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Argon gas enters an adiabatic compressor at \(120 \mathrm{kPa}\) and \(30^{\circ} \mathrm{C}\) with a velocity of \(20 \mathrm{m} / \mathrm{s}\) and exits at \(1.2 \mathrm{MPa}\) \(530^{\circ} \mathrm{C},\) and \(80 \mathrm{m} / \mathrm{s}\). The inlet area of the compressor is \(130 \mathrm{cm}^{2} .\) Assuming the surroundings to be at \(25^{\circ} \mathrm{C}\), determine the reversible power input and exergy destroyed.

Short Answer

Expert verified
The main goal of the exercise is to determine the reversible power input and exergy destroyed during the process.

Step by step solution

01

Find the mass flow rate of argon gas

First, we need to find the mass flow rate of the argon gas entering the compressor. To do this, we can use the equation: \(\dot{m} = \rho AV\), where \(\rho\) is the density of argon gas, \(A\) is the area of the inlet, and \(V\) is the velocity of the gas. However, we know that \(PV=mRT\). Therefore, \(\rho = \frac{m}{V}=\frac{P}{RT}\), where \(P\) is the pressure, \(R\) is the specific gas constant for argon (\(R_{Ar} = 0.2081 \,kJ/kg \cdot K\)), and \(T\) is the temperature in Kelvin. Given the pressure, temperature, and velocity at the inlet, firstly we can find \(\rho_{1}\), then calculate the mass flow rate \(\dot{m}\).
02

Apply the First Law of Thermodynamics

Next, we will apply the First Law of Thermodynamics to the compressor to find the work input. The equation for an adiabatic process is: \(\Delta h + \frac{1}{2}\Delta (V^2) = w\), where \(\Delta h\) is the change in specific enthalpy of argon, \(\Delta (V^2)\) is the change in the velocity squared, and \(w\) is the work input. Since the process is adiabatic, there is no heat transfer involved. Substituting the given values, we can find the work input.
03

Apply the Second Law of Thermodynamics

Now we will apply the Second Law of Thermodynamics to find the exergy destroyed. The exergy balance equation for an adiabatic compressor is: \(\dot{m}(\Delta e_x) = -\dot{W} - T_0\dot{m}(\Delta s)\), where \(\Delta e_x\) is the change in specific exergy, \(\dot{W}\) is the power input, and \(\Delta s\) is the change in specific entropy. To solve for the exergy destroyed, we need to calculate the change in specific exergy. This requires knowing the specific enthalpy and entropy changes as well as the temperature and pressure changes. The exergy change is given by the equation: \(\Delta e_x = \Delta h - T_0\Delta s + \frac{1}{2}\Delta(V^2)\) Using the known values, we can calculate the exergy destroyed during the process.

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Most popular questions from this chapter

In order to cool 1 ton of water at \(20^{\circ} \mathrm{C}\) in an insulated tank, a person pours \(80 \mathrm{kg}\) of ice at \(-5^{\circ} \mathrm{C}\) into the water. Determine ( \(a\) ) the final equilibrium temperature in the \(\operatorname{tank}\) and \((b)\) the exergy destroyed during this process. The melting temperature and the heat of fusion of ice at atmospheric pressure are \(0^{\circ} \mathrm{C}\) and \(333.7 \mathrm{kJ} / \mathrm{kg}\), respectively. Take \(T_{0}=20^{\circ} \mathrm{C}\).

A 70 -lbm copper block initially at \(220^{\circ} \mathrm{F}\) is dropped into an insulated tank that contains \(1.2 \mathrm{ft}^{3}\) of water at \(65^{\circ} \mathrm{F}\) Determine \((a)\) the final equilibrium temperature and \((b)\) the work potential wasted during this process. Assume the surroundings to be at \(65^{\circ} \mathrm{F}\).

Steam at \(7 \mathrm{MPa}\) and \(400^{\circ} \mathrm{C}\) enters a two-stage adiabatic turbine at a rate of \(15 \mathrm{kg} / \mathrm{s}\). Ten percent of the steam is extracted at the end of the first stage at a pressure of \(1.8 \mathrm{MPa}\) for other use. The remainder of the steam is further expanded in the second stage and leaves the turbine at 10 kPa. If the turbine has an isentropic efficiency of 88 percent, determine the wasted power potential during this process as a result of irreversibilities. Assume the surroundings to be at \(25^{\circ} \mathrm{C}\).

Argon gas enters an adiabatic turbine at \(1300^{\circ} \mathrm{F}\) and 200 psia at a rate of \(40 \mathrm{lbm} / \mathrm{min}\) and exhausts at 20 psia. If the power output of the turbine is 105 hp, determine ( \(a\) ) the isentropic efficiency and \((b)\) the second-law efficiency of the turbine. Assume the surroundings to be at \(77^{\circ} \mathrm{F}\).

Steam is condensed in a closed system at a constant pressure of 75 kPa from a saturated vapor to a saturated liquid by rejecting heat to a thermal energy reservoir at \(37^{\circ} \mathrm{C}\) Determine the second-law efficiency of this process. Take \\[ T_{0}=25^{\circ} \mathrm{C} \text { and } P_{0}=100 \mathrm{kPa} \\].

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