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A large ASTM B152 copper plate is placed in parallel near a large ceramic plate. The ceramic plate is at a temperature of \(520^{\circ} \mathrm{C}\). The copper and ceramic plates have emissivity values of \(0.15\) and \(0.92\), respectively. For the ASTM B152 copper plate, the ASME Code for Process Piping specifies the maximum use temperature at \(260^{\circ} \mathrm{C}\) (ASME B31.3-2014, Table A-1M). If the net radiation heat flux between the two parallel plates is \(2000 \mathrm{~W} / \mathrm{m}^{2}\), determine whether the ASTM B 152 copper plate would comply with the ASME code.

Short Answer

Expert verified
Answer: No, the ASTM B152 copper plate does not comply with the ASME code under these conditions, as the calculated temperature of \(410.99^{\circ} \mathrm{C}\) is greater than the maximum use temperature specified by ASME code (\(260^{\circ} \mathrm{C}\)).

Step by step solution

01

Write down the formula for net radiation heat transfer between two parallel plates

We will use the following formula to calculate the net radiation heat flux between the two parallel plates: \[q = \sigma (e_A T_A^4 - e_B T_B^4)\] Where: \(q\) is the net radiation heat flux (\(\mathrm{W/m^2}\)) \(\sigma\) is the Stefan-Boltzmann constant (\(5.67 \times 10^{-8} \mathrm{W/(m^2 K^4)}\)) \(e_A\) and \(e_B\) are the emissivities of the two plates (dimensionless) \(T_A\) and \(T_B\) are the absolute temperatures of the two plates in Kelvin We will use this formula to find the temperature of the copper plate, \(T_A\).
02

Convert temperatures to Kelvin and insert the given data into the formula

First, we need to convert the temperature of the ceramic plate to Kelvin: \(520^{\circ} \mathrm{C} + 273.15 = 793.15 \mathrm{K}\) Now, insert the given data into the formula: \(2000 \mathrm{~W/m^2} = 5.67 \times 10^{-8} \mathrm{W/(m^2 K^4)} (0.15 \cdot T_A^4 - 0.92 \cdot (793.15 \mathrm{K})^4)\)
03

Solve the equation for the temperature of the copper plate, \(T_A\)

Rearrange the formula to solve for \(T_A\): \(T_A^4 = \frac{2000 \mathrm{~W/m^2} + 0.92 \cdot (793.15 \mathrm{K})^4 \times 5.67 \times 10^{-8} \mathrm{W/(m^2 K^4)}}{0.15 \times 5.67 \times 10^{-8} \mathrm{W/(m^2 K^4)}}\) Calculate the value of \(T_A^4\): \(T_A^4 = \frac{2000 + 0.92 \cdot (793.15)^4 \times 5.67 \times 10^{-8}}{0.15 \times 5.67 \times 10^{-8}} = 2.229 \times 10^9\) Now, find the temperature of the copper plate by taking the 4th root of the previous result: \(T_A = (2.229 \times 10^9)^{\frac{1}{4}} = 684.14 \mathrm{K}\)
04

Convert the temperature to Celsius and compare to ASME code's maximum use temperature

To determine if the copper plate complies with the ASME code, convert the temperature to Celsius and compare it to the maximum use temperature specified in the ASME code: \(684.14 \mathrm{K} - 273.15 = 410.99^{\circ} \mathrm{C}\) Since \(410.99 ^{\circ} \mathrm{C}\) is greater than the maximum use temperature specified by ASME code, which is \(260^{\circ} \mathrm{C}\), the ASTM B152 copper plate would not comply with the ASME code under these conditions.

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Most popular questions from this chapter

A row of tubes, equally spaced at a distance that is twice the diameter of the tubes, is positioned between two large parallel plates. The surface temperature of the tubes is constant at \(10^{\circ} \mathrm{C}\) and the top and bottom plates are at constant temperatures of \(100^{\circ} \mathrm{C}\) and \(350^{\circ} \mathrm{C}\), respectively. If the surfaces behave as blackbody, determine the net radiation heat flux leaving the bottom plate.

Two parallel concentric disks, \(20 \mathrm{~cm}\) and \(40 \mathrm{~cm}\) in diameter, are separated by a distance of \(10 \mathrm{~cm}\). The smaller disk \((\varepsilon=0.80)\) is at a temperature of \(300^{\circ} \mathrm{C}\). The larger disk \((\varepsilon=0.60)\) is at a temperature of $800^{\circ} \mathrm{C}$. (a) Calculate the radiation view factors. (b) Determine the rate of radiation heat exchange between the two disks. (c) Suppose that the space between the two disks is completely surrounded by a reflective surface. Estimate the rate of radiation heat exchange between the two disks.

The number of view factors that need to be evaluated directly for a 10 -surface enclosure is (a) 1 (b) 10 (c) 22 (d) 34 (e) 45

Two square plates, with the sides \(a\) and \(b\) (and \(b>a\) ), are coaxial and parallel to each other, as shown in Fig. P13-142, and they are separated by a center-to-center distance of \(L\). The radiation view factor from the smaller to the larger plate, \(F_{a b+}\) is given by $$ F_{a b}=\frac{1}{2 A}\left\\{\left[(B+A)^{2}+4\right]^{0.5}-\left[(B-A)^{2}+4\right]^{0.5}\right\\} $$ where, \(A=a / L\) and \(B=b / L\). (a) Calculate the view factors \(F_{a b}\) and \(F_{b a}\) for $a=20 \mathrm{~cm}\(, \)b=60 \mathrm{~cm}\(, and \)L=40 \mathrm{~cm}$. (b) Calculate the net rate of radiation heat exchange between the two plates described above if \(T_{a}=800^{\circ} \mathrm{C}\), $T_{b}=200^{\circ} \mathrm{C}, \varepsilon_{a}=0.8\(, and \)\varepsilon_{b}=0.4$. (c) A large, square plate (with the side $c=2.0 \mathrm{~m}, \varepsilon_{c}=0.1$, and negligible thickness) is inserted symmetrically between the two plates such that it is parallel to and equidistant from them. For the data given above, calculate the temperature of this third plate when steady operating conditions are established.

Consider an enclosure consisting of \(N\) diffuse and gray surfaces. The emissivity and temperature of each surface as well as the view factors between the surfaces are specified. Write a program to determine the net rate of radiation heat transfer for each surface.

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