/*! 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 34 One lbmol of carbon monoxide gas... [FREE SOLUTION] | 91影视

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One lbmol of carbon monoxide gas is contained in a \(90-\mathrm{ft}^{3}\) rigid, insulated vessel initially at 5 atm. An electric resistor of negligible mass transfers energy to the gas at a constant rate of \(10 \mathrm{Btu} / \mathrm{s}\) for \(2 \mathrm{~min}\). Employing the ideal gas model and ignoring the effects of motion and gravity, determine (a) the change in exergy of the gas, (b) the electrical work, and (c) the exergy destruction, each in Btu. Let \(T_{0}=70^{\circ} \mathrm{F}\), \(p_{0}=1 \mathrm{~atm}\).

Short Answer

Expert verified
Change in exergy: 314.45 Btu, Electrical work: 1200 Btu, Exergy destruction: 885.55 Btu.

Step by step solution

01

Understand the Problem and Gather Data

One pound-mole (lbmol) of carbon monoxide gas is in a rigid, insulated vessel of 90 ft鲁, initially at 5 atm. Energy is supplied via an electric resistor at 10 Btu/s for 2 minutes. Given conditions: T鈧 = 70掳F and p鈧 = 1 atm. Identify the unknowns: change in exergy of the gas, electrical work, and exergy destruction, all in Btu.
02

Calculate the Electrical Work

Electrical power is given as 10 Btu/s and the duration of energy supply is 2 minutes (120 seconds). Electrical work (W) = Power 脳 Time = 10 Btu/s 脳 120 s = 1200 Btu.
03

Compute the Change in Internal Energy

Since the vessel is rigid and insulated, and the gas behaves ideally, the change in internal energy 螖U comes from the electrical work: 螖U = W = 1200 Btu.
04

Determine the Initial and Final Temperatures

Using the ideal gas law: PV = nRT. For initial state P鈧 = 5 atm, V = 90 ft鲁, n = 1 lbmol. Convert initial pressure and temperature to consistent units: P鈧 = 5 atm 脳 14.696 psi/atm = 73.48 psi. Rearrange equation: T鈧 = (P鈧乂) / (nR) where R = 10.731 psi鈰協t鲁/(lbmol鈰吢癛). T鈧 = (73.48 psi 脳 90 ft鲁) / (1 lbmol 脳 10.731 psi鈰協t鲁/(lbmol鈰吢癛)) 鈮 615.96 掳R To find final temperature T鈧, use 螖U = nCv螖T, Cv for CO is 5 Btu/(lbmol鈰吢癛): 螖U = 1 lbmol 脳 5 Btu/(lbmol鈰吢癛) 脳 螖T 1200 Btu = 5 螖T 螖T = 240 掳R T鈧 = T鈧 + 螖T = 615.96 掳R + 240 掳R = 855.96 掳R
05

Calculate Change in Exergy

Change in exergy is given by: 螖Ex = 螖U - T鈧(螖S) where T鈧 = 70掳F = 70 + 459.67 = 529.67 掳R, 螖S = nCv ln(T鈧/T鈧): 螖S = 1 lbmol 脳 5 Btu/(lbmol鈰吢癛) 脳 ln(855.96 / 615.96) 鈮 1.67 Btu/掳R Therefore, 螖Ex = 1200 Btu - 529.67 掳R 脳 1.67 Btu/掳R 鈮 1200 Btu - 885.55 Btu = 314.45 Btu.
06

Calculate Exergy Destruction

Exergy destruction: Ex_destruction = Electrical Work - Change in Exergy Ex_destruction = 1200 Btu - 314.45 Btu 鈮 885.55 Btu.

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Key Concepts

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

Ideal Gas Law
The Ideal Gas Law is a fundamental equation in thermodynamics used to describe the behavior of gases. It combines various gas laws, like Boyle's, Charles's, and Avogadro's laws, into one formula. The equation is given by:
\[ PV = nRT \]
Here,
  • *P* is the pressure of the gas,
  • *V* is the volume,
  • *n* is the number of moles,
  • *R* is the universal gas constant,
  • *T* is the temperature in absolute units (Kelvin or Rankine).

In our exercise, we employed the Ideal Gas Law to determine the initial temperature (*T鈧*) of the carbon monoxide gas. Given that we had one lbmol of gas initially at 5 atm in a 90 ft鲁 vessel, we calculated *T鈧* to be approximately 615.96 掳Rankine. This was a crucial step because it set the stage for all subsequent calculations.
Internal Energy
Internal energy is a key concept in thermodynamics, representing the total energy contained within a system due to the microscopic motions of its particles. For an ideal gas, the change in internal energy (\[ \Delta U \] ). is given by: \[ \Delta U = n \cdot C_v \cdot \Delta T \] where
  • *n* is the number of moles,
  • *C_v* is the specific heat capacity at constant volume,
  • \( \Delta T \) is the change in temperature.
Since the vessel in our problem was rigid (no volume change) and insulated (no heat transfer), the change in internal energy directly matched the electrical work done on the system, which was 1200 Btu.

In our exercise, using the specific heat capacity for carbon monoxide (*C_v* = 5 Btu/(lbmol鈰吢癛)), we determined the temperature change (\( \Delta T \) = 240 掳R). This allowed us to find the final temperature ( T鈧) of the gas.
Electrical Work
Electrical work involves transferring energy to a system using electrical power, which can result in changes in temperature and internal energy of the system. The formula utilized is:

\[ W = P \cdot t \] Here,
  • *W* is the work done, usually measured in energy units like Btu,
  • *P* is the power rate (Btu/s),
  • *t* is the duration for which power is supplied (seconds).
In the problem, the electric resistor supplied energy at a constant rate of 10 Btu/s for a duration of 2 minutes (120 seconds). Hence, the total electrical work done was:
\[ W = 10 \ Btu/s \cdot 120 \ s = 1200 \ Btu \]
This electrical work was pivotal as it equated to the change in internal energy, given the conditions of the rigid and insulated vessel.
Exergy Destruction
Exergy destruction quantifies the loss of system efficiency due to irreversibilities, such as friction or unresisted heat flow, within a thermodynamic process. It's an essential measure because it indicates the potential for improvement in energy conversion processes. The formula for exergy destruction is:
\[ \Delta Ex_d = W - \Delta Ex \] where
  • *W* is the electrical work done on the system,
  • \( \Delta Ex \) is the change in exergy.
In our specific exercise, exergy destruction was calculated by first finding the change in exergy ( \Delta Ex). This involves subtracting the product of the ambient temperature ( T鈧) and change in entropy (\( \Delta S \)) from the change in internal energy. Finally, we determined the exergy destruction to be 885.55 Btu, highlighting significant irreversibilities during this energy transfer process.

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Most popular questions from this chapter

One-half pound of air is contained in a closed, rigid, insulated tank. Initially the temperature is \(520^{\circ} \mathrm{R}\) and the pressure is \(14.7\) psia. The air is stirred by a paddle wheel until its temperature is \(600^{\circ} \mathrm{R}\). Using the ideal gas model, determine for the air the change in exergy, the transfer of exergy accompanying work, and the exergy destruction, all in Btu. Ignore the effects of motion and gravity and let \(T_{0}=537^{\circ} \mathrm{R}, p_{0}=14.7\) psia.

A concrete slab measuring \(0.3 \mathrm{~m} \times 4 \mathrm{~m} \times 6 \mathrm{~m}\), initially at \(298 \mathrm{~K}\), is exposed to the sun for several hours, after which its temperature is \(301 \mathrm{~K}\). The density of the concrete is 2300 \(\mathrm{kg} / \mathrm{m}^{3}\) and its specific heat is \(c=0.88 \mathrm{~kJ} / \mathrm{kg}+\mathrm{K}\). (a) Determine the increase in exergy of the slab, in kJ. (b) To what elevation, in \(\mathrm{m}\), would a \(1000-\mathrm{kg}\) mass have to be raised from zero elevation relative to the reference environment for its exergy to equal the exergy increase of the slab? Let \(T_{0}=298 \mathrm{~K}\), \(p_{0}=1 \mathrm{~atm}, g=9.81 \mathrm{~m} / \mathrm{s}^{2}\).

Argon enters an insulated turbine operating at steady state at \(1000^{\circ} \mathrm{C}\) and \(2 \mathrm{MPa}\) and exhausts at \(350 \mathrm{kPa}\). The mass flow rate is \(0.5 \mathrm{~kg} / \mathrm{s}\) and the turbine develops power at the rate of \(120 \mathrm{~kW}\). Determine (a) the temperature of the argon at the turbine exit, in \({ }^{\circ} \mathrm{C}\). (b) the exergy destruction rate of the turbine, in \(k W\). (c) the turbine exergetic efficiency. Neglect kinetic and potential energy effects. Let \(T_{0}=20^{\circ} \mathrm{C}\), \(p_{0}=1\) bar.

Air enters a turbine operating at steady state with a pressure of \(75 \mathrm{lbf} / \mathrm{in}^{2}\), a temperature of \(800^{\circ} \mathrm{R}\), and a velocity of 400 ft/s. At the turbine exit, the conditions are \(15 \mathrm{lbf} / \mathrm{in}^{2}\), \(600^{\circ} \mathrm{R}\), and \(100 \mathrm{ft} / \mathrm{s}\). Heat transfer from the turbine to its surroundings takes place at an average surface temperature of \(620^{\circ} \mathrm{R}\). The rate of heat transfer is 2 Btu per lb of air passing through the turbine. For the turbine, determine the work developed and the exergy destruction, each in Btu per lb of air flowing. Let \(T_{0}=40^{\circ} \mathrm{F}, p_{0}=15 \mathrm{lbf} / \mathrm{in}^{2}{ }^{2}\)

Liquid water at \(20 \mathrm{lbf} / \mathrm{in}^{2}, 50^{\circ} \mathrm{F}\) enters a mixing chamber operating at steady state with a mass flow rate of \(5 \mathrm{lb} / \mathrm{s}\) and mixes with a separate stream of steam entering at \(20 \mathrm{lb} / / \mathrm{in} .{ }^{2}\), \(250^{\circ} \mathrm{F}\) with a mass flow rate of \(0.38 \mathrm{lb} / \mathrm{s}\) A single mixed stream exits at \(20 \mathrm{lbf} / \mathrm{in}^{2}, 130^{\circ} \mathrm{F}\). Heat transfer from the mixing chamber occurs to its surroundings. Neglect the effects of motion and gravity and let \(T_{0}=70^{\circ} \mathrm{F}, p_{0}=1 \mathrm{~atm}\). Determine the rate of exergy destruction, in Btu/s, for a control volume including the mixing chamber and enough of its immediate surroundings that heat transfer occurs at \(70^{\circ} \mathrm{F}\).

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