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The condenser of a room air conditioner is designed to reject heat at a rate of \(15,000 \mathrm{~kJ} / \mathrm{h}\) from refrigerant-134a as the refrigerant is condensed at a temperature of \(40^{\circ} \mathrm{C}\). Air \(\left(c_{p}=1005 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) flows across the finned condenser coils, entering at \(25^{\circ} \mathrm{C}\) and leaving at \(35^{\circ} \mathrm{C}\). If the overall heat transfer coefficient based on the refrigerant side is \(150 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the heat transfer area on the refrigerant side.

Short Answer

Expert verified
Answer: The heat transfer area on the refrigerant side is approximately 2.78 m².

Step by step solution

01

Convert heat rejection rate to Watts

We are given that the heat rejection rate is \(15,000 \mathrm{~kJ} / \mathrm{h}\). To convert this value to Watts, we will use the following conversion factors: 1 kJ = 1000 J 1 h = 3600 s So, the heat rejection rate in Watts can be calculated as: Heat rejection rate (W) = \(\dfrac{15,000 \times 1000}{3600} \mathrm{~W} = 4166.67 \mathrm{~W}\)
02

Calculate the temperature difference

We are given that the air enters the condenser at a temperature of \(25^{\circ} \mathrm{C}\) and leaves at \(35^{\circ} \mathrm{C}\). Since the refrigerant is at a constant temperature of \(40^{\circ} \mathrm{C}\), the average temperature difference between the refrigerant and the air is: Temperature difference (\(\Delta T\)) = \(\dfrac{(40 - 25) + (40 - 35)}{2} = \dfrac{15 + 5}{2} = 10^{\circ} \mathrm{C}\)
03

Apply the heat transfer equation

The rate of heat transfer (\(Q\)) can be written as: \(Q = U \cdot A \cdot \Delta T\) where: - \(Q\): heat transfer rate - \(U\): overall heat transfer coefficient - \(A\): heat transfer area - \(\Delta T\): temperature difference between the refrigerant and the air We need to find the heat transfer area \(A\). So, we will rearrange the equation above to get: \(A = \dfrac{Q}{U \cdot \Delta T}\) Now, we can substitute the values we have found in Step 1 and Step 2, and the given overall heat transfer coefficient, into the equation above to calculate the heat transfer area: \(A = \dfrac{4166.67}{150 \cdot 10} = \dfrac{4166.67}{1500} = 2.78 \mathrm{~m}^2\)
04

Final answer for heat transfer area

The heat transfer area on the refrigerant side is approximately 2.78 square meters.

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Key Concepts

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

Refrigerant-134a
Refrigerant-134a is a commonly used refrigerant in many air conditioning and refrigeration systems. Developed as a replacement for older refrigerants, it offers several benefits including low toxicity, non-flammability, and relatively lower Global Warming Potential (GWP) compared to its predecessors. Understanding Refrigerant-134a is key, especially when dealing with heat transfer scenarios in equipment like a condenser. In the exercise, as the refrigerant condenses at a temperature of 40°C, it reaches a phase change. This phase change is crucial for efficient heat rejection, as it allows substantial amounts of heat to be rejected without large changes in temperature, maintaining optimal performance of the cooling system.
Overall Heat Transfer Coefficient
The overall heat transfer coefficient (U) is a measure of a system's ability to conduct heat. For our exercise, U is given as 150 W/m²·K. This coefficient combines all the resistances to heat flow throughout different layers and interfaces. The concept can be likened to how well a thermal "blanket" lets heat pass through, considering all materials involved. The higher the value, the better the system is at transferring heat. This coefficient is vital in determining the necessary heat transfer area in the condenser design, directly influencing efficiency. So, understanding and calculating U helps in designing systems that can effectively handle or reject heat, guiding the design of components like a condenser.
Temperature Difference
Temperature difference (\(\Delta T\)) is a critical factor in the heat transfer process. It represents the driving force for heat flow from the hot refrigerant to the cooler air. In the given problem, \(\Delta T\) is calculated by averaging the difference between the refrigerant temperature (40°C) and the temperatures of air entering (25°C) and leaving (35°C) the system. This average temperature difference, calculated as 10°C, reflects the effective difference that influences the rate of heat transfer. The bigger the temperature difference, the more efficient the heat transfer process becomes. Recognizing and calculating this difference ensures that the condenser operates at its design intent, maximizing heat rejection efficiency.
Condenser Design
Designing a condenser involves carefully balancing various parameters to ensure efficient heat rejection. In the context of this exercise, the design primarily focuses on the heat transfer area required based on the overall heat transfer coefficient and the temperature difference. A well-designed condenser effectively removes unwanted heat from the refrigerant, allowing it to cool and condense. This involves using appropriate materials with high thermal conductivity, optimal fin design for enhanced air flow, and calculating the precise surface area needed. Here, we calculated a heat transfer area of approximately 2.78 m². Such calculations are fundamental in ensuring that the condenser runs efficiently, as they allow for appropriate sizing and selection of materials, enhancing system reliability and performance.

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Most popular questions from this chapter

How is the NTU of a heat exchanger defined? What does it represent? Is a heat exchanger with a very large NTU \((\) say, 10\()\) necessarily a good one to buy?

Hot oil \(\left(c_{p}=2200 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) is to be cooled by water \(\left(c_{p}=4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) in a 2 -shell-passes and 12 -tube-passes heat exchanger. The tubes are thin-walled and are made of copper with a diameter of \(1.8 \mathrm{~cm}\). The length of each tube pass in the heat exchanger is \(3 \mathrm{~m}\), and the overall heat transfer coefficient is \(340 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). Water flows through the tubes at a total rate of \(0.1 \mathrm{~kg} / \mathrm{s}\), and the oil through the shell at a rate of \(0.2 \mathrm{~kg} / \mathrm{s}\). The water and the oil enter at temperatures \(18^{\circ} \mathrm{C}\) and \(160^{\circ} \mathrm{C}\), respectively. Determine the rate of heat transfer in the heat exchanger and the outlet temperatures of the water and the oil.

Hot water coming from the engine is to be cooled by ambient air in a car radiator. The aluminum tubes in which the water flows have a diameter of \(4 \mathrm{~cm}\) and negligible thickness. Fins are attached on the outer surface of the tubes in order to increase the heat transfer surface area on the air side. The heat transfer coefficients on the inner and outer surfaces are 2000 and \(150 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), respectively. If the effective surface area on the finned side is 10 times the inner surface area, the overall heat transfer coefficient of this heat exchanger based on the inner surface area is (a) \(150 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (b) \(857 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (c) \(1075 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (d) \(2000 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (e) \(2150 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\)

Consider an oil-to-oil double-pipe heat exchanger whose flow arrangement is not known. The temperature measurements indicate that the cold oil enters at \(20^{\circ} \mathrm{C}\) and leaves at \(55^{\circ} \mathrm{C}\), while the hot oil enters at \(80^{\circ} \mathrm{C}\) and leaves at \(45^{\circ} \mathrm{C}\). Do you think this is a parallel-flow or counter-flow heat exchanger? Why? Assuming the mass flow rates of both fluids to be identical, determine the effectiveness of this heat exchanger.

A shell-and-tube process heater is to be selected to heat water \(\left(c_{p}=4190 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) from \(20^{\circ} \mathrm{C}\) to \(90^{\circ} \mathrm{C}\) by steam flowing on the shell side. The heat transfer load of the heater is \(600 \mathrm{~kW}\). If the inner diameter of the tubes is \(1 \mathrm{~cm}\) and the velocity of water is not to exceed \(3 \mathrm{~m} / \mathrm{s}\), determine how many tubes need to be used in the heat exchanger.

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