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Cryogenic fluid flows inside a 10-mm-diameter metal tube. The metal tube is enclosed by a concentric polypropylene tube with a diameter of \(15 \mathrm{~mm}\). The minimum temperature limit for polypropylene tube is \(-18^{\circ} \mathrm{C}\), specified by the ASME Code for Process Piping (ASME B31.3-2014, Table B-1). The gap between the concentric tubes is a vacuum. The inner metal tube and the outer polypropylene tube have emissivity values of \(0.5\) and \(0.97\), respectively. The concentric tubes are placed in a vacuum environment, where the temperature of the surroundings is \(0^{\circ} \mathrm{C}\). Determine the lowest temperature that the inner metal tube can go without cooling the polypropylene tube below its minimum temperature limit of $-18^{\circ} \mathrm{C}$. Assume both tubes have thin walls.

Short Answer

Expert verified
Answer: The lowest temperature that the inner metal tube can reach without cooling the polypropylene tube below its minimum temperature limit is approximately -38°C.

Step by step solution

01

Identify the variables needed for the radiative heat transfer equation

To calculate the radiative heat transfer between two concentric tubes, we need to know the area of the inner tube, the emissivity values of both tubes, their temperatures, and the Stefan-Boltzmann constant. Based on the information given, we have the following variables: - Diameter of inner metal tube (D1) = \(10 \mathrm{~mm}\) - Diameter of outer polypropylene tube (D2) = \(15 \mathrm{~mm}\) - Emissivity of metal tube (ε1) = \(0.5\) - Emissivity of polypropylene tube (ε2) = \(0.97\) - Minimum temperature of polypropylene tube (T2) = \(-18^{\circ} \mathrm{C}\) - Surrounding temperature (Ts) = \(0^{\circ} \mathrm{C}\) - Stefan-Boltzmann constant (σ) = \(5.67 \times 10^{-8} \mathrm{W / m^2K^4}\) Now we will convert the temperature values to Kelvin (K).
02

Convert temperatures to Kelvin

To convert temperatures from Celsius to Kelvin, we add 273.15 Minimum temperature of polypropylene tube in Kelvin (T2): \(T2 = -18 + 273.15 = 255.15 \mathrm{K}\) Surrounding temperature in Kelvin (Ts): \(Ts = 0 + 273.15 = 273.15 \mathrm{K}\)
03

Find the radiative heat transfer coefficient

The effective radiative heat transfer coefficient (hr) can be calculated using the following formula: \(hr = \frac{1 - \epsilon_1}{A_1(1 - \frac{D_1}{D_2})} + \frac{1}{\epsilon_1A_1} \bigg( \frac{\epsilon_2}{\epsilon_1} - 1 \bigg) \) Where \(A_1\) is the area of the first surface (inner metal tube) and can be calculated as: \(A_1 = \pi D_1 L\) Since we are not given the length (L) of the tubes, we can use the ratio of area to length (A1/L) in our formula: \(\frac{A_1}{L} = \pi D_1\) Now substituting the emissivity values, and diameters, our formula becomes: \(hr = \frac{1 - 0.5}{\pi (10 \times 10^{-3})(1 - \frac{10 \times 10^{-3}}{15 \times 10^{-3}})}+ \frac{1}{0.5\pi(10 \times 10^{-3})}\bigg(\frac{0.97}{0.5} - 1 \bigg)\) Calculate hr: \(hr \approx 28.076 \mathrm{W/m^2K}\)
04

Determine the lowest temperature of the inner metal tube without cooling the polypropylene tube below its minimum temperature limit

Now, we can use the radiative heat transfer equation: \(q = hr \times A_1 (T1^4 - T2^4)\) We want to find T1 when the heat transfer (q) between the concentric tubes is equal to the heat transfer from the polypropylene tube to its surroundings (T2). So we can write: \(q = hr \times A_1 ((T1^4 - Ts^4) - (T2^4 - Ts^4))\) Rearrange the formula for T1: \(T1^4 = \frac{q + hr \times A_1 (T2^4 - Ts^4)}{hr \times A_1} + Ts^4\) For our case, since the minimum temperature limit of the polypropylene tube is reached, the radiative heat transfer between the tubes is zero (q = 0): \(T1^4 = \frac{0 + hr \times A_1 (T2^4 - Ts^4)}{hr \times A_1} + Ts^4\) Substitute the known values and calculate T1: \(T1^4 = \frac{28.076 \times \pi (10 \times 10^{-3}) (255.15^4 - 273.15^4)}{28.076 \times \pi (10 \times 10^{-3})} + 273.15^4\) Solve for T1: \(T1 \approx 235.17 \mathrm{K}\) Now, convert T1 back to Celsius: \(T1 = 235.17 - 273.15\) \(T1 \approx -38^{\circ}\mathrm{C}\) Therefore, the lowest temperature that the inner metal tube can go without cooling the polypropylene tube below its minimum temperature limit is approximately \(-38^{\circ}\mathrm{C}\)

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Most popular questions from this chapter

The convection heat transfer coefficient for a clothed person while walking in still air at a velocity of \(0.5\) to \(2 \mathrm{~m} / \mathrm{s}\) is given by \(h=8.6 V^{0.53}\), where \(V\) is in \(\mathrm{m} / \mathrm{s}\) and \(h\) is in \(\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Plot the convection coefficient against the walking velocity, and compare the convection coefficients in that range to the average radiation coefficient of about $5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$.

A 5-m-diameter spherical furnace contains a mixture of \(\mathrm{CO}_{2}\) and \(\mathrm{N}_{2}\) gases at \(1200 \mathrm{~K}\) and \(1 \mathrm{~atm}\). The mole fraction of \(\mathrm{CO}_{2}\) in the mixture is \(0.15\). If the furnace wall is black and its temperature is to be maintained at \(600 \mathrm{~K}\), determine the net rate of radiation heat transfer between the gas mixture and the furnace walls.

Consider a person who is resting or doing light work. Is it fair to say that roughly one-third of the metabolic heat generated in the body is dissipated to the environment by convection, one-third by evaporation, and the remaining onethird by radiation?

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 a long semicylindrical duct of diameter \(1.0 \mathrm{~m}\). Heat is supplied from the base surface, which is black, at a rate of $1200 \mathrm{~W} / \mathrm{m}^{2}\(, while the side surface with an emissivity of \)0.4$ is maintained at \(650 \mathrm{~K}\). Neglecting the end effects, determine the temperature of the base surface.

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