Consider a large 3-cm-thick stainless steel plate in which heat is generated uniformly at a rate of \(5 \times 10^{6} \mathrm{~W} / \mathrm{m}^{3}\). Assuming the plate is losing heat from both sides, determine the heat flux on the surface of the plate during steady operation. Answer: \(75 \mathrm{~kW} / \mathrm{m}^{2}\)

Short Answer

Expert verified
Answer: The heat flux on the surface of the plate during steady operation is 75 kW/m^2.

Step by step solution

01

Calculate the volume of heat generated per unit area

To calculate the heat generated per unit area, we will use the following formula: Heat_generated_per_unit_area = Heat_generation_rate × Thickness Where: - Heat_generated_per_unit_area is the heat generated per unit area (W/m^2) - Heat_generation_rate is the rate of heat generation (5 x 10^6 W/m^3) - Thickness is the thickness of the plate (0.03 m)
02

Calculate the heat generated per unit area

Using the formula from Step 1, we will calculate the heat generated per unit area: Heat_generated_per_unit_area = (5 x 10^6 W/m^3) × 0.03 m Heat_generated_per_unit_area = 150000 W/m^2
03

Calculate the heat loss from both sides of the plate

Since the plate loses heat from both sides, we need to divide the total heat generated per unit area by 2 to obtain the heat loss from each side: Heat_loss_per_side = Heat_generated_per_unit_area / 2
04

Calculate the heat flux on the surface of the plate

Now, we can calculate the heat flux on the surface of the plate using the value from Step 3: Heat_loss_per_side = 150000 W/m^2 / 2 Heat_loss_per_side = 75000 W/m^2 The heat flux on the surface of the plate during steady operation is 75 kW/m^2, which matches the provided solution.

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Key Concepts

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

Heat Generation in Solids
Understanding the process of heat generation in solids is fundamental in thermal engineering. It’s a scenario encountered in numerous applications, from electronic components to industrial machining processes. Heat generation can be attributed to various sources such as electrical resistance, chemical reactions, or even nuclear reactions in some cases.

When thermal energy is generated within a solid, it is often expressed in terms of a volumetric heat generation rate, represented by the symbol 'q'' and with units of watts per cubic meter \( \mathrm{W/m^3} \). In the given exercise, the stainless steel plate has a uniform heat generation rate of \( 5 \times 10^6 \mathrm{W/m^3} \). To interpret this, imagine every cubic meter of the steel plate producing 5 million joules every second.

For a more practical approach, such as in the provided exercise, it may be necessary to convert this volumetric rate to an area-specific rate, especially when dealing with heat conduction across a thin plate. This translation is essential for designing cooling systems or in thermal simulations to ensure material integrity and safety in various engineering applications.
Steady-State Thermal Conduction
Steady-state thermal conduction is a condition where the temperature distribution in the material does not change over time, meaning that the thermal energy entering any region of the material is equal to the thermal energy leaving it. This balance is essential in many engineering designs as it implies a predictable and stable operation of the system.

In the context of our textbook problem, assuming steady-state means that the heat generated within the steel plate is consistently being dissipated across its surfaces over time. The rate of heat conduction through a material is governed by Fourier's law of heat conduction, which states that the heat flux \( q \) through a material is proportional to the negative gradient of the temperature and the material's area, given by the equation \( q = -k \cdot A \cdot \frac{dT}{dx} \), where 'k' is the thermal conductivity of the material.

In simpler terms, under steady-state conditions, the plate reaches an equilibrium where the amount of heat it generates internally is equal to the amount it loses to its surroundings, preventing any rise in temperature within the plate over time. This is a decisive factor for thermal management in various engineering fields.
Thermal Analysis of Plates
Thermal analysis of plates involves understanding how heat is conducted and dissipated in plate-like structures. These structures are particularly interesting because of their broad application in electronics, construction, and mechanical systems where they can serve as walls, barriers, or heat exchangers.

A critical aspect of plate thermal analysis is boundary conditions, which define how the plate interacts with its environment. In our textbook example, the stainless steel plate loses heat from both of its larger surfaces, which is a common boundary condition known as 'convective cooling'.

To ensure accurate thermal analysis, it's essential to consider the plate's thickness, material properties, and surface area. By calculating the thermal flux, as shown in the step-by-step solution (75 \( \mathrm{kW/m^2} \)), engineers can predict the temperature distribution within the plate and the extent of heat loss. This is critical for designing thermal systems that are efficient, safe, and tailored to the specific conditions of their application.

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Most popular questions from this chapter

Consider a long solid cylinder of radius \(r_{o}=4 \mathrm{~cm}\) and thermal conductivity \(k=25 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). Heat is generated in the cylinder uniformly at a rate of \(\dot{e}_{\text {gen }}=35 \mathrm{~W} / \mathrm{cm}^{3}\). The side surface of the cylinder is maintained at a constant temperature of \(T_{s}=80^{\circ} \mathrm{C}\). The variation of temperature in the cylinder is given by $$ T(r)=\frac{\dot{e}_{\text {gen }} r_{o}^{2}}{k}\left[1-\left[1-\left(\frac{r}{r_{o}}\right)^{2}\right]+T_{s}\right. $$ Based on this relation, determine \((a)\) if the heat conduction is steady or transient, \((b)\) if it is one-, two-, or three-dimensional, and \((c)\) the value of heat flux on the side surface of the cylinder at \(r=r_{o^{*}}\)

A flat-plate solar collector is used to heat water by having water flow through tubes attached at the back of the thin solar absorber plate. The absorber plate has an emissivity and an absorptivity of \(0.9\). The top surface \((x=0)\) temperature of the absorber is \(T_{0}=35^{\circ} \mathrm{C}\), and solar radiation is incident on the absorber at \(500 \mathrm{~W} / \mathrm{m}^{2}\) with a surrounding temperature of \(0^{\circ} \mathrm{C}\). Convection heat transfer coefficient at the absorber surface is \(5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), while the ambient temperature is \(25^{\circ} \mathrm{C}\). Show that the variation of temperature in the absorber plate can be expressed as \(T(x)=-\left(\dot{q}_{0} / k\right) x+T_{0}\), and determine net heat flux \(\dot{q}_{0}\) absorbed by the solar collector.

Exhaust gases from a manufacturing plant are being discharged through a 10 - \(\mathrm{m}\) tall exhaust stack with outer diameter of \(1 \mathrm{~m}\), wall thickness of \(10 \mathrm{~cm}\), and thermal conductivity of \(40 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The exhaust gases are discharged at a rate of \(1.2 \mathrm{~kg} / \mathrm{s}\), while temperature drop between inlet and exit of the exhaust stack is \(30^{\circ} \mathrm{C}\), and the constant pressure specific heat of the exhaust gasses is \(1600 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\). On a particular day, the outer surface of the exhaust stack experiences radiation with the surrounding at \(27^{\circ} \mathrm{C}\), and convection with the ambient air at \(27^{\circ} \mathrm{C}\) also, with an average convection heat transfer coefficient of \(8 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Solar radiation is incident on the exhaust stack outer surface at a rate of \(150 \mathrm{~W} / \mathrm{m}^{2}\), and both the emissivity and solar absorptivity of the outer surface are 0.9. Assuming steady one-dimensional heat transfer, (a) obtain the variation of temperature in the exhaust stack wall and (b) determine the inner surface temperature of the exhaust stack.

Consider a chilled-water pipe of length \(L\), inner radius \(r_{1}\), outer radius \(r_{2}\), and thermal conductivity \(k\). Water flows in the pipe at a temperature \(T_{f}\) and the heat transfer coefficient at the inner surface is \(h\). If the pipe is well-insulated on the outer surface, \((a)\) express the differential equation and the boundary conditions for steady one-dimensional heat conduction through the pipe and \((b)\) obtain a relation for the variation of temperature in the pipe by solving the differential equation.

A circular metal pipe has a wall thickness of \(10 \mathrm{~mm}\) and an inner diameter of \(10 \mathrm{~cm}\). The pipe's outer surface is subjected to a uniform heat flux of \(5 \mathrm{~kW} / \mathrm{m}^{2}\) and has a temperature of \(500^{\circ} \mathrm{C}\). The metal pipe has a variable thermal conductivity given as \(k(T)=k_{0}(1+\beta T)\), where \(k_{0}=7.5 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), \(\beta=0.0012 \mathrm{~K}^{-1}\), and \(T\) is in \(\mathrm{K}\). Determine the inner surface temperature of the pipe.

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