/*! 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 38 A vertical cylindrical mass of \... [FREE SOLUTION] | 91Ó°ÊÓ

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A vertical cylindrical mass of \(5 \mathrm{~kg}\) undergoes a process during which the velocity decreases from \(30 \mathrm{~m} / \mathrm{s}\) to \(15 \mathrm{~m} / \mathrm{s}\), while the elevation remains unchanged. The initial specific internal energy of the mass is \(1.2 \mathrm{~kJ} / \mathrm{kg}\) and the final specific internal energy is \(1.9 \mathrm{~kJ} / \mathrm{kg}\). During the process, the mass receives \(2 \mathrm{~kJ}\) of energy by heat transfer through its bottom surface and loses \(1 \mathrm{~kJ}\) of energy by heat transfer through its top surface. The lateral surface experiences no heat transfer. For this process, evaluate (a) the change in kinetic energy of the mass in \(\mathrm{kJ}\), and (b) the work in \(\mathrm{kJ}\).

Short Answer

Expert verified
(a) -1.6875 kJ, (b) -0.8125 kJ

Step by step solution

01

- Calculate Initial Kinetic Energy

The initial kinetic energy is given by the formula \( KE_{initial} = \frac{1}{2} m v_{initial}^2 \). Plugging in the values, we get \[ KE_{initial} = \frac{1}{2} \times 5 \times 30^2 = 2250 \text{J} = 2.25 \text{kJ} \]
02

- Calculate Final Kinetic Energy

The final kinetic energy is given by the formula \( KE_{final} = \frac{1}{2} m v_{final}^2 \). Plugging in the values, we get \[ KE_{final} = \frac{1}{2} \times 5 \times 15^2 = 562.5 \text{J} = 0.5625 \text{kJ} \]
03

- Calculate Change in Kinetic Energy

The change in kinetic energy \( \Delta KE \) is the difference between the initial and final kinetic energy. Therefore, \[ \Delta KE = KE_{final} - KE_{initial} = 0.5625 - 2.25 = -1.6875 \text{kJ} \]
04

- Calculate Change in Internal Energy

The mass-specific internal energy change is given by \( \Delta U = m \times \left( u_{final} - u_{initial} \right) \). Plugging in the values, we get \[ \Delta U = 5 \times (1.9 - 1.2) = 5 \times 0.7 = 3.5 \text{kJ} \]
05

- Calculate Total Heat Transfer

The total heat transfer (Q) is the sum of energy received and lost by heat transfer. Therefore, \[ Q = 2 \text{kJ} - 1 \text{kJ} = 1 \text{kJ} \]
06

- Apply the First Law of Thermodynamics

The first law of thermodynamics states that \( Q - W = \Delta U + \Delta KE \). Rearrange this to solve for work (W): \[ W = Q - \Delta U - \Delta KE \]
07

- Calculate Work Done

Substitute the values into the equation: \[ W = 1 - 3.5 - (-1.6875) = 1 - 3.5 + 1.6875 = -0.8125 \text{kJ} \]

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Key Concepts

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

kinetic energy
In physics, kinetic energy is the energy an object possesses due to its motion. The faster an object moves, the more kinetic energy it has. The formula to calculate kinetic energy is given by \( KE = \frac{1}{2} mv^2 \), where \( m \) is the mass and \( v \) is the velocity of the object.
In the given exercise, the initial and final velocities of the cylindrical mass are provided. We can calculate the initial kinetic energy using the formula:
\[ KE_{initial} = \frac{1}{2} \times 5 \times 30^2 \]
which equals 2.25 kJ. Similarly, the final kinetic energy is calculated as:
\[ KE_{final} = \frac{1}{2} \times 5 \times 15^2 \]
which equals 0.5625 kJ. The change in kinetic energy is then:
\[ \Delta KE = KE_{final} - KE_{initial} = 0.5625 - 2.25 = -1.6875 kJ \]
internal energy
Internal energy is the total energy contained within a system, related to both the microscopic kinetic and potential energies of its particles. It is an intrinsic property and is different from kinetic and potential energy which are macroscopic forms of energy.
In this problem, the specific internal energy (energy per kilogram) changes from 1.2 kJ/kg to 1.9 kJ/kg. To find the total change in internal energy, we use the formula:
\[ \Delta U = m \times ( u_{final} - u_{initial} ) \]
Given the mass is 5 kg, we plug in the values:
\[ \Delta U = 5 \times (1.9 - 1.2) = 5 \times 0.7 = 3.5 kJ \]
This indicates an increase in the internal energy of the system by 3.5 kJ.
heat transfer
Heat transfer is the exchange of thermal energy between physical systems. The heat transfer can be through conduction, convection, or radiation. In this problem, the mass receives heat via its bottom surface and loses it through its top surface.
The amount of heat added to the system is 2 kJ, while the heat lost is 1 kJ. The net heat transfer (Q) to the system can be calculated as:
\[ Q = 2 \text{kJ} - 1 \text{kJ} = 1 \text{kJ} \]
This net heat transfer is crucial in applying the First Law of Thermodynamics to find the work done or energy change in the system.
first law of thermodynamics
The First Law of Thermodynamics, also known as the law of energy conservation, states that energy cannot be created or destroyed in an isolated system. It can only be transformed from one form to another. The mathematical representation of this law is:
\[ Q - W = \Delta U + \Delta KE \]
where \( Q \) is heat added to the system, \( W \) is work done by the system, \( \Delta U \) is the change in internal energy, and \( \Delta KE \) is the change in kinetic energy.
Using the given values:
\[ Q = 1 \text{kJ}, \Delta U = 3.5 \text{kJ}, \Delta KE = -1.6875 \text{kJ} \]
we rearrange the formula to solve for work (W):
\[ W = Q - \Delta U - \Delta KE = 1 - 3.5 - (-1.6875) = 1 - 3.5 + 1.6875 = -0.8125 \text{kJ} \]
Hence, the work done by the system in this process is -0.8125 kJ.

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Most popular questions from this chapter

A 30 -seat turboprop airliner whose mass is \(12,000 \mathrm{~kg}\) takes off from an airport and eventually achieves its cruising speed of \(600 \mathrm{~km} / \mathrm{h}\) at an altitude of \(9,000 \mathrm{~m}\). For \(g-9.8 \mathrm{~m} / \mathrm{s}^{2}\), determine the change in kinetic energy and the change in gravitational potential energy of the airliner, each in \(\mathrm{kJ}\).

\(.\mathrm{~A}\) gas within a piston-cylinder assembly undergoes a thermodynamic cycle consisting of three processes: Process 1-2: Constant volume, \(V=0.028 \mathrm{~m}^{3}, U_{2}-U_{1}=\) \(26.4 \mathrm{~kJ}\). Process 2-3: Expansion with \(p V=\) constant, \(U_{3}=U_{2}\). Process 3-1: Constant pressure, \(p=1.4\) bar, \(W_{31}=-10.5 \mathrm{~kJ}\). There are no significant changes in kinetic or potential energy. (a) Sketch the cycle on a \(p-V\) diagram. (b) Calculate the net work for the cycle, in \(\mathrm{kJ}\). (c) Calculate the heat transfer for process 2-3, in \(\mathrm{kJ}\). (d) Calculate the heat transfer for process 3-1, in \(\mathrm{kJ}\). Is this a power cycle or a refrigeration cycle?

\(\mathrm{~A}\) gas undergoes a process from state 1 , where \(p_{1}=\) \(415 \mathrm{kPa}, v_{1}=0.37 \mathrm{~m}^{3} / \mathrm{kg}\), to state 2 , where \(p_{2}=138 \mathrm{kPa}\), according to \(p v^{1.3}=\) constant. The relationship between pressure, specific volume, and specific internal energy is $$ u=(1.443) p v-221.557 $$ where \(p\) is in \(\mathrm{kPa}, v\) is in \(\mathrm{m}^{3} / \mathrm{kg}\), and \(u\) is in \(\mathrm{kJ} / \mathrm{kg}\). The mass of gas is \(4.5 \mathrm{~kg}\). Neglecting kinetic and potential energy effects, determine the heat transfer, in \(\mathrm{kJ}\).

\(.\) Air contained within a piston-cylinder assembly undergoes three processes in series: Process 1-2: Compression at constant pressure from \(p_{1}=\) \(69 \mathrm{kPa}, V_{1}=0.11 \mathrm{~m}^{3}\) to state 2 . Process 2-3: Constant-volume heating to state 3 , where \(p_{3}=345 \mathrm{kPa}\). Process 3-1: Expansion to the initial state, during which the pressure-volume relationship is \(p V=\) constant. Sketch the processes in series on \(p\)-V coordinates. Evaluate (a) the volume at state 2 , in \(\mathrm{m}^{3}\), and (b) the work for each process, in \(\mathrm{kJ}\).

According to the New York City Transit Authority, the operation of subways raise tunnel and station temperatures as much as \(263-266 \mathrm{~K}\) above ambient temperature. Principal contributors to the temperature rise include train motor operation, lighting and energy from the passengers themselves. Passenger discomfort can increase significantly in hot-weather periods if air conditioning is not provided. Still, because on-board air-conditioning units discharge energy by heat transfer to their surroundings, such units contribute to the overall tunnel and station energy management problem. Investigate the application to subways of altemative cooling strategies that provide substantial cooling with a minimal power requirement, including but not limited to thermal storage and nighttime ventilation. Write a report with at least three references.

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