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Refrigerant \(134 a\) enters the evaporator of a refrigeration system operating at steady state at \(-4^{\circ} \mathrm{C}\) and quality of \(20 \%\) at a velocity of \(7 \mathrm{~m} / \mathrm{s}\). At the exit, the refrigerant is a saturated vapor at a temperature of \(-4^{\circ} \mathrm{C}\). The evaporator flow channel has constant diameter. If the mass flow rate of the entering refrigerant is \(0.1 \mathrm{~kg} / \mathrm{s}\), determine (a) the diameter of the evaporator flow channel, in \(\mathrm{cm}\). (b) the velocity at the exit, in \(\mathrm{m} / \mathrm{s}\).

Short Answer

Expert verified
Diameter of the flow channel is 1.15 cm and exit velocity is 1.07 m/s.

Step by step solution

01

- Determine the specific volumes

First, find the specific volumes of the refrigerant at the inlet and the outlet. The specific volume for refrigerant 134a at \(-4^{\text{°}} \text{C} \text{ and vapor quality } (\text{quality of 20%})\) can be found using the equation: \(v = vf + x(vg - vf)\), where \(v\) (specific volume),\( x = 0.2 )\),\( v_f = 0.000736 \text{ m}^3/\text{kg}\), and\( v_g = 0.19409 \text{ m}^3/\text{kg}\).
02

- Calculate the specific volume at inlet

Using the values from thermodynamic tables,\(v_f = 0.000736 \text{ m}^3/\text{kg}\) and\(v_g = 0.19409 \text{ m}^3/\text{kg}\):\[v_{inlet} = 0.000736 + 0.2(0.19409 - 0.000736)\]\[v_{inlet} = 0.00144 \text{ m}^3/\text{kg}\]
03

- Express continuity equation at inlet

Use the mass flow rate formula to express the continuity equation at the inlet:\[ \text{mass flow rate} (m) = \rho \times \text{cross-sectional area} (A) \times \text{velocity} (V) \]\[ \rho = \frac{1}{v} \]\[ 0.1~kg/s = \frac{1}{0.00144 \text{ m}^3/\text{kg}} \times \frac{\begin{pi} * D^2}{4} (7 m/s)\]
04

- Solve for the diameter

Solving for the diameter (D) of the evaporator flow channel, we get:\[ 0.1 = \frac{1}{0.00144} \times \frac{\begin{pi} * D^2}{4} \times(7)\]Solving for \(D\) gives \(\text{D} = 1.15 \text{ cm}\)
05

- Use continuity equation at exit

For the exit, use the continuity equation with the known mass flow rate, cross-sectional area, and unknown velocity:\[ v_{exit} = v_g\ = 0.19409 \text{ m}^3/\text{kg}\]\[\text{mass flow rate} = \rho_{exit}\times A\times V_{exit}\] \[0.1~kg/s = \frac{1}{0.19409} * \frac{\begin{pi} * D^2}{4}\times V_{exit}\]
06

- Solve for the exit velocity

Solving for exit velocity \(V_{exit}\) with \(D = 0.0115 \text{ m}\) gives:\[0.1 = \frac{1}{0.19409} * \frac{\begin{pi} * (0.0115^2)}{4}\times V_{exit}\]Thus, the exit velocity,\(V_{exit}= 1.07 m/s\)

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Key Concepts

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

Specific Volume
In the study of refrigeration systems, the specific volume is a critical concept. It measures the volume occupied by a unit mass of a substance. This property is essential for calculating other parameters like density and for solving problems involving fluid flow and heat transfer. In this exercise, the specific volume helps us determine different states of the refrigerant.
For refrigerant 134a at \(-4^{\text{°}}\text{C}\) and a vapor quality of \(20\text{%}\), we use \(v = v_f + x(v_g - v_f)\), where \(v_f\) is the specific volume of the liquid-phase refrigerant, and \(v_g\) is the specific volume in the vapor phase. The quality (\(x\)) represents the fraction of the refrigerant mass that is vapor. After substituting the values from the thermodynamic tables (\(v_f = 0.000736 \text{ m}^3/\text{kg}\) and \(v_g = 0.19409 \text{ m}^3/\text{kg}\)), we calculate the specific volume at the inlet as: \(v_{\text{inlet}} = 0.000736 + 0.2(0.19409 - 0.000736) = 0.00144 \text{ m}^3/\text{kg}\)
Understanding specific volume helps us track the refrigerant's behavior through different phases and temperatures within the refrigeration cycle.
Continuity Equation
The continuity equation is crucial for analyzing fluid flow in refrigeration systems. It ensures that mass is conserved in the system. For a steady-state process (no accumulation of mass), the mass flow rate entering a system equals the mass flow rate exiting the system.
Mathematically, it's expressed as: \(m = \rho \times A \times V\), where \(m\) is mass flow rate, \(\rho\) is density, \(A\) is cross-sectional area, and \(V\) is velocity. Using the specific volume (\(v\)) to find density (\(\rho\)), we have \(\rho = \frac{1}{v}\).
In this exercise, using the continuity equation at the inlet:\(0.1 \text{ kg/s} = \frac{1}{0.00144 \text{ m}^3/\text{kg}} \times \frac{\begin{pi} * D^2}{4} \times 7 \text{ m/s}\) we can solve for the diameter of the evaporator flow channel as:\(D = 1.15 \text{ cm}\).
At the exit, we use: \(0.1 \text{ kg/s} = \frac{1}{0.19409} \times \frac{\begin{pi} * D^2}{4} \times V_{\text{exit}}\) and solving for the exit velocity gives:\(V_{\text{exit}} = 1.07 \text{ m/s}\). Therefore, the continuity equation provides a framework for solving fluid dynamic problems by relating these quantities.
Evaporator Flow Channel
The evaporator flow channel is an integral part of the refrigeration system. It is where the refrigerant absorbs heat, leading to its phase change from a liquid to a vapor. This process occurs at a nearly constant temperature and pressure, known as the evaporation point.
In this exercise, the diameter of the evaporator flow channel remains constant, making calculations more straightforward. Given the mass flow rate and the specific volumes at both the inlet and the outlet, the continuity equation allows us to determine both the diameter of the channel and the velocity of the refrigerant at different points.
Knowing these values ensures the system can be designed to optimize the refrigerant's flow and heat absorption, leading to better performance and efficiency in the refrigeration cycle. Properly analyzing the evaporator flow channel plays a vital role in enhancing the overall design and functionality of a refrigeration system.

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Most popular questions from this chapter

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.

At steady state, air at \(200 \mathrm{kPa}, 325 \mathrm{~K}\), and mass flow rate of \(0.5 \mathrm{~kg} / \mathrm{s}\) enters an insulated duct having differing inlet and exit cross-sectional areas The inlet cross-sectional area is \(6 \mathrm{~cm}^{2}\). At the duct exit, the pressure of the air is \(100 \mathrm{kPa}\) and the velocity is \(250 \mathrm{~m} / \mathrm{s}\). Neglecting potential energy effects and modeling air as an ideal gas with constant \(c_{p}=\) \(1.008 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}\), determine (a) the velocity of the air at the inlet, in \(\mathrm{m} / \mathrm{s}\). (b) the temperature of the air at the exit, in \(\mathrm{K}\). (c) the exit cross-sectional area, in \(\mathrm{cm}^{2}\).

Air modeled as an ideal gas enters a combustion chamber at \(20 \mathrm{lbf} / \mathrm{in}^{2}\) and \(70^{\circ} \mathrm{F}\) through a rectangular duct, \(5 \mathrm{ft}\) by \(4 \mathrm{ft}\). If the mass flow rate of the air is \(830,000 \mathrm{lb} / \mathrm{h}\), determine the velocity, in \(\mathrm{ft} / \mathrm{s}\).

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.

Air enters a diffuser operating at steady state at \(540^{\circ} \mathrm{R}\), 15 lbf/in. \({ }^{2}\), with a velocity of \(600 \mathrm{ft} / \mathrm{s}\), and exits with a velocity of \(60 \mathrm{ft} / \mathrm{s}\). The ratio of the exit area to the inlet area is 8 . Assuming the ideal gas model for the air and ignoring heat transfer, determine the temperature, in \({ }^{\circ} \mathrm{R}\), and pressure, in lbf/in. \({ }^{2}\), at the exit.

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