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A rigid tank having a volume of \(0.1 \mathrm{~m}^{3}\) initially contains water as a two-phase liquid-vapor mixture at 1 bar and a quality of \(1 \%\). The water is heated in two stages: Stage 1: Constant-volume heating until the pressure is 20 bar. Stage 2: Continued heating while saturated water vapor is slowly withdrawn from the tank at a constant pressure of 20 bar. Heating ceases when all the water remaining in the tank is saturated vapor at 20 bar. For the water, evaluate the heat transfer, in kJ, for each stage of heating. Ignore kinetic and potential energy effects.

Short Answer

Expert verified
Use steam tables for properties. Calculate internal energy changes ( delta U ) for both stages. Sum heat transfers for total heat transfer.

Step by step solution

01

Determine initial state properties

The tank contains a two-phase mixture of water at 1 bar and a quality (x) of 1%. Use steam tables to find the specific volumes (v_{f} ) and (v_{g} ) at 1 bar. Calculate the initial specific volume (v_{i} ) using the formula v_{i} = (1 - x) v_{f} + x v_{g} ).
02

Determine specific volume at 20 bar

Since the heating is at a constant volume, the specific volume does not change. Therefore, the specific volume at 20 bar (v_{2w} ) is the same as the initial specific volume (v_{i} ). Find v_{f} and v_{g} at 20 bar, and if v_{i} is less than v_{f} , the water is a sub-cooled liquid; if v_{i} is greater than v_{g} , it is a superheated vapor; otherwise, it is a mixture.
03

Calculate internal energy change for Stage 1

Using the specific volumes and properties from the steam tables, calculate the change in internal energy (delta U ) during stage 1 using delta U = m(u_2f - u_1) ) where m is mass, u_2f is the internal energy at final state (saturated liquid at 20 bar), and u_1 is the initial internal energy.
04

Calculate heat transfer for Stage 1

Since the process is at constant volume, work done (W ) is zero and heat transfer (Q ) is equal to the change in internal energy ( delta U ).
05

Calculate internal energy change for Stage 2

In Stage 2, heat is added till the water remaining in the tank becomes saturated vapor at 20 bar. Calculate the change in internal energy ( delta U ) using the internal energy values for the initial mixture and the final state (saturated vapor).
06

Calculate heat transfer for Stage 2

Use the first law of thermodynamics and recognize that the tank is rigid (constant volume), so work done (W ) is zero. Therefore, heat transfer for stage 2 is equal to the change in internal energy ( delta U ).
07

Calculate total heat transfer

Sum the heat transfers from stages 1 and 2 to obtain the total heat transfer.

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Key Concepts

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

two-phase liquid-vapor mixture
In thermodynamics, a two-phase liquid-vapor mixture means that the substance exists partially as liquid and partially as vapor simultaneously, in equilibrium. This often happens with water where part of it is liquid and part of it is steam.
For example, when water is at 1 bar pressure and has a quality of 1%, only 1% of the water is in the vapor phase while the remaining 99% is still liquid.
To analyze such mixtures, we use the concept of **quality (x)**, which represents the fraction of the mass of the mixture that is vapor. Quality is defined as:
  • x = (mass of vapor) / (total mass)
Using steam tables, we can determine specific properties like specific volume, specific enthalpy, and specific internal energy for the liquid and vapor phases. The formula to calculate the specific volume for a two-phase mixture is:
  • v = (1 - x) v_f + x v_g
where v_f is the specific volume of the liquid phase and v_g is the specific volume of the vapor phase. These properties help us understand how the mixture behaves when it undergoes processes like heating.
constant-volume heating
In this problem, the water inside the tank is heated at constant volume, meaning the volume of the tank does not change throughout the process. During constant-volume heating, no work is done since the volume remains fixed ( W = 0 ).
The specific volume ( v ) also does not change. Instead, the energy changes that occur due to heating are reflected in the internal energy ( U ) changes of the water. This makes the internal energy a crucial variable to consider.
Using steam tables, we can find the internal energy values for various states of the mixture at different pressures. According to the First Law of Thermodynamics for a closed system:
  • Q = ΔU) + ( W
where Q is the heat added, ΔU is the change in internal energy, and W is the work done. In constant-volume processes, since W is zero:
  • Q = ΔU)
Essentially, all the heat added to the system goes into changing its internal energy.
internal energy change
Internal energy ( U ) change is a core concept when solving thermodynamics problems. Internal energy is the sum of all the microscopic forms of energy of a system.
During heating, especially at constant volume, the change in internal energy ( ΔU ) significantly reflects the heat added or removed from the system. Internal energy can be found using steam tables which provide u_f (specific internal energy of the saturated liquid) and u_g (specific internal energy of the saturated vapor) at various pressures and temperatures.
For a two-phase mixture, the specific internal energy is determined as:
  • u = (1 - x) u_f + x u_g
where x is the quality of the mixture. To calculate the change in internal energy during heating, we need to find the internal energy values at the start and end states. The change in internal energy ( ΔU ) can then be computed by:
  • ΔU = m(u_2 - u_1)
where m is the mass of the substance, u_1 is the initial specific internal energy, and u_2 is the specific internal energy at the final state.
steam tables
Steam tables are essential in solving thermodynamics problems involving water and steam. They provide the properties of water in both liquid and vapor phases at various temperatures and pressures.
These properties include specific volume ( v ), specific internal energy ( u ), specific enthalpy ( h ), and specific entropy ( s ), for both the liquid phase (denoted by the subscript f ) and the vapor phase (denoted by the subscript g ).
For example, steam tables help us find:
  • v_f and v_g : Specific volumes of liquid and vapor phases, respectively.
  • u_f and u_g : Specific internal energies of liquid and vapor phases, respectively.
  • h_f and h_g : Specific enthalpies of liquid and vapor phases, respectively.
When dealing with a two-phase mixture, we use these values to interpolate between the liquid and vapor states depending on the quality ( x ) of the mixture. Therefore, steam tables are a vital tool in determining the thermodynamic properties required to analyze processes involving heating, compression, and other changes of state.

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Most popular questions from this chapter

Figure P4.8 shows a mixing tank initially containing \(2000 \mathrm{lb}\) of liquid water. The tank is fitted with two inlet pipes, one delivering hot water at a mass flow rate of \(0.8 \mathrm{lb} / \mathrm{s}\) and the other delivering cold water at a mass flow rate of \(1.2 \mathrm{lb} / \mathrm{s}\). Water exits through a single exit pipe at a mass flow rate of \(2.5 \mathrm{lb} / \mathrm{s}\). Determine the amount of water, in lb, in the tank after one hour.

Air enters a compressor operating at steady state with a pressure of \(14.7 \mathrm{lbf} / \mathrm{in}^{2}\) and a temperature of \(70^{\circ} \mathrm{F}\). The volumetric flow rate at the inlet is \(16.6 \mathrm{ft}^{3} / \mathrm{s}\), and the flow area is \(0.26 \mathrm{ft}^{2}\). At the exit, the pressure is \(35 \mathrm{lbf} / \mathrm{in}^{2}\), the temperature is \(280^{\circ} \mathrm{F}\), and the velocity is \(50 \mathrm{ft} / \mathrm{s}\). Heat transfer from the compressor to its surroundings is \(1.0 \mathrm{Btu}\) per \(\mathrm{lb}\) of air flowing. Potential energy effects are negligible, and the ideal gas model can be assumed for the air. Determine (a) the velocity of the air at the inlet, in \(\mathrm{ft} / \mathrm{s}\), (b) the mass flow rate, in \(\mathrm{lb} / \mathrm{s}\), and (c) the compressor power, in Btu/s and hp.

The procedure to inflate a hot-air balloon requires a fan to move an initial amount of air into the balloon envelope followed by heat transfer from a propane burner to complete the inflation process. After a fan operates for 10 minutes with negligible heat transfer with the surroundings, the air in an initially deflated balloon achieves a temperature of \(80^{\circ} \mathrm{F}\) and a volume of \(49,100 \mathrm{ft}^{3}\). Next the propane burner provides heat transfer as air continues to flow into the balloon without use of the fan until the air in the balloon reaches a volume of \(65,425 \mathrm{ft}^{3}\) and a temperature of \(210^{\circ} \mathrm{F}\). Air at \(77^{\circ} \mathrm{F}\) and \(14.7 \mathrm{lb} / 1 n^{2}\) surrounds the balloon. The net rate of heat transfer is \(7 \times 10^{6} \mathrm{Btu} / \mathrm{h}\). Ignoring effects due to kinetic and potential energy, modeling the air as an ideal gas, and assuming the pressure of the air inside the balloon remains the same as that of the surrounding air, determine (a) the power required by the fan, in hp. (b) the time required for full inflation of the balloon, in min.

Figure P4.101 shows a pumped-hydro energy storage system delivering water at steady state from a lower reservoir to an upper reservoir using off-peak electricity (see Sec. 4.8.3). Water is delivered to the upper reservoir at a volumetric flow rate of \(150 \mathrm{~m}^{3} / \mathrm{s}\) with an increase in elevation of \(20 \mathrm{~m}\). There is no significant change in temperature, pressure, or kinetic energy from inlet to exit. Heat transfer from the pump to its surroundings occurs at a rate of \(0.6 \mathrm{MW}\) and \(g=9.81 \mathrm{~m} / \mathrm{s}^{2}\). Determine the pump power required, in MW. Assuming the same volumetric flow rate when the system generates on-peak electricity using this water, will the power be greater, less, or the same as the pump power? Explain.

Refrigerant 134 a enters a water-jacketed compressor operating at steady state at \(-10^{\circ} \mathrm{C}, 1.4\) bar, with a mass flow rate of \(4.2 \mathrm{~kg} / \mathrm{s}\), and exits at \(50^{\circ} \mathrm{C}, 12\) bar. The compressor power required is \(150 \mathrm{~kW}\). Neglecting kinetic and potential energy effects, determine the rate of heat transfer to the cooling water circulating through the water jacket.

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