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Consider a \(0.2-\mathrm{m}\)-diameter and \(1.8-\mathrm{m}\)-long horizontal cylinder in a room at \(20^{\circ} \mathrm{C}\). If the outer surface temperature of the cylinder is \(40^{\circ} \mathrm{C}\), the natural convection heat transfer coefficient is (a) \(2.9 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (b) \(3.5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (c) \(4.1 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (d) \(5.2 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (e) \(6.1 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\)

Short Answer

Expert verified
Question: A horizontal cylinder with a diameter of \(0.20\, \mathrm{m}\) and an outer surface temperature of \(40^{\circ}\mathrm{C}\) is in a room of temperature \(20^{\circ}\mathrm{C}\). Using the following properties of air: kinematic viscosity \((15.89 \times 10^{-6}\,\mathrm{m^2/s})\), thermal diffusivity \((2.22 \times 10^{-5}\,\mathrm{m^2/s})\), and thermal conductivity \((0.0257\, \mathrm{W/m\cdot K})\), calculate the natural convection heat transfer coefficient. Options: A) 1.47 W/m²·K B) 1.82 W/m²·K C) 2.19 W/m²·K D) 2.53 W/m²·K

Step by step solution

01

Calculate the temperature difference and temperature ratio

In order to find the Rayleigh number, we first need the temperature difference between the cylinder and the surrounding room. Since the cylinder's outer surface temperature is given as \(40^{\circ}\mathrm{C}\) and the room's temperature is given as \(20^{\circ}\mathrm{C}\), the temperature difference \(ΔT\) is: \(ΔT = 40 - 20 = 20 ^{\circ}\mathrm{C}\) Next, we need to calculate the average temperature between the cylinder surface and the room, which can be calculated as: \(T_{avg} = (T_{cylinder} + T_{room})/2 = (40 + 20) / 2 = 30^{\circ}\mathrm{C}\)
02

Calculate the Rayleigh Number, Prandtl Number, and Grashof Number

The Rayleigh Number can be calculated as the product of the Grashof Number and the Prandtl Number. We can find those numbers using the following formulas for a horizontal cylinder: \(Gr = \frac{g \cdot b \cdot D^3 \cdot ΔT}{ν^2}\) Here, \(g\) is the acceleration due to gravity \((9.81\, \mathrm{m/s^2})\), \(b\) is the thermal expansion coefficient \((1/T_{avg})\), \(D\) is the diameter of the cylinder \((0.2\, \mathrm{m})\), \(ΔT\) is the temperature difference \((20^{\circ}\mathrm{C})\), and \(ν\) is the kinematic viscosity \((15.89 \times 10^{-6}\,\mathrm{m^2/s})\). \(Pr = \frac{ν}{α}\) Here, \(α\) is the thermal diffusivity \((2.22 \times 10^{-5}\,\mathrm{m^2/s})\). Using these formulas, we can calculate the two numbers and then find the Rayleigh Number using: \(Ra = Gr \cdot Pr\) After calculating all the numbers, we can proceed to find the Nusselt number.
03

Determine the Nusselt Number

For a horizontal cylinder, we can use the following correlation to determine the Nusselt number: \(Nu = c_1 \cdot Ra^{c_2}\) \(c_1\) and \(c_2\) are constants depending on the geometry of the object; for a horizontal cylinder with the given conditions, they are \(c_1 = 0.60\) and \(c_2 = 0.25\). We can now use this formula to calculate the Nusselt Number with the Rayleigh Number calculated in Step 2.
04

Calculate the natural convection heat transfer coefficient

After calculating the Nusselt Number, we can find the natural convection heat transfer coefficient, \(h\), using the following formula: \(h = \frac{k \cdot Nu}{D}\) Here, \(k\) is the thermal conductivity \((0.0257\, \mathrm{W/m\cdot K})\) and \(D\) is the diameter of the cylinder \((0.2\, \mathrm{m})\). Now, we can plug in all the values and calculate the natural convection heat transfer coefficient. Then, compare the result with the given options to find the correct choice.

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Most popular questions from this chapter

A hot fluid $\left(k_{\text {fluid }}=0.72 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)$ is flowing as a laminar fully developed flow inside a pipe with an inner diameter of \(35 \mathrm{~mm}\) and a wall thickness of $5 \mathrm{~mm}\(. The pipe is \)10 \mathrm{~m}$ long, and the outer surface is exposed to air at \(10^{\circ} \mathrm{C}\). The average temperature difference between the hot fluid and the pipe inner surface is $\Delta T_{\text {avg }}=10^{\circ} \mathrm{C}$, and the inner and outer surface temperatures are constant. Determine the outer surface temperature of the pipe. Evaluate the air properties at \(50^{\circ} \mathrm{C}\). Is this a good assumption?

A solar collector consists of a horizontal aluminum tube of outer diameter $5 \mathrm{~cm}\( enclosed in a concentric thin glass tube of \)7 \mathrm{~cm}$ diameter. Water is heated as it flows through the aluminum tube, and the annular space between the aluminum and glass tubes is filled with air at $1 \mathrm{~atm}$ pressure. The pump circulating the water fails during a clear day, and the water temperature in the tube starts rising. The aluminum tube absorbs solar radiation at a rate of \(20 \mathrm{~W}\) per meter length, and the temperature of the ambient air outside is \(30^{\circ} \mathrm{C}\). Approximating the surfaces of the tube and the glass cover as being black (emissivity \(\varepsilon=1\) ) in radiation calculations and taking the effective sky temperature to be \(20^{\circ} \mathrm{C}\), determine the temperature of the aluminum tube when equilibrium is established (i.e., when the net heat loss from the tube by convection and radiation equals the amount of solar energy absorbed by the tube). For evaluation of air properties at $1 \mathrm{~atm}\( pressure, assume \)33^{\circ} \mathrm{C}$ for the surface temperature of the glass cover and \(45^{\circ} \mathrm{C}\) for the aluminum tube temperature. Are these good assumptions?

Consider a vertical plate with length \(L\), placed in quiescent air. If the film temperature is \(20^{\circ} \mathrm{C}\) and the average Nusselt number in natural convection is of the form \(\mathrm{Nu}=\mathrm{CRa}_{L}^{n}\), show that the average heat transfer coefficient can be expressed as $$ \begin{aligned} h &=1.51(\Delta T / L)^{1 / 4} \quad 10^{4}<\mathrm{Ra}_{L}<10^{9} \\ h &=1.19 \Delta T^{1 / 3} \quad 10^{10}<\mathrm{Ra}_{L}<10^{13} \end{aligned} $$

A \(50-\mathrm{cm} \times 50-\mathrm{cm}\) circuit board that contains 121 square chips on one side is to be cooled by combined natural convection and radiation by mounting it on a vertical surface in a room at $25^{\circ} \mathrm{C}\(. Each chip dissipates \)0.18 \mathrm{~W}$ of power, and the emissivity of the chip surfaces is 0.7. Assuming the heat transfer from the back side of the circuit board to be negligible, and the temperature of the surrounding surfaces to be the same as the air temperature of the room, determine the surface temperature of the chips. Evaluate air properties at a film temperature of \(30^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\) pressure. Is this a good assumption? Answer: \(36.2^{\circ} \mathrm{C}\)

A 6-m-internal-diameter spherical tank made of \(1.5\)-cm-thick stainless steel \((k=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) is used to store iced water at \(0^{\circ} \mathrm{C}\) in a room at \(20^{\circ} \mathrm{C}\). The walls of the room are also at \(20^{\circ} \mathrm{C}\). The outer surface of the tank is black (emissivity \(\varepsilon=1\) ), and heat transfer between the outer surface of the tank and the surroundings is by natural convection and radiation. Assuming the entire steel tank to be at \(0^{\circ} \mathrm{C}\) and thus the thermal resistance of the tank to be negligible, determine \((a)\) the rate of heat transfer to the iced water in the tank and \((b)\) the amount of ice at \(0^{\circ} \mathrm{C}\) that melts during a 24-h period. The heat of fusion of water is \(333.7 \mathrm{~kJ} / \mathrm{kg}\). Answers: (a) $15.4 \mathrm{~kW}\(, (b) \)3988 \mathrm{~kg}$

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