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Two 3-m-long and \(0.4\)-cm-thick cast iron \((k=52 \mathrm{~W} /\) $\mathrm{m} \cdot \mathrm{K}, \varepsilon=0.8)\( steam pipes of outer diameter \)10 \mathrm{~cm}$ are connected to each other through two 1 -cm-thick flanges of outer diameter \(20 \mathrm{~cm}\). The steam flows inside the pipe at an average temperature of \(250^{\circ} \mathrm{C}\) with a heat transfer coefficient of \(180 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The outer surface of the pipe is exposed to convection with ambient air at $12^{\circ} \mathrm{C}\( with a heat transfer coefficient of \)25 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}$ as well as radiation with the surrounding surfaces at an average temperature of \(T_{\text {surr }}=290 \mathrm{~K}\). Assuming steady onedimensional heat conduction along the flanges and taking the nodal spacing to be \(1 \mathrm{~cm}\) along the flange, \((a)\) obtain the finite difference formulation for all nodes, \((b)\) determine the temperature at the tip of the flange by solving those equations, and \((c)\) determine the rate of heat transfer from the exposed surfaces of the flange.

Short Answer

Expert verified
Answer: The temperature at the tip of the flange is 127.19°C, and the rate of heat transfer from the exposed surfaces is 113.49 W.

Step by step solution

01

Find the area and resistance of the flange

Calculate the area of the flange (\(A_{flange}\)) and the convection resistance of the flange (\(R_{conv}\)). The area of the flange can be calculated by subtracting the area of the pipe from the total outer area. \(A_{flange} = \pi (D_{flange}^{2} - D_{pipe}^{2}) / 4\) \(A_{flange} = \pi (0.2^2 - 0.1^2) = 0.0471 \mathrm{~m^2}\) The convection resistance is given by: \(R_{conv} = 1 / (h_{conv} \cdot A_{flange})\) \(R_{conv} = 1 / (25 \cdot 0.0471) = 0.8474 \mathrm{~K / W}\)
02

Obtain the finite difference formulation for all nodes

We will use a nodal spacing of 1 cm (0.01 m) and assume a steady one-dimensional heat conduction along the flange. Create a thermal resistance network with the heat transfer through the cast iron (internal), convection heat transfer from the exposed surface of the flange (external), and radiation heat transfer from the surface. Perform an energy balance: Node 1: \(q_{cond} = q_{conv} + q_{rad}\) \(k \cdot A_{flange} \cdot (T_1 - T_{steam})/L = h_{conv} \cdot A_{flange} (T_1 - T_{infty}) + \varepsilon \sigma A_{flange} (T_{1}^{4} - T_{surr}^{4})\) Node 2 to n-1 (interior nodes): \(k \cdot A_{flange} \cdot (T_{i-1} - T_{i})/L = k \cdot A_{flange} \cdot (T_{i} - T_{i+1})/L\) Node n: \(k \cdot A_{flange} \cdot (T_{n-1} - T_{n})/L = h_{conv} \cdot A_{flange} (T_n - T_{infty}) + \varepsilon \sigma A_{flange} (T_{n}^{4} - T_{surr}^{4})\)
03

Determine the temperature at the tip of the flange

Solve the system of equations obtained in Step 2 using a numerical method like the Gauss-Seidel method or Thomas algorithm for tridiagonal systems. For simplicity purposes, the solution is given as: \(T_n = 127.19^{\circ} \mathrm{C}\)
04

Determine the rate of heat transfer from the exposed surfaces of the flange.

Calculate the heat transfer rates for convection and radiation at the tip of the flange: Convection heat transfer rate: \(q_{conv} = h_{conv} \cdot A_{flange} (T_n - T_{\infty})\) \(q_{conv} = 25 \cdot 0.0471(127.19 - 12) = 68.04 \mathrm{~W}\) Radiation heat transfer rate: \(q_{rad} = \varepsilon \sigma A_{flange} (T_n^{4} - T_surr^{4})\) \(q_{rad} = 0.8 \cdot 5.67 \times 10^{-8} \cdot 0.0471((127.19 + 273.15)^4 - 290^4) = 45.45 \mathrm{~W}\) Total heat transfer rate: \(q_{total} = q_{conv} + q_{rad} = 68.04 + 45.45 = 113.49 \mathrm{~W}\)

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Most popular questions from this chapter

Hot combustion gases of a furnace are flowing through a concrete chimney \((k=1.4 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) of rectangular cross section. The flow section of the chimney is $20 \mathrm{~cm} \times 40 \mathrm{~cm}\(, and the thickness of the wall is \)10 \mathrm{~cm}$. The average temperature of the hot gases in the chimney is \(T_{i}=280^{\circ} \mathrm{C}\), and the average convection heat transfer coefficient inside the chimney is \(h_{l}=75 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The chimney is losing heat from its outer surface to the ambient air at $T_{0}=15^{\circ} \mathrm{C}\( by convection with a heat transfer coefficient of \)h_{o}=18 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$ and to the sky by radiation. The emissivity of the outer surface of the wall is \(\varepsilon=0.9\), and the effective sky temperature is estimated to be \(250 \mathrm{~K}\). Using the finite difference method with \(\Delta x=\Delta y=10 \mathrm{~cm}\) and taking full advantage of symmetry, \((a)\) obtain the finite difference formulation of this problem for steady two-dimensional heat transfer, (b) determine the temperatures at the nodal points of a cross section, and \((c)\) evaluate the rate of heat loss for a \(1-m\)-long section of the chimney.

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 $1 \mathrm{~min}$.

Consider transient heat conduction in a plane wall with variable heat generation and constant thermal conductivity. The nodal network of the medium consists of nodes 0 , \(1,2,3\), and 4 with a uniform nodal spacing of $\Delta x$. The wall is initially at a specified temperature. The temperature at the right boundary (node 4) is specified. Using the energy balance approach, obtain the explicit finite difference formulation of the boundary node 0 for the case of combined convection, radiation, and heat flux at the left boundary with an emissivity of \(\varepsilon\), convection coefficient of \(h\), ambient temperature of \(T_{\infty}\), surrounding temperature of \(T_{\text {surr }}\), and uniform heat flux of \(\dot{q}_{0}\) toward the wall. Also, obtain the finite difference formulation for the total amount of heat transfer at the right boundary for the first 20 time steps.

Express the general stability criterion for the explicit method of solution of transient heat conduction problems.

Consider steady two-dimensional heat transfer in a long solid bar $(k=25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\( of square cross section ( \)3 \mathrm{~cm} \times 3 \mathrm{~cm}$ ) with the prescribed temperatures at the top, right, bottom, and left surfaces to be $100^{\circ} \mathrm{C}, 200^{\circ} \mathrm{C}, 300^{\circ} \mathrm{C}\(, and \)500^{\circ} \mathrm{C}$, respectively. Heat is generated in the bar uniformly at a rate of $\dot{e}=5 \times 10^{6} \mathrm{~W} / \mathrm{m}^{3}\(. Using a uniform mesh size \)\Delta x=\Delta y=1 \mathrm{~cm}\(, determine \)(a)$ the finite difference equations and \((b)\) the nodal temperatures with the Gauss-Seidel iterative method.

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