/*! This file is auto-generated */ .wp-block-button__link{color:#fff;background-color:#32373c;border-radius:9999px;box-shadow:none;text-decoration:none;padding:calc(.667em + 2px) calc(1.333em + 2px);font-size:1.125em}.wp-block-file__button{background:#32373c;color:#fff;text-decoration:none} Problem 12 Sections of the trans-Alaska pip... [FREE SOLUTION] | 91Ó°ÊÓ

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Sections of the trans-Alaska pipeline run above the ground and ate supported by vertical steel shafts \((k=25\) W/m \(-\mathrm{K})\) that are \(1 \mathrm{~m}\) long and have a cross-sectional area of \(0.005 \mathrm{~m}^{2}\). Under normal cperating conditions, the temperature variation along the length of a shaft is known to be governed by an expression of the form $$ T=100-150 x+10 x^{2} $$ where \(T\) and \(x\) have units of \({ }^{\circ} \mathrm{C}\) and meters, respectively. Temperature variations are small over the shaft cross section. Evaluate the temperature and conduction heat rate at the shaft-pipeline joint \((x=0)\) and at the shaft-ground interface \((x=1 \mathrm{~m})\). Explain the difference in the heat rates.

Short Answer

Expert verified
At the joint: 100°C, 18.75 W; at the ground: -40°C, 16.25 W. Heat rate differs due to changing temperature gradient.

Step by step solution

01

Temperature at Shaft-Pipeline Joint

To find the temperature at the shaft-pipeline joint, substitute \(x = 0\) into the given temperature expression:\[ T = 100 - 150(0) + 10(0)^2 = 100^\circ \text{C} \] The temperature at the shaft-pipeline joint is 100°C.
02

Temperature at Shaft-Ground Interface

To find the temperature at the shaft-ground interface, substitute \(x = 1\) into the given expression:\[ T = 100 - 150(1) + 10(1)^2 = 100 - 150 + 10 = -40^\circ \text{C} \] The temperature at the shaft-ground interface is -40°C.
03

Calculate Temperature Gradient

To evaluate the conduction heat rate, calculate the temperature gradient \(\frac{dT}{dx}\). Differentiate the given temperature expression:\[ \frac{dT}{dx} = -150 + 2 \cdot 10x = -150 + 20x \]
04

Temperature Gradient at Shaft-Pipeline Joint

Substitute \(x = 0\) into the gradient obtained in Step 3:\[ \left(\frac{dT}{dx}\right)_{x=0} = -150 + 20(0) = -150 \text{ °C/m} \]
05

Temperature Gradient at Shaft-Ground Interface

Substitute \(x = 1\) into the gradient obtained in Step 3:\[ \left(\frac{dT}{dx}\right)_{x=1} = -150 + 20(1) = -130 \text{ °C/m} \]
06

Calculate Heat Rate at Shaft-Pipeline Joint

Use Fourier's Law, \(q = -kA \frac{dT}{dx}\), where \(k = 25\text{ W/m-K}\), and \(A = 0.005\text{ m}^2\) to find the heat rate:\[ q_{x=0} = -25 \cdot 0.005 \cdot (-150) = 18.75 \text{ W} \]
07

Calculate Heat Rate at Shaft-Ground Interface

Use Fourier's Law again with the gradient at \(x = 1\):\[ q_{x=1} = -25 \cdot 0.005 \cdot (-130) = 16.25 \text{ W} \]
08

Explanation of Heat Rate Difference

The difference in the heat rates is due to the change in temperature gradient along the length of the shaft. The gradient is more negative at the pipeline joint \((x=0)\), resulting in a higher heat flow rate compared to the ground interface \((x=1)\).

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Key Concepts

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

Fourier's Law
Fourier's Law is a fundamental principle of heat conduction. It states that the rate of heat transfer through a material is proportional to the negative of the temperature gradient and the cross-sectional area through which the heat flows. The formula for Fourier's Law is:
  • \( q = -k A \frac{dT}{dx} \)
Here, \( q \) is the heat conduction rate (W), \( k \) is the thermal conductivity of the material (W/m-K), \( A \) is the cross-sectional area (m²), and \( \frac{dT}{dx} \) is the temperature gradient (°C/m).
This law is critical in understanding how heat moves through materials and designing systems like cooling devices and heat exchangers.
In our exercise, Fourier's Law helps calculate the heat transferred from the pipeline to the ground via the steel shaft.
Temperature Gradient
The temperature gradient is the rate of change of temperature with respect to distance. In mathematical terms, it is the derivative of temperature \( T \) with respect to position \( x \), \( \frac{dT}{dx} \).
In the context of heat conduction, it tells us how quickly the temperature changes along the material. A higher gradient indicates a steeper change in temperature, leading to more significant heat transfer.
In our problem, you need to calculate the temperature gradient at two points on the shaft to understand the heat conduction rate. At \( x = 0 \), the gradient is steeper compared to \( x = 1 \), indicating more heat flow near the pipeline joint.
Conduction Heat Rate
Conduction heat rate is the amount of thermal energy transferred per unit time from one point to another within a material due to a temperature difference.
Using Fourier's Law, we calculate this rate:
  • For \( x = 0 \), the heat rate is found to be 18.75 W.
  • For \( x = 1 \), the heat rate reduces to 16.25 W.
This reduction demonstrates the dependency of the conduction heat rate on the temperature gradient.
It indicates how efficiently heat is being transferred through the steel shaft, providing insights for thermal insulation or heating system improvements in real-world applications.
Trans-Alaska Pipeline
The Trans-Alaska Pipeline is a major oil pipeline that runs through the state of Alaska. Due to extreme environmental conditions, parts of the pipeline are supported by steel shafts to prevent the oil from cooling and freezing.
The thermal conductivity of these steel shafts is crucial in regulating the temperature of the oil they transport. Engineers must carefully consider the heat conduction properties to maintain optimal temperatures.
The temperature changes along the shaft, impacting the heat flow rate, as observed in the given exercise.
This understanding ensures that the pipeline operates efficiently and safely, preventing blockages or potential hazards.
Differentiation in Thermodynamics
Differentiation is a mathematical tool used extensively in thermodynamics to analyze how a quantity changes with another, such as temperature with distance. It allows us to derive relationships and optimize systems for desired thermal performance.
In our exercise, differentiation helps determine the temperature gradient. By differentiating the temperature expression \( T = 100 - 150x + 10x^2 \), we find \( \frac{dT}{dx} = -150 + 20x \).
This equation lets us evaluate the gradient at different points along the shaft, essential for calculating the heat conduction rate using Fourier's Law.
This approach is central in heat transfer analysis, ensuring better system design and energy efficiency.

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Most popular questions from this chapter

A plane layer of coal of thickness \(L=1 \mathrm{~m}\) experiences uniform volumetric generation at a rate of \(\hat{q}=20 \mathrm{~W} / \mathrm{m}^{2}\) due to slow exidation of the coal particles. Averuged over a daily period, the top surface of the layer transfers heat by convection to ambient air for which \(h=5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and \(T_{\mathrm{m}}=25^{\circ} \mathrm{C}\), while receiving solar irrudiation in the amoent \(G_{5}=400 \mathrm{~W} / \mathrm{m}^{2}\). Irnatiation from the amosphere may be neglected. The solar absorptivity and emissivity of the surface are each \(\alpha_{S}=\varepsilon=0.95\). (a) Write the steady-sate form of the heat diffusion equation for the layer of coul. Verify that this equation is satisfied by a temperiture distribution of the form $$ T(x)=T_{x}+\frac{\dot{q} L^{2}}{2 k}\left(1-\frac{x^{2}}{L^{2}}\right) $$ From this distribution, what can you say about conditions at the bottom surface \((x=0)\) ? Sketch the temperature distribution and label key features. (b) Obtain an expression for the rate of heat transfer by conduction per unit area at \(x=L\). Applying an energy balance to a control surface about the top surface of the layer, obtain an expression for \(T_{r}\) Evaluate \(T_{4}\) and \(T(0)\) for the prescribed conditions. (c) Daily average values of \(G_{5}\) and \(h\) depend on a number of factors such as time of year, cloud cover, and wind conditions. For \(h=5 \mathrm{~W} / \mathrm{m}^{2}-\mathrm{K}\), compute and plot \(T_{\text {t and }} T(0)\) as a function of \(G_{5}\) for \(50 \leq G_{s} \leq 500 \mathrm{~W} / \mathrm{m}^{2}\). For \(G_{5}=400 \mathrm{~W} / \mathrm{m}^{2}\), compute and plot \(T_{\text {, and }} T(0)\) as a function of \(h\) for \(5 \leq h \leq 50 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\).

A spherical particle of radius \(r_{1}\) experiences uniform thermal generation at a rate of \(\dot{q}\). The particle is encapoulated by a spherical shell of cutside radius \(r_{2}\) that is cooled by ambient air. The thermal conductivities of the particle and shell are \(k_{1}\) and \(k_{2}\), respectively, where \(k_{1}=2 k_{2}\) (a) By applying the conservation of encrgy principle to spherical control volume \(A\), which is placed at an arbitrary location within the sphere, determine a relationship between the temperature gradient, \(d T / d r\), and the local radius, \(r\), for \(0 \leq r \leq r_{1}\). (b) By applying the conservation of energy principle to ppherical control volume \(B\), which is placed at an artitrary location within the spherical shell, determine a relationship between the temperature gradient, dT/Lr, and the local radius, \(r_{\text {, for }} r_{1} \leq r \leq r_{2}\). (c) On \(T-r\) coordinates, sketch the temperature distribution over the range \(0 \leq r \leq r_{2}\).

The steady-state temperature distribution in a onedimensional wall of thermal conductivity \(50 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) and thickness \(50 \mathrm{~mm}\) is observed to be \(T\left({ }^{\circ} \mathrm{C}\right)=a+b \mathrm{x}^{2}\). where \(a=200^{\circ} \mathrm{C}, b=-2000^{\circ} \mathrm{C} / \mathrm{m}^{2}\), and \(x\) is in meters. (a) What is the heat generation rate \(q\) in the wall? (b) Determine the heat fluxes at the two wall faces. In what manner are these heat fluxes related to the heat generation rate?

A spherical shell of inner and outer radii \(r_{\text {c and }} r_{e}\) ts spectively, contains heat-dissipating components, and at a particular instant the temperature distribution in the shell is known to be of the form $$ T(r)=\frac{C_{1}}{r}+C_{2} $$ Are conditions stendy-state or transient? How do the heat flux and heat rate vary with radius?

A young engineer is asked to design a themal protection barricr for a sensitive clectronic device that might be exposed to irradiation from a high- powered infrarcd laser. Having learmed as a student thut a low thermal conductivity material provides good insulating characteristics, the enginecr specifies use of a nanostructured aerogel, characterized by a thermal conductivity of \(k_{e}=\) 0.0ns W/m - \(\mathrm{K}\), for the protective harrier. The engineer's boss questions the wisdom of selecting the acrogel because it has a low themal conductivity. Consider the sudden laser irradiation of (a) peire aluminum, (b) glass, and (c) aerogel. The laser provides irradiation of \(G=10 \times 10^{6}\) Whm \({ }^{2}\). The absorptivities of the materials are \(a=0.2,0.9\), and \(0.8\) for the aluminum, glass, and acrogel, rerpectively, and the initial ternperature of the barrier is \(T_{i}=300 \mathrm{~K}\). Explain why the boss is concerncd. Hint: All materials experience thetmal expunsion (or contraction), and local stresses that develop within a material are, to a first approximation, proportional io the local temperahure gradicnt.

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