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Steam at \(120^{\circ} \mathrm{C}\) is conuinuously passed through a \(50 \mathrm{~cm}\) long rubber tube of inner and outer radii \(1.0 \mathrm{~cm}\) and \(1.2 \mathrm{~cm}\). The room temperature is \(30^{\circ} \mathrm{C}\). Calculate the rate of heat flow through the walls of the tube. Thermal conductivity of rubber \(=0.15 . \mathrm{J} / \mathrm{m}-\mathrm{s}-{ }^{\circ} \mathrm{C}\).

Short Answer

Expert verified
The heat flow rate through the tube is approximately 2326.74 J/s.

Step by step solution

01

Understand the Setup

The problem describes a rubber tube through which steam is passed. The tube has an inner radius of \(1.0\, \text{cm}\) and an outer radius of \(1.2\, \text{cm}\), with a length of \(50\, \text{cm}\). The steam inside has a temperature of \(120^{\circ} \mathrm{C}\), while the outside temperature is \(30^{\circ} \mathrm{C}\). We are asked to find the rate of heat flow through the tube's walls.
02

Apply Fourier's Law of Heat Conduction for Cylinders

For a cylindrical shape, the heat transfer rate \(Q\) can be determined by the formula: \[Q = \frac{2\pi k L (T_1 - T_2)}{\ln(r_o / r_i)}\] where \(k\) is the thermal conductivity, \(L\) is the length of the cylinder, \(T_1\) and \(T_2\) are the temperatures, and \(r_o\), \(r_i\) are the outer and inner radii, respectively.
03

Convert Units to Meters and Insert Known Values

Convert the inner and outer radii from centimeters to meters: \[r_i = 0.01\, \text{m}, \quad r_o = 0.012\, \text{m}\]and the length,\[L = 0.5\, \text{m}\]Insert the known values into the formula: \[T_1 = 120^{\circ} \mathrm{C}, \quad T_2 = 30^{\circ} \mathrm{C}, \quad k = 0.15\, \text{J}/\text{m-s-}^{\circ}\text{C}\]
04

Calculate Natural Logarithm and Substitute into the Formula

Calculate the logarithmic term: \[\ln\left(\frac{r_o}{r_i}\right) = \ln\left(\frac{0.012}{0.01}\right)\]Compute to get\[\ln(1.2) \approx 0.1823\]
05

Calculate the Heat Transfer Rate

Substitute all values into the heat transfer formula:\[Q = \frac{2\pi \times 0.15 \times 0.5 \times (120 - 30)}{0.1823}\]Performing the calculations gives\[Q \approx \frac{135\pi}{0.1823} \approx 2326.74 \text{ J/s}\]
06

Conclusion

The rate of heat flow through the walls of the rubber tube is approximately \(2326.74\, \text{J/s}\).

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Thermal Conductivity
Thermal conductivity is a measure of a material's ability to conduct heat. It is an essential property that determines how quickly heat is transferred through a substance. Materials with high thermal conductivities, like metals, are excellent heat conductors, making them ideal for applications requiring quick heat dissipation. In contrast, materials with low thermal conductivities, such as rubber and other insulators, slow down heat transfer.

In the context of our exercise, the thermal conductivity of rubber is given as 0.15 J/m-s-°C. This value indicates how efficiently heat transfers through the rubber tube walls. A low value means that rubber is not a highly efficient conductor of heat, making it useful for applications where heat retention is desired.

To calculate the rate of heat transfer using thermal conductivity, we integrate it with other factors such as the temperature difference and the dimensions of the object (in this case, the cylindrical rubber tube). This requires us to apply specific formulas tailored to the object's shape, as we'll explore next when discussing Fourier's Law and cylindrical heat transfer.
Fourier's Law
Fourier's Law of heat conduction is fundamental in understanding how heat transfer works. It states that the heat transfer rate through a material is proportional to the negative gradient of temperatures and the area through which the heat flows. In simple terms, this law explains how temperature differences drive the flow of heat from hotter regions to cooler ones.

For the rubber tube in our example, Fourier's Law comes into play to calculate the precise rate of heat flow. This law is expressed mathematically for different shapes. In this exercise, we're considering a cylindrical object, which requires us to use a specific formula adapted from Fourier's Law:
  • For a simple flat surface: \(Q = k imes A imes (T_1 - T_2) / d\)
  • For a cylindrical surface: \(Q = \frac{2\pi k L (T_1 - T_2)}{\ln(r_o / r_i)}\)
Here, \(Q\) is the rate of heat transfer, \(k\) is the thermal conductivity, \(L\) is the length, \(T_1\) and \(T_2\) are temperatures on each side of the material, and \(r_o\) and \(r_i\) are the outer and inner radii of the cylinder, respectively. This formula allows us to consider the unique geometry of the cylinder in calculating heat transfer, showcasing the adaptability of Fourier's Law.
Cylindrical Heat Transfer
Cylindrical heat transfer deals with the calculation of heat flow through cylindrical shapes, which is common in engineering applications involving pipes and other tubular structures. Understanding this process is crucial since many industrial applications utilize cylindrical components.

For a cylinder, the specific geometry affects how heat flows through it. The formula used considers the cylinder's radial dimensions, meaning the radii from the center to the inner and outer surfaces are critical. In our example, the inner radius is 1.0 cm (converted to 0.01 m) and the outer radius is 1.2 cm (converted to 0.012 m).

The formula for heat flow through a cylinder, as adapted from Fourier's Law, includes a logarithmic term that accounts for the radial change:
  • \(Q = \frac{2\pi k L (T_1 - T_2)}{\ln(r_o / r_i)}\)
This calculation ensures an accurate representation of the heat transfer process through the cylindrical wall by considering the material's thermal conductivity and the temperature gradient. Using this formula, the problem in the exercise is solved to find the rate at which heat flows through the rubber tube, highlighting the importance of understanding both the material properties and the geometry of the object in heat transfer scenarios.

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Most popular questions from this chapter

A wall has two layers \(A\) and \(B\), each made of diffeent materials, The thickness of both the layers is the same. The thermal conductivity of \(A, K_{A}=3 K_{B^{*}}\) The temperature across the wall is \(20^{\circ} \mathrm{C}\). In thermal equilibrium (a) the temperature difference across \(A=150^{\circ} \mathrm{C}\) (b) rate of heat transfer across \(A\) is more than across \(B\) (c) rate of heat transfer across both is same (d) temperature difference across \(A\) is \(5^{\circ} \mathrm{C}\) :

Four identical rods \(\Lambda B, C D, C F\) and \(D E\) are joined as shown in figure. The length, cross sectional area and thermal conductivity of cach rod are \(l, \Lambda\) and \(K\) respectively. The ends \(\Lambda, E\) and \(F\) are maintained at temperature \(T_{1}\), \(T_{2}\) and \(T_{3}\) respectively. \(\Lambda\) ssuming no loss of heat to the aumosphere. Find the temperature at \(B\), the mid point of \(C D\).

A calorimeter contains a mixture of \(250 \mathrm{gm}\) of water and \(200 \mathrm{gm}\) of ice at \(0 \% \mathrm{C}\). The water cquivalent of the calorimcter is \(60 \mathrm{gm}\). Now \(300 \mathrm{~g}\) of steam at \(100^{\circ} \mathrm{C}\) is passed through this mixture, then calculate (a) the final temperature of the mixturc, (b) the amount of steam condensed, (c) the weight of the contents of the calorimeter, and (d) the amount of steam which remained uncondensed. (Latent heat of steam \(=536 \mathrm{cal} / \mathrm{gm}\) and I.atent heat of icc \(=80 \mathrm{cal} / \mathrm{gm}]\)

Therc are four vernicr scalcs; whosc specifications are given in column-I and the least count is given in Column-II \((S=\) valuc of main scale division, \(n=\) number of marks on vemicr) \begin{tabular}{l|l} Column-I & Column-II \end{tabular} (a) \(S=1 \mathrm{~mm}, n=10\) (p) \(0.05 \mathrm{~mm}\) (b) \(S=0.5 \mathrm{~mm}, n=10\) (q) \(0.01 \mathrm{~mm}\) (c) \(S=0.5 \mathrm{~mm}, n=20\) (r) \(0.1 \mathrm{~mm}\) (d) \(S=1 \mathrm{~mm}, n=100\) (s) \(0.025 \mathrm{~mm}\)

The space between two concentric spheres of radius \(R_{1}\) and \(R_{2}\) is filled with a uniform heat conducting material. Il's inner and outhcr surfaces are maintained at temperature \(T_{1}\) and \(T_{2} .\) Find the distance from the cenure where the tempcraure is \(\frac{T_{1}+T_{2}}{2}\).

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