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Engine oil \(\left(c_{p}=2100 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) is to be heated from \(20^{\circ} \mathrm{C}\) to \(60^{\circ} \mathrm{C}\) at a rate of \(0.3 \mathrm{~kg} / \mathrm{s}\) in a \(2-\mathrm{cm}\)-diameter thinwalled copper tube by condensing steam outside at a temperature of \(130^{\circ} \mathrm{C}\left(h_{f g}=2174 \mathrm{~kJ} / \mathrm{kg}\right)\). For an overall heat transfer coefficient of \(650 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the rate of heat transfer and the length of the tube required to achieve it.

Short Answer

Expert verified
Answer: The required length of the copper tube is approximately 7.045 meters.

Step by step solution

01

Calculate the mass flow rate of engine oil.

Given, the flow rate of engine oil is \(0.3\ kg/s\).
02

Determine the heat transfer required by the engine oil to raise its temperature.

To find the heat transfer required to raise the temperature of engine oil from \(20^\circ C\) to \(60^\circ C\), we can use the formula: \(Q=mc_p\Delta T\) Where \(Q\) is the heat transfer, \(m\) is the mass flow rate of engine oil, \(c_p\) is the specific heat capacity and \(\Delta T\) is the change in temperature. Given \(m=0.3\ kg/s\), \(c_p=2100\ J/kg\cdot K\), and \(\Delta T = 60-20 = 40^\circ C\). Therefore, \(Q = (0.3)(2100)(40)= 25200\ W\).
03

Calculate the rate of heat transfer between the steam and engine oil.

We are given the overall heat transfer coefficient U as \(650\ W/m^2\cdot K\). Also, we know \(Q=U\cdot A\cdot\Delta T_{lm}\) where the area A is given by \(A = \pi d L\) and \(\Delta T_{lm}\) is the log mean temperature difference. First, we need to calculate the log mean temperature difference. The outlet temperature of the engine oil is given as \(60^\circ C\). Since the steam is at a constant temperature, the inlet temperature difference can be calculated as \(\Delta T_1 = 130 - 60 = 70^\circ C\). Similarly, the outlet temperature difference is \(\Delta T_2 = 130 - 20 = 110^\circ C\). Now, we can find the log mean temperature difference: \(\Delta T_{lm} = \frac{\Delta T_2 - \Delta T_1}{\ln(\Delta T_2/\Delta T_1)}=\frac{110-70}{\ln(110/70)} = 87.25^\circ C\)
04

Find the length of the copper tube required for the desired heat transfer.

We have the rate of heat transfer \(Q=25200\ W\) and \(\Delta T_{lm}=87.25^\circ C\). We can now solve for the area, \(A\) \(A = \frac{Q}{U\cdot \Delta T_{lm}}=\frac{25200}{650\cdot 87.25}=0.443\ m^2\) Now, we can find the length of the copper tube. We know the diameter of the tube is \(2\ \mathrm{cm} = 0.02\ \mathrm{m}\) and the area \(A=0.443\ \mathrm{m}^2\). \(L = \frac{A}{\pi d}=\frac{0.443}{\pi\cdot 0.02}=7.045\ m\) So, the length of the copper tube required to achieve the desired rate of heat transfer is approximately \(7.045\ \mathrm{m}\).

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Key Concepts

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

Engine Oil Heating
Heating engine oil involves raising its temperature to meet operational or process needs. In this exercise, the engine oil is heated from 20°C to 60°C, and understanding this process requires examining the energy required to achieve this temperature increase. This process occurs within a thin-walled copper tube where the oil is heated using condensing steam.

To heat the oil effectively, steam at a temperature of 130°C is utilized, condensing on the exterior of the tube. The heat from the steam transfers through the copper tube wall into the flowing engine oil, thus increasing its temperature. The specific parameters such as flow rate and diameter of the tube influence the heating process and determine the efficiency of heat transfer.
Specific Heat Capacity
Specific heat capacity, denoted as \( c_p \), is an important property that defines how much energy is required to change the temperature of a substance. For engine oil in this scenario, \( c_p = 2100 \ \mathrm{J/kg\cdot K} \). This value indicates how much heat energy is needed to raise the temperature of 1 kilogram of oil by 1 Kelvin.

To calculate the total amount of heat transfer \( Q \) needed to elevate the oil temperature from 20°C to 60°C, the formula used is:
  • \( Q = mc_p\Delta T \)
where \( m \) is the mass flow rate, \( \Delta T \) is the temperature change (which in this case, is 40°C), and \( c_p \) is the specific heat capacity. Hence, understanding the specific heat capacity allows us to quantify the amount of heat energy required for the oil's temperature increase.
Log Mean Temperature Difference
The log mean temperature difference (LMTD) is a crucial concept in determining the efficiency of heat exchangers, like the one used to heat engine oil. LMTD provides a weighted average temperature difference between the hot and cold fluids across the heat exchanger. In this setup, it considers the steam at 130°C and the engine oil, varying from 20°C to 60°C.

LMTD is calculated as:
  • \( \Delta T_{lm} = \frac{\Delta T_2 - \Delta T_1}{\ln(\Delta T_2/\Delta T_1)} \)
where \( \Delta T_1 \) is the temperature difference at the inlet, and \( \Delta T_2 \) at the outlet. For this example, \( \Delta T_1 = 70 \ \mathrm{°C} \) (130-60) and \( \Delta T_2 = 110 \ \mathrm{°C} \) (130-20), resulting in an LMTD of approximately 87.25°C. A higher LMTD indicates a greater potential for heat transfer, thus more efficient heating.
Heat Transfer Coefficient
The heat transfer coefficient \( U \) is a vital factor in determining how effectively heat is transferred through the heat exchanger. In this example, the heat transfer coefficient is given as \( 650 \ \mathrm{W/m^2\cdot K} \). This coefficient quantifies the heat transfer per unit area per degree of temperature difference between the fluids.

The formula for heat transfer \( Q \) including \( U \) and the LMTD is:
  • \( Q = U\cdot A\cdot\Delta T_{lm} \)
where \( A \) is the surface area of the tube. The heat transfer coefficient helps us calculate the tube's required length to achieve the desired heating, ensuring the engine oil reaches the correct temperature with optimum efficiency.

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Most popular questions from this chapter

There are two heat exchangers that can meet the heat transfer requirements of a facility. One is smaller and cheaper but requires a larger pump, while the other is larger and more expensive but has a smaller pressure drop and thus requires a smaller pump. Both heat exchangers have the same life expectancy and meet all other requirements. Explain which heat exchanger you would choose and under what conditions.

A shell-and-tube heat exchanger with 1-shell pass and 14-tube passes is used to heat water in the tubes with geothermal steam condensing at \(120^{\circ} \mathrm{C}\left(h_{f g}=2203 \mathrm{~kJ} / \mathrm{kg}\right)\) on the shell side. The tubes are thin-walled and have a diameter of \(2.4 \mathrm{~cm}\) and length of \(3.2 \mathrm{~m}\) per pass. Water \(\left(c_{p}=4180 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) enters the tubes at \(22^{\circ} \mathrm{C}\) at a rate of \(3.9 \mathrm{~kg} / \mathrm{s}\). If the temperature difference between the two fluids at the exit is \(46^{\circ} \mathrm{C}\), determine (a) the rate of heat transfer, \((b)\) the rate of condensation of steam, and \((c)\) the overall heat transfer coefficient.

Consider a condenser unit (shell and tube heat exchanger) of an HVAC facility where saturated refrigerant \(\mathrm{R} 134 \mathrm{a}\) at a saturation pressure of \(1318.6 \mathrm{kPa}\) and a rate of \(2.5 \mathrm{~kg} / \mathrm{s}\) flows through thin-walled copper tubes. The refrigerant enters the condenser as saturated vapor and it is desired to have a saturated liquid refrigerant at the exit. The cooling of refrigerant is carried out by cold water that enters the heat exchanger at \(10^{\circ} \mathrm{C}\) and exits at \(40^{\circ} \mathrm{C}\). Assuming initial overall heat transfer coefficient of the heat exchanger to be \(3500 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\), determine the surface area of the heat exchanger and the mass flow rate of cooling water for complete condensation of the refrigerant. In practice, over a long period of time, fouling occurs inside the heat exchanger that reduces its overall heat transfer coefficient and causes the mass flow rate of cooling water to increase. Increase in the mass flow rate of cooling water will require additional pumping power making the heat exchange process uneconomical. To prevent the condenser unit from under performance, assume that fouling has occurred inside the heat exchanger and has reduced its overall heat transfer coefficient by \(20 \%\). For the same inlet temperature and flow rate of refrigerant, determine the new flow rate of cooling water to ensure complete condensation of the refrigerant at the heat exchanger exit.

A 1-shell-pass and 8-tube-passes heat exchanger is used to heat glycerin \(\left(c_{p}=0.60 \mathrm{Btu} / \mathrm{lbm} \cdot{ }^{\circ} \mathrm{F}\right)\) from \(65^{\circ} \mathrm{F}\) to \(140^{\circ} \mathrm{F}\) by hot water \(\left(c_{p}=1.0 \mathrm{Btu} / \mathrm{lbm} \cdot{ }^{\circ} \mathrm{F}\right)\) that enters the thinwalled \(0.5\)-in-diameter tubes at \(175^{\circ} \mathrm{F}\) and leaves at \(120^{\circ} \mathrm{F}\). The total length of the tubes in the heat exchanger is \(500 \mathrm{ft}\). The convection heat transfer coefficient is \(4 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F}\) on the glycerin (shell) side and \(50 \mathrm{Btu} / \mathrm{h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F}\) on the water (tube) side. Determine the rate of heat transfer in the heat exchanger \((a)\) before any fouling occurs and \((b)\) after fouling with a fouling factor of \(0.002 \mathrm{~h} \cdot \mathrm{ft}^{2} \cdot{ }^{\circ} \mathrm{F} /\) Btu on the outer surfaces of the tubes.

Explain how the maximum possible heat transfer rate \(\dot{Q}_{\max }\) in a heat exchanger can be determined when the mass flow rates, specific heats, and the inlet temperatures of the two fluids are specified. Does the value of \(\dot{Q}_{\max }\) depend on the type of the heat exchanger?

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