/*! 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 66 A vertical slab of Wood's metal ... [FREE SOLUTION] | 91影视

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A vertical slab of Wood's metal is joined to a substrate on one surface and is melted as it is uniformly irradiated by a laser source on the opposite surface. The metal is initially at its fusion temperature of \(T_{f}=72^{\circ} \mathrm{C}\), and the melt runs off by gravity as soon as it is formed. The absorptivity of the metal to the laser radiation is \(\alpha_{1}=0.4\), and its latent heat of fusion is \(h_{s f}=33 \mathrm{~kJ} / \mathrm{kg}\). (a) Neglecting heat transfer from the irradiated surface by convection or radiation exchange with the surroundings, determine the instantaneous rate of melting in \(\mathrm{kg} / \mathrm{s} \cdot \mathrm{m}^{2}\) if the laser irradiation is \(5 \mathrm{~kW} / \mathrm{m}^{2}\). How much material is removed if irradiation is maintained for a period of \(2 \mathrm{~s}\) ? (b) Allowing for convection to ambient air, with \(T_{\infty}=20^{\circ} \mathrm{C}\) and \(h=15 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), and radiation exchange with large surroundings \((\varepsilon=0.4\), \(T_{\text {sur }}=20^{\circ} \mathrm{C}\) ), determine the instantaneous rate of melting during irradiation.

Short Answer

Expert verified
(a) The instantaneous rate of melting when neglecting heat transfer is \(0.0606\, kg/s\cdot m^{2}\), and the material removed after 2 seconds is \(0.1212\, kg/m^{2}\). (b) Considering heat transfer, the instantaneous rate of melting is \(0.0948\, kg/s\cdot m^{2}\).

Step by step solution

01

Calculate the absorbed heat energy

We are given that the laser irradiation is \(5 kW/m^2\) and the absorptivity is \(0.4\). Calculate the absorbed heat energy: \[E_{abs} = Irradiation \times Absorptivity\] \[E_{abs}=5\, kW/m^{2}\times0.4=2 kW/m^{2}\]
02

Determine the rate of melting

To find the rate of melting (in kg/s.m虏), divide the absorbed energy by the latent heat of fusion: \[Rate_{melting}= \frac{E_{abs}}{h_{sf}}\] \[Rate_{melting}= \frac{2000\, \cancel{J/s} \cdot m^{2}}{33000\, \cancel{J}/kg}= 0.0606\,kg/s\cdot m^{2}\]
03

Calculate the material removed in 2 seconds

Multiply the rate of melting by the irradiation time (2 s) to find the total material removed: \[Material_{removed}= Rate_{melting} \times Time\] \[Material_{removed}= 0.0606\, kg/s\cdot m^{2}\times 2s= 0.1212\, kg/m^{2}\] (a) The instantaneous rate of melting is \(0.0606\, kg/s\cdot m^{2}\) and \(0.1212\, kg/m^{2}\) of material is removed after 2 seconds. (b) Considering heat transfer:
04

Calculate the convective heat transfer

Determine the convective heat transfer using the given temperature and heat transfer coefficient: \[Q_{conv} = h(T_{\infty} - T_{f})\] \[Q_{conv} = 15\,W/m^{2}K(20^{\circ} C - 72^{\circ} C) = -780\,W/m^2\]
05

Calculate the radiative heat transfer

Calculate the radiative heat transfer using the given emissivity and surrounding temperature: \[Q_{rad}=\varepsilon\sigma(T_{f}^{4} - T_{sur}^{4})\] \[Q_{rad} = 0.4(5.67\times10^{-8} W/m^2 K^4)((345 K)^4 -(293)^4) \approx -350.724\,W/m^2\]
06

Calculate the remaining energy for melting

To find the remaining energy for melting, sum the energy absorbed and heat transfer energies: \[E_{remaining}= E_{abs} - Q_{conv} - Q_{rad}\] \[E_{remaining}= 2000\,W/m^{2}+780\,W/m^2+350.724\,W/m^2 \approx 3130.724\,W/m^2\]
07

Calculate the instantaneous rate of melting with heat transfer

Divide the remaining energy by the latent heat of fusion to find the rate of melting with heat transfer: \[Rate_{melting\_heat\_transfer}=\frac{E_{remaining}}{h_{sf}}\] \[Rate_{melting\__ht\_transfer}=\frac{3130.712\,\cancel{J/s}\cdot m^{2}}{33000\,\cancel{J}/kg}\approx0.0948\,kg/s\cdot m^{2}\] (b) The instantaneous rate of melting considering heat transfer is \(0.0948\, kg/s\cdot m^{2}\).

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Key Concepts

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

Latent Heat of Fusion
Latent heat of fusion refers to the amount of heat required to change a substance from a solid to a liquid at constant temperature and pressure. In the context of our original exercise, the Wood's metal slab is subjected to this process. The metal starts melting at its fusion temperature of 72掳C.

When the laser irradiates the metal at a power of 5 kW/m虏, the absorbed heat energy is calculated by multiplying this power by the metal's absorptivity, which is 0.4:
  • Absorbed Energy: 2 kW/m虏
To determine how fast the metal melts, you can divide the absorbed heat energy by the latent heat of fusion, given as 33 kJ/kg. This calculation gives you the melting rate, which shows how much material turns from solid to liquid per square meter every second:
  • Instantaneous Melting Rate: 0.0606 kg/s路m虏
Understanding latent heat is essential for calculating heat required in phase transitions without temperature changes.
Convective Heat Transfer
Convective heat transfer is the transfer of heat between a solid surface and a fluid due to fluid motion. In the exercise, convection occurs between the surface of the Wood's metal and ambient air.

The convective heat loss is determined by the surrounding air temperature (20掳C), the metal's fusion temperature (72掳C), and a heat transfer coefficient (15 W/m虏路K). You utilize the formula:
  • \[Q_{conv} = h(T_{f} - T_{ ext{ambient}})\]
The result of this calculation is a heat loss of -780 W/m虏, meaning heat is leaving the metal. This needs to be subtracted from the absorbed energy to find out how much energy actually aids the melting process. This accounts for the real-world scenario where not all energy results in melting because of surrounding heat exchanges.

Taking convective heat loss into account helps in identifying less apparent influences on thermal systems, allowing for more precise engineering calculations.
Radiative Heat Transfer
Radiative heat transfer is the process where heat is emitted as electromagnetic waves. This method does not require a medium and can occur across a vacuum, unlike conduction and convection.

In the problem, the metal also exchanges heat through radiation with its large surroundings maintained at 20掳C. The emissivity of the surface is given as 0.4 and the Stefan-Boltzmann constant (\(5.67 \times 10^{-8} \) W/m虏K鈦) is used in the formula:
  • \[Q_{rad}= \varepsilon \sigma(T_{f}^{4} - T_{sur}^{4})\]
This gives a radiative heat loss of approximately -350.724 W/m虏.

Again, this amount must also be deducted from the absorbed energy. By considering radiation, you assess how much heat is lost to large, cool surroundings through emission. Understanding radiative effects is critical for designing systems involved with high temperatures or in space, where radiation is a dominant form of heat transfer.

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Most popular questions from this chapter

An instrumentation package has a spherical outer surface of diameter \(D=100 \mathrm{~mm}\) and emissivity \(\varepsilon=0.25\). The package is placed in a large space simulation chamber whose walls are maintained at \(77 \mathrm{~K}\). If operation of the electronic components is restricted to the temperature range \(40 \leq T \leq 85^{\circ} \mathrm{C}\), what is the range of acceptable power dissipation for the package? Display your results graphically, showing also the effect of variations in the emissivity by considering values of \(0.20\) and \(0.30\).

A vacuum system, as used in sputtering electrically conducting thin films on microcircuits, is comprised of a baseplate maintained by an electrical heater at \(300 \mathrm{~K}\) and a shroud within the enclosure maintained at \(77 \mathrm{~K}\) by a liquid-nitrogen coolant loop. The circular baseplate, insulated on the lower side, is \(0.3 \mathrm{~m}\) in diameter and has an emissivity of \(0.25\). (a) How much electrical power must be provided to the baseplate heater? (b) At what rate must liquid nitrogen be supplied to the shroud if its heat of vaporization is \(125 \mathrm{~kJ} / \mathrm{kg}\) ? (c) To reduce the liquid nitrogen consumption, it is proposed to bond a thin sheet of aluminum foil \((\varepsilon=0.09)\) to the baseplate. Will this have the desired effect?

A computer consists of an array of five printed circuit boards (PCBs), each dissipating \(P_{b}=20 \mathrm{~W}\) of power. Cooling of the electronic components on a board is provided by the forced flow of air, equally distributed in passages formed by adjoining boards, and the convection coefficient associated with heat transfer from the components to the air is approximately \(h=200 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Air enters the computer console at a temperature of \(T_{i}=20^{\circ} \mathrm{C}\), and flow is driven by a fan whose power consumption is \(P_{f}=25 \mathrm{~W}\). (a) If the temperature rise of the airflow, \(\left(T_{o}-T_{i}\right)\), is not to exceed \(15^{\circ} \mathrm{C}\), what is the minimum allowable volumetric flow rate \(\dot{\forall}\) of the air? The density and specific heat of the air may be approximated as \(\rho=1.161\) \(\mathrm{kg} / \mathrm{m}^{3}\) and \(c_{p}=1007 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), respectively. (b) The component that is most susceptible to thermal failure dissipates \(1 \mathrm{~W} / \mathrm{cm}^{2}\) of surface area. To minimize the potential for thermal failure, where should the component be installed on a PCB? What is its surface temperature at this location?

A square silicon chip \((k=150 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K})\) is of width \(w=5 \mathrm{~mm}\) on a side and of thickness \(t=1 \mathrm{~mm}\). The chip is mounted in a substrate such that its side and back surfaces are insulated, while the front surface is exposed to a coolant. If \(4 \mathrm{~W}\) are being dissipated in circuits mounted to the back surface of the chip, what is the steady-state temperature difference between back and front surfaces?

A thermodynamic analysis of a proposed Brayton cycle gas turbine yields \(P=5 \mathrm{MW}\) of net power production. The compressor, at an average temperature of \(T_{c}=400^{\circ} \mathrm{C}\), is driven by the turbine at an average temperature of \(T_{h}=1000^{\circ} \mathrm{C}\) by way of an \(L=1\)-m-long, \(d=70-\mathrm{mm}-\) diameter shaft of thermal conductivity \(k=40 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). (a) Compare the steady-state conduction rate through the shaft connecting the hot turbine to the warm compressor to the net power predicted by the thermodynamics-based analysis. (b) A research team proposes to scale down the gas turbine of part (a), keeping all dimensions in the same proportions. The team assumes that the same hot and cold temperatures exist as in part (a) and that the net power output of the gas turbine is proportional to the overall volume of the device. Plot the ratio of the conduction through the shaft to the net power output of the turbine over the range \(0.005 \mathrm{~m} \leq L \leq 1 \mathrm{~m}\). Is a scaled-down device with \(L=0.005 \mathrm{~m}\) feasible?

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