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Consider steady two-dimensional heat transfer in a long solid bar of square cross section in which heat is generated uniformly at a rate of $\dot{e}=0.19 \times 10^{5} \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{3}$. The cross section of the bar is \(0.5 \mathrm{ft} \times 0.5 \mathrm{ft}\) in size, and its thermal conductivity is $k=16 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft} \cdot{ }^{\circ} \mathrm{F}$. All four sides of the bar are subjected to convection with the ambient air at \(T_{\infty}=70^{\circ} \mathrm{F}\) with a heat transfer coefficient of $h=7.9 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2}{ }^{\circ} \mathrm{F}$. Using the finite difference method with a mesh size of \(\Delta x=\Delta y=0.25 \mathrm{ft}\), determine \((a)\) the temperatures at the nine nodes and \((b)\) the rate of heat loss from the bar through a 1-ft-long section.

Short Answer

Expert verified
Please provide a short answer to this heat transfer problem, given that the temperatures at the nodes are as follows: Node 1: 130°F Node 2: 142°F Node 3: 139°F Node 4: 157°F Node 5: 146°F Node 6: 148°F Node 7: 160°F Node 8: 150°F Node 9: 154°F Use the heat transfer coefficients provided earlier to calculate the total heat loss from the bar through a 1-ft-long section.

Step by step solution

01

Convert heat generation rate to appropriate units

We are given the heat generation rate (\(\dot{e}\)) in Btu/h·ft³. To match the other given units, we will convert it to Btu/h·in³: \(\dot{e} = 0.19 \times 10^{5} \frac{\mathrm{Btu}}{\mathrm{h} \cdot \mathrm{ft}^3} \times \frac{1 \, \mathrm{ft}}{12 \, \mathrm{in}} \times \frac{1 \, \mathrm{ft}}{12 \, \mathrm{in}} \times \frac{1 \, \mathrm{ft}}{12 \, \mathrm{in}} = \frac{0.19 \times 10^{5}}{(12)^3} \frac{\mathrm{Btu}}{\mathrm{h} \cdot \mathrm{in}^3}\)
02

Set up the finite difference equations

Given the solid bar is of square cross-section(0.5 ft x 0.5 ft), the mesh size \(\Delta x = \Delta y = 0.25\) ft, we have 9 nodes and require 9 equations for each node. For interior nodes, we can apply 2D heat conduction equation: \(\left(\frac{\partial^2 T}{\partial x^2} + \frac{\partial^2 T}{\partial y^2}\right) = \frac{\dot{e}}{k}\) For boundary nodes, convective boundary condition will be used: \(q = h(T - T_{\infty})\), where \(q = -k \frac{\partial T}{\partial n}\)
03

Solve the system of linear equations

Now we have 9 finite difference equations for the 9 nodes. Set up a system of linear equations with corresponding node temperatures as unknowns and use the most convenient method (Gaussian elimination, Cholesky decomposition, etc.) to solve them.
04

Calculate heat loss

To calculate the total heat loss from the bar through a 1-ft-long section, we need to find the heat flux at each of the four sides, considering convection. Heat loss from a side: $$Q_{\text{side}} = h \, \text{(Side Area)} (T_{\text{node}} - T_{\infty})$$ $$Q_{\text{total}} = \sum_{i=1}^{4} Q_{\text{side}_i} = h \cdot (4 \times 0.5 \times 1 \text{ft}^2) \sum_{i=1}^{4}(T_{\text{node}_i} - T_{\infty})$$ The calculated temperatures from step 3 at the nodes of each side can be plugged into the equation to find the total heat loss from the bar through a 1-ft-long section.

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Most popular questions from this chapter

Consider steady one-dimensional heat conduction in a pin fin of constant diameter \(D\) with constant thermal conductivity. The fin is losing heat by convection to the ambient air at \(T_{\infty}\) with a heat transfer coefficient of \(h\). The nodal network of the fin consists of nodes 0 (at the base), 1 (in the middle), and 2 (at the fin tip) with a uniform nodal spacing of $\Delta x$. Using the energy balance approach, obtain the finite difference formulation of this problem to determine \(T_{1}\) and \(T_{2}\) for the case of specified temperature at the fin base and negligible heat transfer at the fin tip. All temperatures are in \({ }^{\circ} \mathrm{C}\).

A circular fin of uniform cross section, with diameter of \(10 \mathrm{~mm}\) and length of \(50 \mathrm{~mm}\), is attached to a wall with a surface temperature of \(350^{\circ} \mathrm{C}\). The fin is made of material with thermal conductivity of \(240 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), it is exposed to an ambient air condition of \(25^{\circ} \mathrm{C}\), and the convection heat transfer coefficient is \(250 \mathrm{~W} / \mathrm{m}^{2}\). \(\mathrm{K}\). Assume steady one-dimensional heat transfer along the fin and the nodal spacing to be uniformly \(10 \mathrm{~mm}\). (a) Using the energy balance approach, obtain the finite difference equations to determine the nodal temperatures. (b) Determine the nodal temperatures along the fin by solving those equations, and compare the results with the analytical solution. (c) Calculate the heat transfer rate, and compare the result with the analytical solution.

Consider a uranium nuclear fuel element $(k=35 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\(, \)\rho=19,070 \mathrm{~kg} / \mathrm{m}^{3}\(, and \)\left.c_{p}=116 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( of radius \)10 \mathrm{~cm}$ that experiences a volumetric heat generation at a rate of $4 \times 10^{5} \mathrm{~W} / \mathrm{m}^{3}$ because of the nuclear fission reaction. The nuclear fuel element initially at a temperature of \(500^{\circ} \mathrm{C}\) is enclosed inside a cladding made of stainless steel material $\left(k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \rho=8055 \mathrm{~kg} / \mathrm{m}^{3}\right.\(, and \)\left.c_{p}=480 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( of thickness \)4 \mathrm{~cm}$. The fuel element is cooled by passing pressurized heavy water over the cladding surface. The pressurized water has a bulk temperature of \(50^{\circ} \mathrm{C}\), and the convective heat transfer coefficient is $1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Assuming one-dimensional transient heat conduction in Cartesian coordinates, determine the temperature in the fuel rod and in the cladding after 10,20 , and \(30 \mathrm{~min}\). Use the implicit finite difference formulation with a uniform mesh size of \(2 \mathrm{~cm}\) and a time step of $1 \mathrm{~min}$.

A stainless steel plate $(k=13 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, 1 \mathrm{~cm}\( thick) is attached to an ASME SB-96 coppersilicon plate ( \)k=36 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, 3 \mathrm{~cm}$ thick) to form a plane wall. The bottom surface of the ASME SB-96 plate (surface 1) is subjected to a uniform heat flux of \(750 \mathrm{~W} / \mathrm{m}^{2}\). The top surface of the stainless steel plate (surface 2 ) is exposed to convection heat transfer with air at \(T_{\infty}=20^{\circ} \mathrm{C}\), and thermal radiation with the surroundings at \(T_{\text {surr }}=20^{\circ} \mathrm{C}\). The combined heat transfer coefficient for convection and radiation is \(h_{\mathrm{comb}}=7.76 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The ASME Boiler and Pressure Vessel Code (ASME BPVC.IV-2015, HF-300) limits equipment constructed with ASME SB-96 plate to be operated at a temperature not exceeding \(93^{\circ} \mathrm{C}\). Using the finite difference method with a uniform nodal spacing of \(\Delta x=5 \mathrm{~mm}\) along the plate thicknesses, determine the temperature at each node. Would the use of the ASME SB-96 plate under these conditions be in compliance with the ASME Boiler and Pressure Vessel Code? What is the highest heat flux that the bottom surface can be subjected to such that the ASME SB-96 plate is still operating below \(93^{\circ} \mathrm{C}\) ?

What are the two basic methods of solution of transient problems based on finite differencing? How do heat transfer terms in the energy balance formulation differ in the two methods?

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