \mathrm{~mm},(a)\) obtain the finite difference equations, \((b)\) determine the nodal temperatures by solving those equations, and (c) compare the surface temperatures of both sides of the fuel element with analytical solution.

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