/*! 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 53 A hot fluid passes through a thi... [FREE SOLUTION] | 91Ó°ÊÓ

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A hot fluid passes through a thin-walled tube of \(10-\mathrm{mm}\) diameter and \(1 . \mathrm{m}\) length. and a coolant at \(T_{\mathrm{w}}=25^{\circ} \mathrm{C}\) is in cross flow over the tube. When the flow rate is \(\dot{m}=18 \mathrm{~kg} / \mathrm{h}\) and the inlet temperature is \(T_{m u}=85^{\circ} \mathrm{C}\). the outlet temperature is \(T_{\operatorname{mor}}=78^{\circ} \mathrm{C}\). Assuming fully developed flow and thermal conditions in the tube, determine the outlet temperarure, \(T_{\text {man }}\) if the flow rate is increased by a factor of 2 . That is, \(m=36 \mathrm{~kg} / \mathrm{h}\), with all other conditions the same, The thermophysical properties of the hot fluid are $$ \rho=1079 \mathrm{~kg} / \mathrm{m}^{3}, \quad c_{p}=2637 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, \quad \mu=0.0034 \mathrm{~N} \text { - } $$ \(\mathrm{sm}^{2}\), and \(k=0.261 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\).

Short Answer

Expert verified
The outlet temperature for the increased flow rate is approximately 81.5°C.

Step by step solution

01

- Determine Heat Transfer Rate for Original Conditions

The heat transfer rate can be calculated using the equation: \( q = \dot{m} \cdot c_p \cdot (T_{in} - T_{out}) \). Here, \( \dot{m} = 18 \frac{\text{kg}}{\text{h}} = 0.005 \frac{\text{kg}}{\text{s}} \), \( c_p = 2637 \frac{\text{J}}{\text{kg} \cdot \text{K}} \), \( T_{in} = 85^\circ C \), and \( T_{out} = 78^\circ C \). Substituting these values, we have: \( q = 0.005 \cdot 2637 \cdot (85 - 78) \). Calculate \( q \) to determine the heat transfer rate.
02

- Calculate Heat Transfer for Increased Flow Rate

When the mass flow rate is doubled, \( \dot{m} = 36 \frac{\text{kg}}{\text{h}} = 0.01 \frac{\text{kg}}{\text{s}} \). The heat transfer rate must remain approximately the same since the external conditions are unchanged. Assume \( q' \approx q \). Thus, \( q' = \dot{m}_{new} \cdot c_p \cdot (T_{in} - T_{out,new}) \). Set \( q' = q \) from Step 1 and solve for \( T_{out,new} \).
03

- Solve for New Outlet Temperature

Rearrange the equation from Step 2 to solve for \( T_{out,new} \): \( T_{out,new} = T_{in} - \frac{q}{\dot{m}_{new} \cdot c_p} \). Insert the values \( q \) from Step 1 and \( \dot{m}_{new} = 0.01 \), \( c_p = 2637 \) to find \( T_{out,new} \).
04

- Result and Interpretation

Substituting the calculated heat transfer rate \( q \) from Step 1 into the equation from Step 3, compute \( T_{out,new} \). Verify if this temperature is consistent with physical expectations noting that higher flow rates generally reduce the outlet temperature. Provide the solution as the final outlet temperature for the increased flow rate scenario.

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Key Concepts

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

Thermophysical Properties
Understanding the thermophysical properties of a substance is key in analyzing heat transfer scenarios. These properties describe the behavior of a fluid as it undergoes changes in temperature. Key thermophysical properties include:
  • Density (\( \rho \)): This property, measured in \( \text{kg/m}^3 \), indicates the mass per unit volume of a substance. In this case, the hot fluid has a density of \( 1079 \text{ kg/m}^3 \).
  • Specific Heat Capacity (\( c_p \)): Represented in \( \text{J/kg} \cdot \text{K} \), this is the amount of heat required to change the temperature of a unit mass by one degree Kelvin. Here, \( c_p \) is \( 2637 \text{ J/kg} \cdot \text{K} \) for the hot fluid.
  • Viscosity (\( \mu \)): Measured in \( \text{N} \cdot \text{s/m}^2 \), it indicates a fluid's resistance to flow. The hot fluid has a viscosity of \( 0.0034 \text{ N} \cdot \text{s/m}^2 \).
  • Thermal Conductivity (\( k \)): This property, measured in \( \text{W/m} \cdot \text{K} \), indicates a material's ability to conduct heat. For our fluid, it is \( 0.261 \text{ W/m} \cdot \text{K} \).
By understanding these properties, engineers can predict how efficiently a fluid will transfer heat when heated or cooled, which is crucial when designing systems involving heat exchange.
Mass Flow Rate
The mass flow rate is a critical concept in heat transfer, especially in systems involving fluid flows. It measures the mass of the fluid passing through a given cross-sectional area per unit of time. In our exercise, the mass flow rate (\( \dot{m} \)) initially is \( 18 \text{ kg/h} \), which is then doubled.
  • To work with mass flow rate conveniently in calculations, it is often converted from hours to seconds, yielding here \( 0.005 \text{ kg/s} \) initially.
  • A higher mass flow rate generally means more fluid is available to carry heat away, which can affect the outlet temperature of the system.
  • When the mass flow rate was doubled to \( 0.01 \text{ kg/s} \), there was a drop in outlet temperature due to the increased heat capacity of the added mass, which carries away more heat.
The relationship shows why controlling mass flow rate is essential for managing the temperature in thermal systems.
Outlet Temperature Calculation
Calculating the outlet temperature of a fluid in heat-exchange systems is pivotal for system effectiveness. This requires understanding of how changes in conditions, like mass flow rate, impact the temperature.
  • The outlet temperature can be found using the equation: \[ T_{out,new} = T_{in} - \frac{q}{\dot{m}_{new} \cdot c_p} \] where \( T_{in} \) is the inlet temperature, \( q \) is the heat transfer rate from the original conditions, \( \dot{m}_{new} \) is the new mass flow rate, and \( c_p \) is the specific heat capacity.
  • By doubling the mass flow rate, assuming unchanged external conditions, the outlet temperature \( T_{out,new} \) will be lower than the original outlet temperature due to higher fluid mass absorbing the heat.
  • This calculation illustrates how control over fluid flow and heat transfer can manage the thermal output of a system, making it a powerful tool in engineering applications where precise temperature control is necessary.
Understanding and executing these calculations allow engineers to ensure systems operate within desired thermal limits.

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Most popular questions from this chapter

Cooling water flows through the \(25.4-\mathrm{mm}\)-diameter thin-walled tubes of a steam condenser at \(1 \mathrm{~m} / \mathrm{s}\), and a surface temperature of \(350 \mathrm{~K}\) is maintained by the condensing steam. The water inlet temperature is \(290 \mathrm{~K}\). and the tubes are \(5 \mathrm{~m}\) long. (a) What is the water cutlet temperature? Evaluate water properties at an assumed average mean temperature, \(\bar{T}_{\mathrm{m}}=300 \mathrm{~K}\). (b) Was the assumed value for \(\bar{T}_{m}\) reasonable? If not, repeat the calculntion using properties evaluated at a more appropriate temperature. [(c) A range of tube lengths from 4 to \(7 \mathrm{~m}\) is available to the engineer designing this condenser, Generate a plot to show what coolant mean velocities are possible if the water outlet temperature is to remain at the value found for part (b). All other conditions remain the same.

A heating contractor must heat \(0.2 \mathrm{~kg} / \mathrm{s}\) of water from \(15^{\circ} \mathrm{C}\) to \(35^{\circ} \mathrm{C}\) using hot gases in cross flow over a thinwalled tube. Your assignment is to develop a series of design graphs that can be used to demonstrate acceptable combinations of tube dimensions \((D\) and \(L)\) and of hot gas conditions \(\left(T_{\text {e }}\right.\) and \(V\) ) that satisfy this requirement. In your analysis, consider the following parameter ranges: \(D=20,30\), or \(40 \mathrm{~mm} ; L=3,4\), or \(6 \mathrm{~m}\); \(T_{=}=250,375\), or \(500^{\circ} \mathrm{C}\) : and \(20 \leq V \leq 40 \mathrm{~m} / \mathrm{s}\),

It is common practice to recover waste heat froen as oil of gas-fired fumace by using the exhaust gases te poe heat the combustion air. A device commonly used \(5 x\) this purpose consists of a concentric pipe arrangentr for which the exhaust gases are passed through the inte pipe, while the cooler combustion air fows througt a annular passage around the pipe. Consider conditions for which there is a uriform heat transfer rate per unit length, \(q_{i}^{\prime}=1.25 \times 10^{5}\) Whm from the exhaus gases to the pipe inner surface, whice air flows through the annular passage at a rate of \(m_{e}=21\) \(\mathrm{kg} / \mathrm{s}\). The thin-walled inner pipe is of diamcter \(D_{i}=2 \mathrm{n}\) while the outer pipe, which is well insulated from the sesroundings, is of diameter \(D_{e}=2.05 \mathrm{~m}\). The air properics may be taken to be \(c_{p}=1030 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, \mu=200 \mathrm{X}\) \(10^{-1} \mathrm{~N} \cdot \mathrm{s} / \mathrm{m}^{2}, k=0.041 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\), and \(P r=0.6 \mathrm{R} .\) (a) If air enters at \(T_{e .1}=300 \mathrm{~K}\) and \(L=7 \mathrm{~m}\), whar is the air outlet temperature \(T_{a, z}\) ? (b) If the airflow is fully developed throughout the annular region, what is the iemperature of the inner pipe at the inlet \(\left(T_{\text {wi }}\right)\) and outlet \(\left(T_{\text {Ma }}\right)\) sections \(d\) the device? What is the outer surface tempentus \(T_{\text {se } 1}\) at the inlet?

Consider a horizontal, thin-walled circular tube of diameler \(D=0.025 \mathrm{~m}\) submerged in a container of \(n\)-octadecane (paraffin), which is used to store thermal energy. As hot water flows through the tube, heat is transferred to the paraffin, converting it from the solid to liq: uid state at the phase change temperature of \(T_{\mathrm{s}}=\) \(27.4^{\circ} \mathrm{C}\). The latent heat of fusion and density of paraffin are \(h_{t j}=244 \mathrm{~kJ} / \mathrm{kg}\) and \(\rho=770 \mathrm{~kg} / \mathrm{m}^{3}\), respectively, and thermophysical properties of the water may be taken as \(c_{\mathrm{r}}=4.185 \mathrm{~kJ} / \mathrm{kg}+\mathrm{K}, k=0.653 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \mu=467 \times\) \(10^{-6} \mathrm{~kg} / \mathrm{s} \cdot \mathrm{m}\), and \(\operatorname{Pr}=2.99\). (a) Assuming the tube surface to have a uniform temperature corresponding to that of the phase change, determine the water outlet temperature and total heat transfer rate for a water flow rate of \(0,1 \mathrm{~kg} / \mathrm{s}\) and an inlet temperature of \(60^{\circ} \mathrm{C}\). If \(H=W=\) \(0.25 \mathrm{~m}\), how long would it take to completely liquefy the paraffin, from an initial state for which all the paraffin is solid and at \(27.4^{\circ} \mathrm{C}\) ? (b) The liquefaction process can be accelerated by increasing the flow rate of the water. Compute and plot the heat rate and outlet temperature as a function of flow rate for \(0.1 \leq m \leq 0.5 \mathrm{~kg} / \mathrm{s}\). How long would it take to melt the paraffin for in \(=0.5 \mathrm{~kg} / \mathrm{s}\) ?

Consider a concentric tube annulus for which the inner and outer diameters are 25 and \(50 \mathrm{~mm}\). Water enters the annular region at \(0.04 \mathrm{~kg} / \mathrm{s}\) and \(25^{\circ} \mathrm{C}\). If the inner tube wall is heated electrically at a rate (per unit length) of \(q^{\prime}=4000 \mathrm{~W} / \mathrm{m}\), while the outer tube wall is insulated, how long must the tubes be for the water to acticue \(\boldsymbol{z}\) outlet temperature of \(85^{\circ} \mathrm{C}\) ? What is the inner nube serface temperature at the outlet, where fully devekped conditions may be assumed?

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