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A jacketed-agitated vessel, fitted with a turbine agitator, is used for heating a water stream from \(10^{\circ} \mathrm{C}\) to $54^{\circ} \mathrm{C}$. The average heat transfer coefficient for water at the vessel's inner wall can be estimated from \(\mathrm{Nu}=\) $0.76 \mathrm{Re}^{2 / 3} \mathrm{Pr}^{1 / 3}\(. Saturated steam at \)100^{\circ} \mathrm{C}$ condenses in the jacket, for which the average heat transfer coefficient in $\mathrm{kW} / \mathrm{m}^{2} \cdot \mathrm{K}$ is: \(h_{o}=13.1\left(T_{g}-T_{w}\right)^{-0.25}\). The vessel dimensions are: \(D_{t}=0.6 \mathrm{~m}, H=0.6 \mathrm{~m}\), and \(D_{a}=0.2 \mathrm{~m}\). The agitator speed is \(60 \mathrm{rpm}\). Calculate the mass rate of water that can be heated in this agitated vessel steadily.

Short Answer

Expert verified
In a jacketed-agitated vessel used for heating a water stream from \(10^{\circ} \mathrm{C}\) to \(54^{\circ} \mathrm{C}\), determine the mass flow rate of water that can be heated in this vessel steadily. The mass flow rate of water that can be heated in this agitated vessel steadily is approximately \(0.380 \mathrm{~kg/s}\).

Step by step solution

01

Determine Reynolds number and Prandtl number

First, we need to calculate the Reynolds number (Re) and the Prandtl number (Pr) for the water. Using the given vessel dimensions and agitator speed, we can determine the kinematic viscosity and thermal diffusivity of water and use them to calculate Re and Pr, respectively. The kinematic viscosity of water at approximately \(20^{\circ}C\) is \(\nu = 1 \times 10^{-6} \mathrm{~m}^2/\mathrm{s}\), and its thermal diffusivity is \(\alpha = 1.45 \times 10^{-7} \mathrm{~m}^2/\mathrm{s}\). Reynolds number: \(\mathrm{Re} = \frac{D_t N}{\nu}\) Prandtl number: \(\mathrm{Pr} = \frac{c_p \mu}{k}\), where \(c_p\) is the heat capacity at constant pressure, \(\mu\) is the dynamic viscosity, and \(k\) is the thermal conductivity. Since we are not given these values for water, we will instead use typical values for water: \(c_p = 4.2 \mathrm{~kJ / kg \cdot K}\), \(\mu = 1 \times 10^{-3} \mathrm{~N \cdot s / m^2}\), and \(k = 0.6 \mathrm{~W / m \cdot K}\). Calculate Re and Pr: Re = (0.6 m)(60 rpm)(1/0.0167 Hz)(1/1*10^{-6} m^2/s) = 21600 Pr = (4.2 kJ/kgK)(1*10^{-3} Ns/m^2)/(0.6 W/mK) = 7 Remember these results for the forthcoming steps.
02

Calculate heat transfer coefficient for water inside the vessel

Next, we calculate the heat transfer coefficient for water inside the vessel. Meanwhile, we'll make use of the given Nusselt number correlation: \(\mathrm{Nu} = 0.76 \mathrm{Re}^{2/3} \mathrm{Pr}^{1/3}\). The Nusselt number is the ratio of convective to conductive heat transfer across a boundary, and it can be expressed as \(\mathrm{Nu} = \frac{h_i D_t}{k}\), where \(h_i\) is the heat transfer coefficient inside the vessel and \(D_t\) is the vessel diameter. Calculate the Nusselt number, and then use it to determine \(h_i\): Nu = 0.76 * (21600)^(2/3) * (7)^(1/3) = 160.3 h_i = (160.3 * 0.6 W/mK) / 0.6 m = 160.3 W/m^2K
03

Calculate overall heat transfer coefficient

Now we need to calculate the overall heat transfer coefficient \(U\) using the given function for the average heat transfer coefficient in the jacket, \(h_o = 13.1(T_g - T_w)^{-0.25}\). The inner wall temperature \(T_w\) can be assumed to be \(54^{\circ}C\), and the jacket steam temperature is given as \(T_g = 100^{\circ}C\). Calculate the jacket heat transfer coefficient \(h_o\): h_o = 13.1(100-54)^{-0.25} = 5.43 kW/m^2K To find the overall heat transfer coefficient \(U\), we take the reciprocal of the sum of the reciprocals of \(h_i\) and \(h_{\mathrm{o}}\): \(\frac{1}{U} = \frac{1}{h_{\mathrm{i}}} + \frac{1}{h_{\mathrm{o}}}\) \(U = \frac{1}{\frac{1}{160.3} + \frac{1}{5430}} = 154.4 \mathrm{~W/m^2K}\)
04

Calculate heat transfer area

The heat transfer area (\(A\)) can be calculated using the given vessel dimensions, assuming that heat transfer occurs through the entire inner surface of the cylindrical vessel: \(A = 2 \pi (D_t/2)(H)\) \(A = 2 \pi (0.6\mathrm{m}/2)(0.6\mathrm{m}) = 1.131 \mathrm{~m}^2\)
05

Calculate energy transfer rate

To find the energy transfer rate \(Q\), we will use the following equation: \(Q = U A (T_g - T_w)\) \(Q = 154.4 \mathrm{~W/m^2K} * 1.131 \mathrm{~m}^2 * (100^{\circ} \mathrm{C} - 54^{\circ} \mathrm{C}) = 7.792 \times 10^3 \mathrm{~W}\)
06

Calculate mass flow rate of water

Finally, we can calculate the mass flow rate of water using the energy balance equation: \(\dot{m} = \frac{Q}{c_p (T_{out} - T_{in})}\) \(\dot{m} = \frac{7.792 \times 10^3 \mathrm{~W}}{4.2 \mathrm{~kJ/kgK} * (54^{\circ} \mathrm{C} - 10^{\circ} \mathrm{C})} = 0.380 \mathrm{~kg/s}\) The mass flow rate of water that can be heated in this agitated vessel steadily is approximately \(0.380 \mathrm{~kg/s}\).

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Most popular questions from this chapter

Glycerin \(\left(c_{p}=2400 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\) at \(20^{\circ} \mathrm{C}\) and \(0.5 \mathrm{~kg} / \mathrm{s}\) is to be heated by ethylene glycol $\left(c_{p}=2500 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\right)\( at \)60^{\circ} \mathrm{C}$ and the same mass flow rate in a thin-walled double-pipe parallelflow heat exchanger. If the overall heat transfer coefficient is \(380 \mathrm{~W} / \mathrm{m}^{2}\). \(\mathrm{K}\) and the heat transfer surface area is \(6.5 \mathrm{~m}^{2}\), determine \((a)\) the rate of heat transfer and \((b)\) the outlet temperatures of the glycerin and the glycol.

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 12 times the inner surface area, the overall heat transfer coefficient of this heat exchanger based on the inner surface area is (a) \(760 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (b) \(832 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (c) \(947 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (d) \(1075 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) (e) \(1210 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\)

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 inlet temperatures of the two fluids are specified. Does the value of \(\dot{Q}_{\max }\) depend on the type of the heat exchanger?

Consider two double-pipe counterflow heat exchangers that are identical except that one is twice as long as the other one. Which heat exchanger is more likely to have a higher effectiveness?

In a parallel-flow, water-to-water heat exchanger, the hot water enters at \(75^{\circ} \mathrm{C}\) at a rate of \(1.2 \mathrm{~kg} / \mathrm{s}\) and cold water enters at \(20^{\circ} \mathrm{C}\) at a rate of $0.9 \mathrm{~kg} / \mathrm{s}$. The overall heat transfer coefficient and the surface area for this heat exchanger are \(750 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) and \(6.4 \mathrm{~m}^{2}\), respectively. The specific heat for both the hot and cold fluids may be taken to be $4.18 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K}$. For the same overall heat transfer coefficient and the surface area, the increase in the effectiveness of this heat exchanger if counterflow arrangement is used is (a) \(0.09\) (b) \(0.11\) (c) \(0.14\) (d) \(0.17\) (e) \(0.19\)

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