/*! 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 66 The Clean Air Act prohibited the... [FREE SOLUTION] | 91影视

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The Clean Air Act prohibited the production of chlorofluorocarbons (CFCs) in the United States as of 1996. One widely used \(\mathrm{CFC}\), refrigerant \(\mathrm{R}-12\), has been replaced by \(\mathrm{R}-134 \mathrm{a}\) in many applications because of their similar properties, including a low boiling point at atmospheric pressure, \(T_{\text {sat }}=243 \mathrm{~K}\) and \(246.9 \mathrm{~K}\) for \(\mathrm{R}-12\) and \(\mathrm{R}-134 \mathrm{a}\), respectively. Compare the performance of these two refrigerants under the following conditions. The saturated refrigerant vapor at \(310 \mathrm{~K}\) is condensed as it flows through a 30 -mmdiameter, 0.8-m-long tube whose wall temperature is maintained at \(290 \mathrm{~K}\). If vapor enters the tube at a flow rate of \(0.010 \mathrm{~kg} / \mathrm{s}\), what is the rate of condensation and the flow rate of vapor leaving the tube? The relevant properties of \(\mathrm{R}-12\) at \(T_{\text {et }}=310 \mathrm{~K}\) are \(\rho_{e}=50.1 \mathrm{~kg} / \mathrm{m}^{3}\), \(h_{f s}=160 \mathrm{~kJ} / \mathrm{kg}\), and \(\mu_{v}=150 \times 10^{-7} \mathrm{~N} \cdot \mathrm{s} / \mathrm{m}^{2}\) and those of liquid \(\mathrm{R}-12\) at \(T_{f}=300 \mathrm{~K}\) are \(\rho_{l}=1306\) \(\mathrm{kg} / \mathrm{m}^{3}, c_{p,}=978 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, \mu_{I}=2.54 \times 10^{-4} \mathrm{~N} \cdot \mathrm{s} / \mathrm{m}^{2}\), \(k_{l}=0.072 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The properties of the saturated \(\mathrm{R}-134 \mathrm{a}\) vapor are \(\rho_{v}=46.1 \mathrm{~kg} / \mathrm{m}^{3}, h_{f 8}=166 \mathrm{~kJ} / \mathrm{kg}\), and \(\mu_{v}=136 \times 10^{-7} \mathrm{~N} \cdot \mathrm{s} / \mathrm{m}^{2}\).

Short Answer

Expert verified
In conclusion, under the given conditions, both refrigerants R-12 and R-134a have relatively similar performance. For R-12, the rate of condensation is \(7.5 \times 10^{-4}\, kg/s\) and the flow rate of vapor leaving the tube is \(9.25 \times 10^{-3}\, kg/s\). For R-134a, the rate of condensation is \(7.23 \times 10^{-4}\, kg/s\) and the flow rate of vapor leaving the tube is \(9.27 \times 10^{-3}\, kg/s\). Both refrigerants perform closely during the condensation process in the tube.

Step by step solution

01

Find the Tube鈥檚 Cross-Sectional Area

The tube has a diameter of 30 mm (0.03 m) and is 0.8 meters long. The cross-sectional area (A) can be calculated using the following formula: \[A = \dfrac{\pi d^2}{4}\] where d is the diameter of the tube. Plugging in the given diameter: \[A = \dfrac{\pi(0.03)^2}{4} = 7.07 \times 10^{-4} m^2\]
02

Calculate the Initial Vapor Velocities

We can find the initial vapor velocities (V) for both refrigerants using the following formula: \[V = \dfrac{m}{\rho A}\] where m is the mass flow rate (0.010 kg/s), 蟻 is the vapor density, and A is the cross-sectional area. For R-12: \[V_{R-12} = \dfrac{0.010}{50.1 \times 7.07 \times 10^{-4}} = 0.2828\, m/s\] For R-134a: \[V_{R-134a} = \dfrac{0.010}{46.1 \times 7.07 \times 10^{-4}} = 0.3055\, m/s\]
03

Calculate the Reynolds Numbers

We will now calculate the Reynolds numbers (Re) for both refrigerants, which will determine if the flow is laminar or turbulent. \[Re = \dfrac{VD}{\mu}\] For R-12: \[Re_{R-12} = \dfrac{0.2828 \times 0.03}{150\times10^{-7}} = 5656.67\] For R-134a: \[Re_{R-134a} = \dfrac{0.3055 \times 0.03}{136\times10^{-7}} = 6738.97\]
04

Calculate Heat Transfer Coefficients

We will now evaluate the Nusselt numbers (Nu) and heat transfer coefficients (h) for both refrigerants. Since the Reynolds numbers are less than 10,000 for both refrigerants, we can assume the flow is laminar and use the Nusselt number for a laminar flow: \[Nu = 3.66\] We can calculate the heat transfer coefficient using the following formula: \[h = \dfrac{Nu \times k}{D}\] For R-12, the thermal conductivity (k) is 0.072 W/(m路K): \[h_{R-12} = \dfrac{3.66 \times 0.072}{0.03} = 8.793 W/(m^2\cdot K)\] For R-134a, the thermal conductivity (k) is assumed to be approximately the same as R-12 (0.072 W/(m路K)): \[h_{R-134a} = \dfrac{3.66 \times 0.072}{0.03} = 8.793 W/(m^2\cdot K)\]
05

Determine the Area of Heat Transfer and Overall Heat Transfer Rate

The area for heat transfer (As) is the product of the tube's circumference and its length: \[As = \pi D L\] where D is the diameter, and L is the length. Using the given parameters: \[As = \pi (0.03)(0.8) = 0.0754\, m^2\] Next, we can calculate the overall heat transfer rate (Q) for both refrigerants: \[Q = h As (T_e - T_w)\] where Te is the vapor entry temperature, and Tw is the tube wall temperature. For R-12: \[Q_{R-12} = 8.793 \times 0.0754 \times (310-290) = 119.99 W\] For R-134a: \[Q_{R-134a} = 8.793 \times 0.0754 \times (310-290) = 119.99 W\]
06

Calculate the Rate of Condensation and Flow Rate

We will finally calculate the rate of condensation (螖m) and the flow rate of vapor leaving the tube (m_out) for both refrigerants. The rate of condensation can be calculated using the following formula: \[\Delta m = \dfrac{Q}{h_{fg}}\] For R-12: \[\Delta m_{R-12} = \dfrac{119.99}{160 \times 10^3} = 7.5 \times 10^{-4} kg/s\] For R-134a: \[\Delta m_{R-134a} = \dfrac{119.99}{166 \times 10^3} = 7.23 \times 10^{-4} kg/s\] The flow rate of vapor leaving the tube can be calculated using: \[m_{out} = m - \Delta m\] For R-12: \[m_{out,R-12} = 0.010 - 7.5 \times 10^{-4} = 9.25 \times 10^{-3} kg/s\] For R-134a: \[m_{out,R-134a} = 0.010 - 7.23 \times 10^{-4} = 9.27 \times 10^{-3} kg/s\] In conclusion, the rate of condensation is 7.5 x 10^{-4} kg/s and the flow rate of vapor leaving the tube for R-12 is 9.25 x 10^{-3} kg/s. For R-134a, the rate of condensation is 7.23 x 10^{-4} kg/s, and the flow rate of vapor leaving the tube is 9.27 x 10^{-3} kg/s. Both refrigerants have relatively similar performance under these conditions.

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Key Concepts

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

Condensation Rate in Refrigeration Systems
Understanding the condensation rate is crucial when studying refrigeration systems. The condensation rate refers to the speed at which a refrigerant vapor changes phase to become a liquid within the refrigeration cycle. This process occurs in the condenser, where heat is rejected from the refrigerant, allowing it to condense.

In the example exercise, the rate of condensation is determined by evaluating the overall heat transfer rate and the latent heat of vaporization (referred to as \(h_{fg}\) in thermodynamics). The heat transfer rate, represented by \(Q\), calculated in Step 5 of the solution, is directly related to the rate of condensation (\(\Delta m\)) since the heat removed from the refrigerant vapor causes it to condense. The formula \(\Delta m = \frac{Q}{h_{fg}}\) from Step 6 quantifies this relationship.

For the refrigerants R-12 and R-134a, despite their different properties, the calculation results reveal that the rate of condensation is very close, illustrating how similar refrigerants can behave under identical operating conditions. This highlights the importance of selecting a refrigerant with the right properties for efficient system design and operation.
Refrigerant Properties & Performance
Refrigerant properties greatly influence the performance of refrigeration systems. As indicated by the Clean Air Act, traditional refrigerants like \(\mathrm{R}-12\) were phased out due to their adverse environmental impact, prompting the use of substitutes like \(\mathrm{R}-134\mathrm{a}\) that have similar thermodynamic properties but are less harmful to the ozone layer.

The properties mentioned in the problem, such as density (\(\rho\)), specific heat (\(c_{p}\)), dynamic viscosity (\(\mu\)), and thermal conductivity (\(k\)), directly affect heat transfer rates, pressure drops, and energy efficiency. For instance, the density of the vapor influences the velocity at which it flows through the condenser, while the specific heat and thermal conductivity define the refrigerant's capacity to absorb and conduct heat. Additionally, the dynamic viscosity affects the refrigerant鈥檚 flow characteristics through the refrigeration cycle.

This mix of properties must be carefully balanced to achieve optimal refrigeration system performance. In the exercise, by comparing the properties at the same conditions and measuring their effect on condensation rates, students can learn how even slight differences in properties can change the behavior of the refrigeration cycle.
Nusselt Number & Heat Transfer
The Nusselt number (Nu) is a dimensionless parameter essential for characterizing convective heat transfer within a fluid. Essentially, it correlates the convective to conductive heat transfer occurring at a boundary in a fluid flow. In refrigeration systems, the Nusselt number aids in determining the effectiveness of the heat transfer process during the condensation of the refrigerant within the tubes of the condenser.

Step 4 of the problem-solving exercise involves calculating this important number. Given the laminar flow conditions (based on the calculated Reynolds numbers), a Nusselt number of 3.66 is used to estimate the heat transfer coefficient (\(h\)) for both refrigerants. The formula \(h = \frac{Nu \times k}{D}\) incorporates the Nusselt number, thermal conductivity, and diameter of the tube to calculate this coefficient. A higher Nusselt number would signify a more efficient heat transfer from the refrigerant vapor to the tube walls, resulting in a higher condensation rate.

Understanding how the Nusselt number affects the heat transfer rate is imperative for designing efficient refrigeration systems. This value, alongside other properties of the refrigerant, contribute to determining the size and type of condenser required for a specific refrigeration application.

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Most popular questions from this chapter

A thin-walled cylindrical container of diameter \(D\) and height \(L\) is filled to a height \(y\) with a low boiling point liquid (A) at \(T_{\text {e.a. }}\). The container is located in a large chamber filled with the vapor of a high boiling point fluid (B). Vapor-B condenses into a laminar film on the outer surface of the cylindrical container, extending from the location of the liquid-A free surface. The condensation process sustains nucleate boiling in liquid-A along the container wall according to the relation \(q^{n}=\) \(C\left(T_{x}-T_{\text {sat }}\right)^{3}\), where \(C\) is a known empirical constant. (a) For the portion of the wall covered with the condensate film, derive an equation for the average temperature of the container wall, \(T_{x}\). Assume that the properties of fluids \(A\) and \(B\) are known. (b) At what rate is heat supplied to liquid-A? (c) Assuming the container is initially filled completely with liquid, that is, \(y=L\), derive an expression for the time required to evaporate all the liquid in the container.

The condenser of a steam power plant consists of AISI 302 stainless steel tubes \(\left(k_{s}=15 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)\), each of outer and inner diameters \(D_{o}=30 \mathrm{~mm}\) and \(D_{i}=\) \(26 \mathrm{~mm}\), respectively. Saturated steam at \(0.135\) bar condenses on the outer surface of a tube, while water at a mean temperature of \(T_{m}=290 \mathrm{~K}\) is in fully developed flow through the tube. (a) For a water flow rate of \(\dot{m}=0.25 \mathrm{~kg} / \mathrm{s}\), what is the outer surface temperature \(T_{s, o}\) of the tube and the rates of heat transfer and steam condensation per unit tube length? As a first estimate, you may evaluate the properties of the liquid film at the saturation temperature. If one wishes to increase the transfer rates, what is the limiting factor that should be addressed? (b) Explore the effect of the water flow rate on \(T_{s, o}\) and the rate of heat transfer per unit length.

A heater for boiling a saturated liquid consists of two concentric stainless steel tubes packed with dense boron nitride powder. Electrical current is passed through the inner tube, creating uniform volumetric heating \(\dot{q}\) \(\left(\mathrm{W} / \mathrm{m}^{3}\right)\). The exposed surface of the outer tube is in contact with the liquid and the boiling heat flux is given as $$ q_{s}^{\prime \prime}=C\left(T_{s}-T_{\text {sat }}\right)^{3} $$ It is feared that under high-power operation the stainless steel tubes would severely oxidize if temperatures exceed \(T_{s s, x}\) or that the boron nitride would deteriorate if its temperature exceeds \(T_{\mathrm{bn}, x^{*}}\) Presuming that the saturation temperature of the liquid \(\left(T_{\text {sat }}\right)\) and the boiling surface temperature \(\left(T_{x}\right)\) are prescribed, derive expressions for the maximum temperatures in the stainless steel (ss) tubes and in the boron nitride (bn). Express your results in terms of geometric parameters \(\left(r_{1}, r_{2}\right.\), \(\left.r_{3}, r_{4}\right)\), thermal conductivities \(\left(k_{\mathrm{ss}}, k_{\mathrm{ba}}\right)\), and the boiling parameters \(\left(C, T_{\text {sial }}, T_{s}\right)\).

A l-mm-diameter horizontal platinum wire of emissivity \(\varepsilon=0.25\) is operated in saturated water at 1 -atm pressure. (a) What is the surface heat flux if the surface temperature is \(T_{s}=800 \mathrm{~K}\) ? (b) For emissivities of \(0.1,0.25\), and \(0.95\), generate a \(\log -\log\) plot of the heat flux as a function of surface excess temperature, \(\Delta T_{e} \equiv T_{s}-T_{\text {stit }}\), for \(150 \leq \Delta T_{e} \leq 550 \mathrm{~K}\). Show the critical heat flux and the Leidenfrost point on your plot. Separately, plot the percentage contribution of radiation to the total heat flux for \(150 \leq \Delta T_{e} \leq 550 \mathrm{~K}\).

A technique for cooling a multichip module involves submerging the module in a saturated fluorocarbon liquid. Vapor generated due to boiling at the module surface is condensed on the outer surface of copper tubing suspended in the vapor space above the liquid. The thin-walled tubing is of diameter \(D=10 \mathrm{~mm}\) and is coiled in a horizontal plane. It is cooled by water that enters at \(285 \mathrm{~K}\) and leaves at \(315 \mathrm{~K}\). All the heat dissipated by the chips within the module is transferred from a \(100-\mathrm{mm} \times 100-\mathrm{mm}\) boiling surface, at which the flux is \(10^{5} \mathrm{~W} / \mathrm{m}^{2}\), to the fluorocarbon liquid, which is at \(T_{\text {sait }}=57^{\circ} \mathrm{C}\). Liquid properties are \(k_{l}=0.0537\) \(\mathrm{W} / \mathrm{m} \cdot \mathrm{K}, c_{p, l}=1100 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, h_{f g}^{\prime} \approx h_{f g}=84,400 \mathrm{~J} / \mathrm{kg}\), \(\rho_{l}=1619.2 \mathrm{~kg} / \mathrm{m}^{3}, \rho_{v}=13.4 \mathrm{~kg} / \mathrm{m}^{3}, \sigma=8.1 \times 10^{-3}\) \(\mathrm{N} / \mathrm{m}, \mu_{l}=440 \times 10^{-6} \mathrm{~kg} / \mathrm{m} \cdot \mathrm{s}\), and \(P r_{l}=9\). (a) For the prescribed heat dissipation, what is the required condensation rate \((\mathrm{kg} / \mathrm{s})\) and water flow rate \((\mathrm{kg} / \mathrm{s})\) ? (b) Assuming fully developed flow throughout the tube, determine the tube surface temperature at the coil inlet and outlet. (c) Assuming a uniform tube surface temperature of \(T_{s}=53.0^{\circ} \mathrm{C}\), determine the required length of the coil.

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