/*! 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 57 A hollow aluminem sphere, with a... [FREE SOLUTION] | 91Ó°ÊÓ

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A hollow aluminem sphere, with an clectrical heater in the center, is used in tests to determine the thermal conductivity of insulating materials. The inner and outer radii of the sphere are \(0.15\) and \(0.18 \mathrm{~m}\), respectively. and testing is done under steady-state conditions with the inner surface of the aluminum maintained at \(250^{\circ} \mathrm{C}\). In a particular test, a spherical shell of insulation is cast on the outer surface of the sphere to a thickness of \(0.12 \mathrm{~m}\). The system is in a roorn for which the air temperature is \(20^{\circ} \mathrm{C}\) and the convection cocfficient at the outer surface of the insulation is \(30 \mathrm{~W} / \mathrm{m}^{2}+\mathrm{K}\). If \(80 \mathrm{~W}\) are dissipated by the heater under steady-state conditions, what is the thermal conductivity of the insulation?

Short Answer

Expert verified
The thermal conductivity of the insulation is approximately 0.033 W/m·K.

Step by step solution

01

Identify Known Values

Start by noting down the known values:- Inner radius of the aluminum sphere, \( r_1 = 0.15 \) m.- Outer radius of the aluminum sphere, \( r_2 = 0.18 \) m.- Thickness of the insulation, \( \delta = 0.12 \) m, therefore outer radius of insulation, \( r_3 = 0.18 + 0.12 = 0.30 \) m.- Inner surface temperature, \( T_1 = 250^{\circ} \text{C} \).- Air temperature, \( T_∞ = 20^{\circ} \text{C} \).- Convective heat transfer coefficient, \( h = 30 \, \text{W/m}^2\cdot\text{K} \).- Heat dissipation, \( Q = 80 \, \text{W} \).
02

Understand the Heat Transfer Process

The problem involves conductive and convective heat transfer. The heat generated by the heater is conducted through the aluminum and the insulation to the outer surface, where it is then convected to the surrounding air.
03

Write the Heat Transfer Equation

Under steady-state conditions, the heat dissipation through conduction through the insulation can be given by:\[ Q = \frac{4\pi k(T_1 - T_2)}{\frac{1}{r_2} - \frac{1}{r_3}} \]where:- \( k \) is the thermal conductivity of the insulation.- \( T_2 \) is the temperature at the outer surface of the insulation.
04

Express the Temperature at the Outer Surface Due to Convection

The convective heat transfer at the outer surface can be expressed as:\[ Q = h \cdot 4\pi r_3^2 (T_2 - T_∞) \]
05

Equate Heat Transfer Rates

Since the heat transfer rate through conduction and convection must be equal at the interface, set the conduction and convection expressions equal:\[ \frac{4\pi k(T_1 - T_2)}{\frac{1}{r_2} - \frac{1}{r_3}} = h \cdot 4\pi r_3^2 (T_2 - T_∞) \]
06

Solve for Thermal Conductivity (k)

Rearrange the equation to solve for \( k \):\[ k = \frac{h r_3^2 (T_2 - T_∞) \cdot (\frac{1}{r_2} - \frac{1}{r_3})}{(T_1 - T_2)} \]Substitute \( T_2 \) back from the equation above to find \( k \), using the fact that \( Q = 80 \, W \) and solve for \( k \).
07

Compute Numerical Value

Substitute the known values into the final expression to calculate the thermal conductivity value. This should include:- \( T_1 = 250^{\circ}C \), \( T_∞ = 20^{\circ}C \), and knowing that heat transfer at steady implies finding a \( T_2 \) to isolate \( k \).- Use any handy numeric tools to compute as needed, ensuring correct substitution and balance to solve for any variable accurately or express analytically as required.

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Key Concepts

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

Steady-State Heat Transfer
In steady-state heat transfer, the temperature across a material does not change with time. This implies that the rate at which heat enters a material is equal to the rate at which it leaves.

In the given exercise, the heat generated by the electric heater inside the hollow aluminum sphere is constant at 80 W. This steady energy production ensures that the thermal gradients, or temperature differences, remain constant throughout the system. The inner surface of the aluminum sphere is kept at a steady temperature of 250°C.

This specific condition allows us to use mathematical models that do not account for changes in time, simplifying our calculations. It lets us accurately determine values like the thermal conductivity of the insulation material.
Spherical Geometry
Spherical geometry is essential in understanding how heat is distributed in this problem. Unlike flat surfaces, heat transfer in spheres (two concentric spherical surfaces in this case) involves radial symmetry.

The aluminum sphere has different inner and outer radii: 0.15 m and 0.18 m, respectively. The thickness of the insulation adds another layer of complexity, creating a third spherical surface at a radius of 0.30 m.

Given the geometry, the equations for heat transfer must account for the changes in the surface area with respect to the radius. The mathematical expressions involve logarithms, as you might have noticed with the fraction terms in the conduction equation: \[ Q = \frac{4\pi k(T_1 - T_2)}{\frac{1}{r_2} - \frac{1}{r_3}} \]
These expressions represent how the curvature of the surfaces affects the heat transfer processes, making spherical geometry a crucial concept for solving the problem correctly.
Conduction and Convection Principles
In our exercise, we have two main types of heat transfer: conduction and convection.
  • **Conduction** involves heat transfer through a solid material, in this case, through the aluminum and the insulation. It relies on the material properties, specifically thermal conductivity. The equation for conduction, \[ Q = \frac{4\pi k(T_1 - T_2)}{\frac{1}{r_2} - \frac{1}{r_3}} \], shows how the thermal conductivity \( k \) influences the rate of heat transfer.

  • **Convection** occurs at the outer surface of the insulation. Here, heat is transferred away to the surrounding air, facilitated by the movement of fluid. The convection heat transfer is described using \[ Q = h \cdot 4\pi r_3^2 (T_2 - T_∞) \], where \( h \) is the convective heat transfer coefficient, describing the efficiency of this process.

The crucial insight is that, at steady-state, the rates of conduction and convection are in balance. Knowing this allows us to equate the conduction model to the convection model to solve for unknown parameters, such as \( k \). This linked approach underlines the importance of understanding both conduction and convection principles to accurately find solutions to thermal problems.

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Most popular questions from this chapter

The evaporator section of a refrigeration unit consists of thin-walled, 10-mm- diameter tubes through which refrigcrant passes at a temperature of \(-18^{\circ} \mathrm{C}\). Air is cooled as it flows over the tubes, maintaining a surface convection coefficient of \(100 \mathrm{~W} / \mathrm{m}^{2}\) - \(\mathrm{K}\), and is subsequently routed to the refrigerator compartment. (a) For the foregoing conditions and an air temperature of \(-3^{\circ} \mathrm{C}\), what is the rate at which heat is extracted from the air per unit tube length? (b) If the refrigerator's defrost unit malfunctions, frost will slowly accumulate on the outer tube surface. Assess the effect of frost formation on the cooling capacity of a tube for frost laycr thicknesses in the range \(0 \leq \delta \leq 4 \mathrm{~mm}\). Frost may be assumed to have a thermal conductivity of \(0.4 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). (c) The refrigerator is disconnected after the defrost unit malfunctions and a \(2 \mathrm{~mm}\)-thick layer of frost has formed. If the tubes are in ambient air for which \(T_{\mathrm{w}}=20^{\circ} \mathrm{C}\) and natural convection maintains a convection coefficient of \(2 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), how long will it take for the frost to melt? The frost may be assamed to have a mass density of \(700 \mathrm{~kg} / \mathrm{m}^{3}\) and a later heat of fusion of \(334 \mathrm{~kJ} / \mathrm{kg}\).

A 40-mm-long, 2 -mm-diameter pin fin is fabricated of an aluminum alloy \(\left(k=140 \mathrm{~W} / \mathrm{m}^{2}+\mathrm{K}\right)\). (a) Determine the fin heat transfer rate for \(T_{b}=50^{\circ} \mathrm{C}\). \(T_{\mathrm{w}}=25^{\circ} \mathrm{C}, h=1000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and an adiabatic tip condition. (b) An engineer suggests that by holding the fin tip at a low temperature, the fin heat transfer rate can be increased. For \(T(x=L)=0^{\circ} \mathrm{C}\), determine the new fin heat transfer rate. Other conditions are as in part (a). (c) Plot the temperature distribution, \(T(x)\), over the range \(0 \leq x \leq L\) for the adiabatic tip case and the preseribed tip temperature case. Also show the ambient temperature in your gruph. Discuss relevant features of the temperature distribution.

A plane wall of thickness \(0.1 \mathrm{~m}\) and thermal conductiv ity \(25 \mathrm{~W} / \mathrm{m}\), K having uniform volumetric heat generation of \(0.3 \mathrm{MW} / \mathrm{m}^{3}\) is insulated on one side, while the other side is exposed to a fluid at \(92^{\circ} \mathrm{C}\). The convection heat transfer coefficient between the wall and the fluid is \(500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Determine the maximum temperature in the wall.

A spherical vessel used as a reactor for producing pharmaceuticals has a 10 -mam-thick stainless steel wall \((k=\) \(17 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) and an inner diameter of \(1 \mathrm{~m}\). The exteria surface of the vessel is exposed to ambient air \(\left(T_{z}=\right.\) \(25^{\circ} \mathrm{C}\) ) for which a convection coefficient of \(6 \mathrm{~W} / \mathrm{m}^{2}+\mathrm{K}\) may be assumed. (a) During steady-state operation, an inner surfact temperature of \(50^{\circ} \mathrm{C}\) is maintained by enengy geneated within the reactor. What is the heat loss from the vessel? (b) If a 20-mm-thick layer of fiberglass insulation \((k=\) \(0.040 \mathrm{~W} / \mathrm{m}\) - K) is applied to the exterior of the ve sel and the rate of thermal energy generation is inchanged, what is the inner surface temperature of the vessel?

A thin clectrical heater is inserted between a long circular rod and a concentric tube with inner and outer radii of 20 and \(40 \mathrm{~mm}\). The rod (A) has a thermal conductivity of \(k_{A}=0.15 \mathrm{~W} / \mathrm{m}+\mathrm{K}\). while the tube (B) has a thermal conductivity of \(k_{\mathrm{B}}=1.5 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\) and its cuter surface is subjected to convection with a fluid of temperature \(T_{w}=-15^{\circ} \mathrm{C}\) and heat transfer coefficient \(50 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The thermal contact resistance betueen the cylinder surfaces and the heater is negligible. (a) Determine the electrical power per unit length of the cylinders (W/m) that is required to maintain the outer surface of eylinder \(\mathrm{B}\) at \(5^{\circ} \mathrm{C}\). (b) What is the temperature at the center of cylinder A?

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