Warning: foreach() argument must be of type array|object, bool given in /var/www/html/web/app/themes/studypress-core-theme/template-parts/header/mobile-offcanvas.php on line 20

A composite wall is made of stainless steel $\left(k_{1}=13 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \quad 30 \mathrm{~mm}\right.$ thick), concrete $\left(k_{2}=1.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, 30 \mathrm{~mm}\right.\( thick \))\(, and nonmetal \)\left(k_{3}=0.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right.\(, \)15 \mathrm{~mm}$ thick) plates. The concrete plate is sandwiched between the stainless steel plate at the bottom and the nonmetal plate at the top. A series of ASTM B21 naval brass bolts are bolted to the nonmetal plate, and the upper surface of the plate is exposed to convection heat transfer with air at \(20^{\circ} \mathrm{C}\) and $h=20 \mathrm{~W} / \mathrm{m}^{2}$.K. At the bottom surface, the stainless steel plate is subjected to a uniform heat flux of $2000 \mathrm{~W} / \mathrm{m}^{2}$. The ASME Code for Process Piping (ASME B31.3-2014, Table A-2M) limits the maximum use temperature for the ASTM B21 bolts to \(149^{\circ} \mathrm{C}\). Using the finite difference method with a uniform nodal spacing of \(\Delta x_{1}=10 \mathrm{~mm}\) for the stainless steel and concrete plates, and \(\Delta x_{2}=5 \mathrm{~mm}\) for the nonmetal plate, determine the temperature at each node. Plot the temperature distribution as a function of \(x\) along the plate thicknesses. Would the ASTM B21 bolts in the nonmetal plate comply with the ASME code?

Short Answer

Expert verified
Question: Determine if the ASTM B21 bolts used in the nonmetal plate of a composite wall comply with the ASME code, which sets a limit for the maximum use temperature. Given the boundary conditions, use the finite difference method to find the temperature distribution along the composite wall made of stainless steel, concrete, and nonmetal plates.

Step by step solution

01

Identify the boundary conditions

The problem states that the bottom surface of the stainless steel plate is subjected to a uniform heat flux of 2000 W/m^2, and the upper surface of the nonmetal plate is exposed to convection heat transfer with air at 20°C and h=20 W/m^2.K.
02

Set up finite difference equations

Start by labeling the nodes in each section of the composite wall. Since we have three plates, we will have three separate equations representing each layer: - Nodes in Stainless Steel: \(T_{1,1}, T_{1,2}, T_{1,3}\) - Nodes in Concrete: \(T_{2,1}, T_{2,2}, T_{2,3}\) - Nodes in Nonmetal: \(T_{3,1}, T_{3,2}, T_{3,3}\) Apply the finite difference method to set up the equations for each node. They will help us create a system of linear equations, which can be solved for the temperature at each node.
03

Solve for temperatures

After setting up the equations, solve for the temperatures at each node using techniques like the Gaussian elimination method or any other method that is preferred for solving a system of linear equations.
04

Plot the temperature distribution

Once the temperatures at the nodes are found, create a plot that represents the temperature distribution along the thicknesses of each layer. This will visually aid in analyzing the temperature distribution along the composite wall.
05

Compare with ASME code

Check the temperature at the node corresponding to the position of the ASTM B21 bolts in the nonmetal plate. Compare this temperature to the maximum limit provided by the ASME code (\(149^{\circ} \mathrm{C}\)). If the temperature is less than or equal to the limit, then the ASTM B21 bolts comply with the ASME code. By following these steps, you can determine the temperature distribution along the composite wall and verify if the ASTM B21 bolts comply with the ASME code.

Unlock Step-by-Step Solutions & Ace Your Exams!

  • Full Textbook Solutions

    Get detailed explanations and key concepts

  • Unlimited Al creation

    Al flashcards, explanations, exams and more...

  • Ads-free access

    To over 500 millions flashcards

  • Money-back guarantee

    We refund you if you fail your exam.

Over 30 million students worldwide already upgrade their learning with Vaia!

One App. One Place for Learning.

All the tools & learning materials you need for study success - in one app.

Get started for free

Most popular questions from this chapter

Consider steady one-dimensional heat conduction in a plane wall with variable heat generation and constant thermal conductivity. The nodal network of the medium consists of nodes \(0,1,2,3,4\), and 5 with a uniform nodal spacing of \(\Delta x\). Using the energy balance approach, obtain the finite difference formulation of the boundary nodes for the case of insulation at the left boundary (node 0 ) and radiation at the right boundary (node 5) with an emissivity of \(\varepsilon\) and surrounding temperature of \(T_{\text {carr }}\)

Consider a 2-m-long and \(0.7-\mathrm{m}\)-wide stainless steel plate whose thickness is \(0.1 \mathrm{~m}\). The left surface of the plate is exposed to a uniform heat flux of \(2000 \mathrm{~W} / \mathrm{m}^{2}\), while the right surface of the plate is exposed to a convective environment at $0^{\circ} \mathrm{C}\( with \)h=400 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. The thermal conductivity of the stainless steel plate can be assumed to vary linearly with temperature range as \(k(T)=k_{o}(1+\beta T)\) where $k_{o}=48 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\( and \)\beta=9.21 \times 10^{-4 \circ} \mathrm{C}^{-1}$. The stainless steel plate experiences a uniform volumetric heat generation at a rate of $8 \times 10^{5} \mathrm{~W} / \mathrm{m}^{3}$. Assuming steady-state one-dimensional heat transfer, determine the temperature distribution along the plate thickness.

Consider transient one-dimensional heat conduction in a plane wall that is to be solved by the explicit method. If both sides of the wall are at specified temperatures, express the stability criterion for this problem in its simplest form.

How can a node on an insulated boundary be treated as an interior node in the finite difference formulation of a plane wall? Explain.

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 \(T_{\text {sarr }}=290 \mathrm{~K}\). 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 onedimensional heat transfer in the fin. Answers: (a) \(177.0^{\circ} \mathrm{C}\), $174.1^{\circ} \mathrm{C}, 171.2^{\circ} \mathrm{C}, 168.4^{\circ} \mathrm{C}, 165.5^{\circ} \mathrm{C} ;\( (b) \)537 \mathrm{~W}$

See all solutions

Recommended explanations on Physics Textbooks

View all explanations

What do you think about this solution?

We value your feedback to improve our textbook solutions.

Study anywhere. Anytime. Across all devices.

Sign-up for free