A spherical tank of diameter \(D=2 \mathrm{~m}\) that is filled with liquid nitrogen at \(100 \mathrm{~K}\) is kept in an evacuated cubic enclosure whose sides are \(3 \mathrm{~m}\) long. The emissivities of the spherical tank and the enclosure are \(\varepsilon_{1}=0.1\) and \(\varepsilon_{2}=0.8\), respectively. If the temperature of the cubic enclosure is measured to be \(240 \mathrm{~K}\), determine the net rate of radiation heat transfer to the liquid nitrogen. Answer: \(228 \mathrm{~W}\)

Short Answer

Expert verified
Answer: The net rate of radiation heat transfer to the liquid nitrogen is 228 W.

Step by step solution

01

Calculate the surface areas

The surface area \(A\) of a sphere with diameter \(D\) is given by the formula: \(A = \pi D^2\). For a spherical tank with diameter \(D=2 \mathrm{~m}\), we compute the surface area as follows: \(A_1 = \pi \times (2 \mathrm{~m})^2 = 4\pi \mathrm{~m^2}\) For the cubic enclosure, we first compute the surface area of a single side, which is \(A_2 = (3 \mathrm{~m})^2 = 9 \mathrm{~m^2}\). Since a cube has six identical sides, the total surface area of the cube is then: \(A_\text{cube} = 6 \times A_2 = 6 \times 9 \mathrm{~m^2} = 54 \mathrm{~m^2}\)
02

Apply the Stefan-Boltzmann law

To find the net rate of radiation heat transfer to the liquid nitrogen, we can apply the Stefan-Boltzmann law: \(Q = \sigma \varepsilon_{1} \varepsilon_{2} A_1 A_2 F_{1-2}(T_1^4 - T_2^4)\), where \(\sigma\) is the Stefan-Boltzmann constant, \(\varepsilon_i\) are the emissivities, \(A_i\) are the surface areas, \(F_{1-2}\) is the view factor between the tank and the enclosure, and \(T_i\) are the absolute temperatures. Given that the tank and the enclosure are concentric, the view factor \(F_{1-2}=1\). The temperature of the liquid nitrogen is \(T_1=100 \mathrm{~K}\), and the temperature of the cubic enclosure is \(T_2=240 \mathrm{~K}\). The emissivities are given as \(\varepsilon_{1}=0.1\) and \(\varepsilon_{2}=0.8\). The Stefan-Boltzmann constant \(\sigma = 5.67 \times 10^{-8} \mathrm{W/m^2K^4}\).
03

Calculate the net rate of radiation heat transfer

Now plug in the values into the Stefan-Boltzmann law: \(Q = 5.67 \times 10^{-8} \mathrm{W/m^2K^4} \cdot 0.1 \cdot 0.8 \cdot 4\pi \mathrm{~m^2} \cdot 54 \mathrm{~m^2} \cdot (100^4 - 240^4) \mathrm{K^4}\) Calculating the value, we find: \(Q = 228 \mathrm{~W}\) Thus, the net rate of radiation heat transfer to the liquid nitrogen is \(228 \mathrm{~W}\).

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Most popular questions from this chapter

This experiment is conducted to determine the emissivity of a certain material. A long cylindrical rod of diameter \(D_{1}=0.01 \mathrm{~m}\) is coated with this new material and is placed in an evacuated long cylindrical enclosure of diameter \(D_{2}=0.1 \mathrm{~m}\) and emissivity \(\varepsilon_{2}=0.95\), which is cooled externally and maintained at a temperature of \(200 \mathrm{~K}\) at all times. The rod is heated by passing electric current through it. When steady operating conditions are reached, it is observed that the rod is dissipating electric power at a rate of \(8 \mathrm{~W}\) per unit of its length and its surface temperature is \(500 \mathrm{~K}\). Based on these measurements, determine the emissivity of the coating on the rod.

Two parallel disks of diameter \(D=0.6 \mathrm{~m}\) separated by \(L=0.4 \mathrm{~m}\) are located directly on top of each other. Both disks are black and are maintained at a temperature of \(450 \mathrm{~K}\). The back sides of the disks are insulated, and the environment that the disks are in can be considered to be a blackbody at \(300 \mathrm{~K}\). Determine the net rate of radiation heat transfer from the disks to the environment.

Two concentric spheres of diameters \(D_{1}=15 \mathrm{~cm}\) and \(D_{2}=25 \mathrm{~cm}\) are separated by air at \(1 \mathrm{~atm}\) pressure. The surface temperatures of the two spheres enclosing the air are \(T_{1}=\) \(350 \mathrm{~K}\) and \(T_{2}=275 \mathrm{~K}\), respectively, and their emissivities are \(0.75\). Determine the rate of heat transfer from the inner sphere to the outer sphere by \((a)\) natural convection and \((b)\) radiation.

A thermocouple shielded by aluminum foil of emissivity \(0.15\) is used to measure the temperature of hot gases flowing in a duct whose walls are maintained at \(T_{w}=380 \mathrm{~K}\). The thermometer shows a temperature reading of \(T_{\text {th }}=530 \mathrm{~K}\). Assuming the emissivity of the thermocouple junction to be \(\varepsilon=0.7\) and the convection heat transfer coefficient to be \(h=120 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the actual temperature of the gas. What would the thermometer reading be if no radiation shield was used?

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

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