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An AISI 316 stainless steel spherical container is used for storing chemicals undergoing exothermic reaction that provides a uniform heat flux of \(60 \mathrm{~kW} / \mathrm{m}^{2}\) to the container's inner surface. The container has an inner diameter of \(1 \mathrm{~m}\) and a wall thickness of \(5 \mathrm{~cm}\). For safety reason to prevent thermal burn on individuals working around the container, it is necessary to keep the container's outer surface temperature below \(50^{\circ} \mathrm{C}\). If the ambient temperature is \(23^{\circ} \mathrm{C}\), determine the necessary convection heat transfer coefficient to keep the container's outer surface temperature below \(50^{\circ} \mathrm{C}\). Is the necessary convection heat transfer coefficient feasible with free convection of air? If not, discuss other option to prevent the container's outer surface temperature from causing thermal burn.

Short Answer

Expert verified
Answer: The necessary convection heat transfer coefficient to keep the container's outer surface temperature below 50°C is approximately 2222 W/(m²K). This value is higher than the typical range for free convection of air (5 to 25 W/(m²K)), so it is not feasible. Alternative options should be considered, such as forced convection or adding insulation material.

Step by step solution

01

Calculate Surface Area and Total Heat Generated

First, we need to find the inner surface area of the container, from which the heat is being generated. The formula for the surface area of a sphere is: \[A = 4 \pi r^{2}\] where A is the surface area and r is the radius. In this case, the inner diameter is given as 1m, so the radius is 0.5m. Therefore, the surface area is: \[A = 4 \pi (0.5)^{2} = \pi \mathrm{m^{2}}\] Next, we need to find the total heat being generated. We are given that the heat flux is 60 kW/m². So, the total heat generated (Q) can be calculated as: \[Q = q_{\text{flux}} \times A\] \[Q = 60 \mathrm{kW/m^{2}} \times \pi \mathrm{m^{2}} = 60\pi \mathrm{kW}\]
02

Heat Transfer Through the Container Wall

Now, we need to determine the heat transfer through the container wall. A formula for the heat transfer rate through a sphere is given by: \[Q = \frac{kA\Delta T}{r}\] where k is the thermal conductivity of the material (AISI 316 stainless steel has k ≈ 14.9 W/m·K), A is the surface area, ΔT is the temperature difference across the wall, and r is the radius of the sphere. We want to keep the outer surface temperature below 50°C, and the ambient temperature is 23°C. Solving for ΔT, we find the temperature difference across the wall: \[\Delta T = T_{\text{inside}} - T_{\text{ambient}}\] We can solve this equation for the temperature difference across the wall, and then use the heat transfer formula to find the temperature difference between the inside and outside of the container.
03

Calculate Required Convection Heat Transfer Coefficient

The convective heat transfer formula states that: \[Q = hA\Delta T_{\text{conv}}\] where h is the convection heat transfer coefficient, A is the surface area, and ΔT_conv is the temperature difference between the outer surface of the container and the ambient temperature. We know that ΔT_conv = 50 - 23 = 27°C. We also know the total heat transfer (Q) from step 1. Now, we will solve for h: \[h = \frac{Q}{A\Delta T_{\text{conv}}}\] \[h = \frac{60\pi \mathrm{kW}}{\pi \mathrm{m^{2}} \times 27 \mathrm{K}} = \frac{60\pi \times 10^3 \mathrm{W}}{\pi \mathrm{m^{2}} \times 27 \mathrm{K}} \approx 2222 \mathrm{W/(m^{2}K)}\]
04

Feasibility and Alternative Options

The typical range of convection heat transfer coefficients for free convection of air is around 5 to 25 W/(m²K). Our calculated value of 2222 W/(m²K) is considerably higher than the typical range, which means free convection of air is not sufficient to prevent the outer surface temperature from exceeding 50°C. Alternative options to prevent thermal burn on the container's outer surface can include: 1. Forced convection (using fans or blowers) which can provide higher convection heat transfer coefficients. 2. Adding insulation material on the container's outer surface to reduce heat transfer and decrease the exposed temperature.

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Key Concepts

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

Heat Flux Calculation
Heat flux is a measure of the rate of heat energy transfer through a given surface per unit time. In our case, the given heat flux is a uniform value of 60 kW/m². To understand how much heat is actually being transferred, we need to account for the surface area of the inner surface of the sphere from which the heat is conducted. By multiplying this heat flux by the spherical surface area \( A = 4 \pi r^{2} \) (where \( r \) is the sphere's radius), we calculate the total heat generation. For the stainless steel container, this resulted in \( Q = q_{\text{flux}} \times A = 60 \pi \mathrm{kW} \) of heat energy being generated. It's crucial that students acknowledge that heat flux provides a rate, and by itself does not indicate the total heat transferred without also considering the area.

In practical situations, like in engineering applications, understanding heat flux helps in designing systems for thermal management, which might involve choosing materials or designing for proper ventilation.
Spherical Heat Transfer
Spherical heat transfer differs from planar or cylindrical heat transfer because the surface area through which heat is transferred changes with the radius. This fundamental characteristic impacts how heat transfer calculations are approached. In our textbook example, the spherical nature of the container means that the heat transfer rate through the stainless steel wall can be calculated using the formula \( Q = \frac{kA\Delta T}{r} \), emphasizing the relationship between thermal conductivity (\( k \)), surface area (\( A \)), temperature difference across the wall (\( \Delta T \)), and the sphere's radius (\( r \)).

The spherical shape ensures that heat is distributed uniformly from every point on the surface, which is an important concept when designing spherical containers or vessels in industries that require strict temperature maintenance, such as chemical storage or reactors.
Thermal Conductivity
Thermal conductivity, represented by \( k \), is a material-specific value that measures a material’s ability to conduct heat. High thermal conductivity materials transfer heat efficiently, while low thermal conductivity materials act as insulators. In our textbook problem, AISI 316 stainless steel has a thermal conductivity of approximately 14.9 W/m·K. The value of \( k \) is crucial for calculating the rate of heat transfer through the spherical wall and allows engineers to select appropriate materials for construction based on thermal requirements.

Students should appreciate that while metals typically have high thermal conductivity and are therefore good at transferring heat, materials with lower thermal conductivity are better suited for thermal insulation purposes.
Surface Area Calculation
The calculation of surface area is essential in heat transfer problems because the rate at which heat is exchanged depends on the surface area exposed to the transfer process. For spherical shapes, the surface area formula \( A = 4 \pi r^{2} \) is used, where \( r \) is the sphere’s radius. In our container example, we utilized this formula to determine the surface area involved in heat transfer, which directly impacted the total heat being generated.

It's important for students to be comfortable with surface area calculations, as they frequently appear in problems involving radiation, convection, and conduction. Understanding how to calculate surface area correctly is key in tackling multidisciplinary problems involving heat transfer, such as in environmental engineering or architectural design.
Forced Convection
Forced convection is a mechanism of heat transfer where fluid motion is generated by an external source, like a pump or a fan. It’s contrasted with natural or free convection, where fluid motion is due to buoyancy forces that arise from density differences caused by temperature variations within the fluid. The calculated convection heat transfer coefficient necessary to keep the outer surface temperature below 50°C in our problem indicated that free convection was insufficient.

Forced convection can provide much higher heat transfer coefficients; hence, it's often used in industrial processes to enhance heat dissipation. For students, understanding when to apply forced convection is critical in the design of thermal systems to ensure safety and efficiency, such as in the cooling systems of electronics or the heating systems of buildings.
Thermal Insulation
Thermal insulation refers to the use of materials with low thermal conductivity to reduce heat transfer between objects or environments. In our exercise, insulating the spherical container could be effective to reduce heat transfer to the external environment and maintain the outer surface temperature below the safety threshold, preventing thermal burns.

This concept is applied extensively in building envelopes to improve energy efficiency and in industrial applications to maintain process temperatures. For students, understanding thermal insulation is essential for designing systems aimed at energy conservation, environmental control, and personal safety. Selecting the right insulation material and thickness is a key component of solving real-world engineering challenges.

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Most popular questions from this chapter

\(80^{\circ} \mathrm{C}\). Also, determine the convection heat transfer coefficients at the beginning and at the end of the heating process. 1-133 It is well known that wind makes the cold air feel much colder as a result of the wind chill effect that is due to the increase in the convection heat transfer coefficient with increasing air velocity. The wind chill effect is usually expressed in terms of the wind chill temperature (WCT), which is the apparent temperature felt by exposed skin. For outdoor air temperature of \(0^{\circ} \mathrm{C}\), for example, the wind chill temperature is \(-5^{\circ} \mathrm{C}\) at \(20 \mathrm{~km} / \mathrm{h}\) winds and \(-9^{\circ} \mathrm{C}\) at \(60 \mathrm{~km} / \mathrm{h}\) winds. That is, a person exposed to \(0^{\circ} \mathrm{C}\) windy air at \(20 \mathrm{~km} / \mathrm{h}\) will feel as cold as a person exposed to \(-5^{\circ} \mathrm{C}\) calm air (air motion under \(5 \mathrm{~km} / \mathrm{h}\) ). For heat transfer purposes, a standing man can be modeled as a 30 -cm- diameter, 170-cm-long vertical cylinder with both the top and bottom surfaces insulated and with the side surface at an average temperature of \(34^{\circ} \mathrm{C}\). For a convection heat transfer coefficient of \(15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the rate of heat loss from this man by convection in still air at \(20^{\circ} \mathrm{C}\). What would your answer be if the convection heat transfer coefficient is increased to \(30 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) as a result of winds? What is the wind chill temperature in this case?

A \(0.3\)-cm-thick, 12-cm-high, and 18-cm-long circuit board houses 80 closely spaced logic chips on one side, each dissipating \(0.06 \mathrm{~W}\). The board is impregnated with copper fillings and has an effective thermal conductivity of \(16 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). All the heat generated in the chips is conducted across the circuit board and is dissipated from the back side of the board to the ambient air. Determine the temperature difference between the two sides of the circuit board. Answer: \(0.042^{\circ} \mathrm{C}\)

The critical heat flux (CHF) is a thermal limit at which a boiling crisis occurs whereby an abrupt rise in temperature causes overheating on fuel rod surface that leads to damage. A cylindrical fuel rod of \(2 \mathrm{~cm}\) in diameter is encased in a concentric tube and cooled by water. The fuel generates heat uniformly at a rate of \(150 \mathrm{MW} / \mathrm{m}^{3}\). The average temperature of the cooling water, sufficiently far from the fuel rod, is \(80^{\circ} \mathrm{C}\). The operating pressure of the cooling water is such that the surface temperature of the fuel rod must be kept below \(300^{\circ} \mathrm{C}\) to avoid the cooling water from reaching the critical heat flux. Determine the necessary convection heat transfer coefficient to avoid the critical heat flux from occurring.

An electronic package with a surface area of \(1 \mathrm{~m}^{2}\) placed in an orbiting space station is exposed to space. The electronics in this package dissipate all \(1 \mathrm{~kW}\) of its power to the space through its exposed surface. The exposed surface has an emissivity of \(1.0\) and an absorptivity of \(0.25\). Determine the steady state exposed surface temperature of the electronic package \((a)\) if the surface is exposed to a solar flux of \(750 \mathrm{~W} /\) \(\mathrm{m}^{2}\), and \((b)\) if the surface is not exposed to the sun.

A \(3-\mathrm{m}^{2}\) black surface at \(140^{\circ} \mathrm{C}\) is losing heat to the surrounding air at \(35^{\circ} \mathrm{C}\) by convection with a heat transfer coefficient of \(16 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and by radiation to the surrounding surfaces at \(15^{\circ} \mathrm{C}\). The total rate of heat loss from the surface is (a) \(5105 \mathrm{~W}\) (b) \(2940 \mathrm{~W}\) (c) \(3779 \mathrm{~W}\) (d) \(8819 \mathrm{~W}\) (e) \(5040 \mathrm{~W}\)

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