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Consider a small hot metal object of mass \(m\) and specific heat \(c\) that is initially at a temperature of \(T_{i}\). Now the object is allowed to cool in an environment at \(T_{\infty}\) by convection with a heat transfer coefficient of \(h\). The temperature of the metal object is observed to vary uniformly with time during cooling. Writing an energy balance on the entire metal object, derive the differential equation that describes the variation of temperature of the ball with time, \(T(t)\). Assume constant thermal conductivity and no heat generation in the object. Do not solve.

Short Answer

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Question: Derive a differential equation for the temperature variation of a hot metal object with mass \(m\), specific heat \(c\), initial temperature \(T_{i}\), environmental temperature \(T_{\infty}\), and heat transfer coefficient \(h\) as it cools down in an environment. Answer: The temperature variation of the hot metal object with time can be described by the following differential equation: $$ \frac{dT(t)}{dt} = -\frac{hA}{mc}(T(t) - T_{\infty}) $$

Step by step solution

01

Define the given parameters and properties

We are given the mass of the hot metal object \(m\), its specific heat \(c\), the initial temperature \(T_{i}\), the environmental temperature \(T_{\infty}\), and the heat transfer coefficient \(h\). We want to find an expression for the temperature \(T(t)\) of the object at any time \(t\).
02

Set up the energy balance equation

The amount of heat energy gained by an environment is equal to the amount of heat energy lost by the hot metal object. The rate of heat transfer is proportional to the temperature difference between the object and the environment and it depends on the heat transfer coefficient \(h\). Therefore, the rate of heat transfer can be written as: $$ -\frac{dQ}{dt} = hA(T(t) - T_{\infty}) $$ where \(A\) is the surface area of the hot metal object and \(-\frac{dQ}{dt}\) denotes the rate of heat transfer (with negative sign indicating loss of heat).
03

Find the heat capacity of the object and its connection to temperature

The heat capacity of the hot metal object is defined as the product of its mass and specific heat: $$ C = mc $$ The amount of heat energy stored in the hot metal object at any given time t can be related to its temperature using the heat capacity: $$ Q(t) = C(T(t) - T_{\infty}) $$
04

Differentiate the heat energy stored in the object with respect to time

To establish a connection between the heat flow rate and temperature changes, we need to differentiate the above equation with respect to time: $$ \frac{dQ}{dt} = C\frac{dT(t)}{dt} $$
05

Combine both expressions involving the rate of heat transfer and derived differential equation

Now, we equate the above differential equation expression with the expression for the rate of heat transfer: $$ -C\frac{dT(t)}{dt} = hA(T(t) - T_{\infty}) $$
06

Simplify the differential equation

Finally, we can write the differential equation describing the temperature variation of the object with time as: $$ \frac{dT(t)}{dt} = -\frac{hA}{mc}(T(t) - T_{\infty}) $$ Thus, we have derived the differential equation for the temperature of the metal object as a function of time.

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Most popular questions from this chapter

The variation of temperature in a plane wall is determined to be $T(x)=110 x-48 x\( where \)x\( is in \)\mathrm{m}\( and \)T\( is in \){ }^{\circ} \mathrm{C}$. If the thickness of the wall is \(0.75 \mathrm{~m}\), the temperature difference between the inner and outer surfaces of the wall is (a) \(110^{\circ} \mathrm{C}\) (b) \(74^{\circ} \mathrm{C}\) (c) \(55^{\circ} \mathrm{C}\) (d) \(36^{\circ} \mathrm{C}\) (e) \(18^{\circ} \mathrm{C}\)

Consider a 20-cm-thick large concrete plane wall $(k=0.77 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})$ subjected to convection on both sides with \(T_{\infty 1}=22^{\circ} \mathrm{C}\) and $h_{1}=8 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\( on the inside and \)T_{\infty 22}=8^{\circ} \mathrm{C}$ and \(h_{2}=12 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) on the outside. Assuming constant thermal conductivity with no heat generation and negligible radiation, \((a)\) express the differential equations and the boundary conditions for steady one-dimensional heat conduction through the wall, (b) obtain a relation for the variation of temperature in the wall by solving the differential equation, and \((c)\) evaluate the temperatures at the inner and outer surfaces of the wall.

Consider a large plane wall of thickness \(L=0.4 \mathrm{~m}\), thermal conductivity \(k=2.3 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and surface area \(A=30 \mathrm{~m}^{2}\). The left side of the wall is maintained at a constant temperature of \(T_{1}=90^{\circ} \mathrm{C}\), while the right side loses heat by convection to the surrounding air at $T_{\infty}=25^{\circ} \mathrm{C}\( with a heat transfer coefficient of \)h=24 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Assuming constant thermal conductivity and no heat generation in the wall, \((a)\) express the differential equation and the boundary conditions for steady one-dimensional heat conduction through the wall, (b) obtain a relation for the variation of temperature in the wall by solving the differential equation, and (c) evaluate the rate of heat transfer through the wall.

A large plane wall has a thickness \(L=50 \mathrm{~cm}\) and thermal conductivity \(k=25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). On the left surface \((x=0)\), it is subjected to a uniform heat flux \(\dot{q}_{0}\) while the surface temperature \(T_{0}\) is constant. On the right surface, it experiences convection and radiation heat transfer while the surface temperature is \(T_{L}=225^{\circ} \mathrm{C}\) and the surrounding temperature is \(25^{\circ} \mathrm{C}\). The emissivity and the convection heat transfer coefficient on the right surface are \(0.7\) and $15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, respectively. (a) Show that the variation of temperature in the wall can be expressed as $T(x)=\left(\dot{q}_{0} / k\right)(L-x)+T_{L},(b)\( calculate the heat flux \)\dot{q}_{0}$ on the left face of the wall, and (c) determine the temperature of the left surface of the wall at \(x=0\).

A metal spherical tank is filled with chemicals undergoing an exothermic reaction. The reaction provides a uniform heat flux on the inner surface of the tank. The tank has an inner diameter of \(5 \mathrm{~m}\), and its wall thickness is \(10 \mathrm{~mm}\). The tank wall has a variable thermal conductivity given as \(k(T)=k_{0}(1+\beta T)\), where $k_{0}=9.1 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \beta=0.0018 \mathrm{~K}^{-1}\(, and \)T$ is in \(\mathrm{K}\). The area surrounding the tank has an ambient temperature of \(15^{\circ} \mathrm{C}\), the tank's outer surface experiences convection heat transfer with a coefficient of \(80 \mathrm{~W} / \mathrm{m}^{2}, \mathrm{~K}\). Determine the heat flux on the tank's inner surface if the inner surface temperature is \(120^{\circ} \mathrm{C}\).

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