/*! 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 48 An \(L=1\)-m-long vertical coppe... [FREE SOLUTION] | 91影视

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An \(L=1\)-m-long vertical copper tube of inner diameter \(D_{i}=20 \mathrm{~mm}\) and wall thickness \(t=2 \mathrm{~mm}\) contains liquid water at \(T_{w}=0^{\circ} \mathrm{C}\). On a winter day, air at \(V=3 \mathrm{~m} / \mathrm{s}, T_{\infty}=-20^{\circ} \mathrm{C}\) is in cross flow over the tube. (a) Determine the heat loss per unit mass from the water (W/kg) when the tube is full of water. (b) Determine the heat loss from the water (W/kg) when the tube is half full.

Short Answer

Expert verified
(a) When the tube is full of water, the heat loss per unit mass is approximately 0.025 W/kg.

Step by step solution

01

(a) Heat loss per unit mass when the tube is full of water

Step 1: Determine the heat transfer coefficients We'll first find the heat transfer coefficients for heat transfer from the water to the inner surface of the copper tube and from the outer surface of the tube to the air. For heat transfer from water to the inner surface, we can use the Nusselt number definition: \(Nu = \dfrac{hD_i}{k}\), where \(h\) is the heat transfer coefficient between water and the inner tube surface, and \(k\) is the thermal conductivity of water. We can look up the Nusselt number for heat transfer from a fluid in a vertical tube to obtain \(Nu 鈮 4.36\). For water at \(0^{\circ}C\), the thermal conductivity is \(k 鈮 0.555 W/m路K\). With the given inner diameter of the tube, \(D_i = 20 mm\), we can find the heat transfer coefficient between water and the inner tube surface: \(h_{wi} = \dfrac{Nu路k}{D_i} 鈮 \dfrac{4.36路0.555}{0.02} 鈮 120.45 W/m^2路K\). For heat transfer from the outer surface of the tube to the air, we'll use the convection heat transfer equation: \(h_{oa} = C路Re^m路Pr^n\), where \(Re\) is the Reynolds number, \(Pr\) is the Prandtl number, and \(C, m\), and \(n\) are constant values, which depend on the flow regime. Given the air speed over the tube, we can calculate the Reynolds number: \(Re = \dfrac{蟻V(D_o - D_i)}{渭}\), where \(蟻\) is the density of air (1.292 kg/m鲁 at -20潞C), \(V\) is the air speed (3 m/s), \(D_o\) is the outer diameter of the tube (\(D_o = D_i + 2t = 20 + 2 路 2 = 24 mm = 0.024 m\)), and \(渭\) is the dynamic viscosity of air (1.717 x 10^-5 kg/m路s at -20潞C). So, \(Re 鈮 \dfrac{1.292路3路(0.024 - 0.02)}{1.717路10^{-5}} 鈮 645.98\). Since the Reynolds number is less than 2300, we have laminar flow. The constants that correspond to laminar flow are \(C = 0.664\), \(m = 0.5\), and \(n = 1/3\). We can look up the Prandtl number for air (\(Pr 鈮 0.728\) at -20潞C) and calculate the heat transfer coefficient between the outer surface and air: \(h_{oa} = 0.664路(645.98)^{0.5}路(0.728)^{(1/3)} 鈮 36.23 W/m^2路K\). Step 2: Calculate the heat transfer rate Next, we'll calculate the heat transfer rate from the water and tube to the ambient air using the heat transfer coefficients we obtained. The heat flow rate is expressed as: \(Q = area * U * (T_w - T_{\infty})\), where \(U\) is the overall heat transfer coefficient, which can be calculated using the thermal resistance of the copper tube and the convective heat transfer coefficients: \(\dfrac{1}{U} = \dfrac{1}{h_{wi}} + \dfrac{t}{k_t路A_i} + \dfrac{1}{h_{oa}}\), where \(k_t\) is the thermal conductivity of copper (\(k_t 鈮 391 W/m路K\)) and \(A_i\) is the inner surface area of the tube, which is given by: \(A_i = 蟺D_iL = 蟺路0.02路1 = 0.0628 m^2\). Hence, we have: \(\dfrac{1}{U} = \dfrac{1}{120.45} + \dfrac{0.002}{391路0.0628} + \dfrac{1}{36.23} 鈮 0.0123\) So, \(U 鈮 81.30 W/m^2路K\). Now we can calculate the heat transfer rate: \(Q = 0.0628路81.30路(0 - (-20)) 鈮 102.3 W\). Step 3: Calculate the heat loss per unit mass To determine the heat loss per unit mass, we'll use the specific heat capacity of liquid water (\(c_p = 4,186 J/kg路K\)): \(Q_m = \dfrac{Q}{c_p路(T_w - T_\infty)} = \dfrac{102.3}{4,186路} 鈮 0.025 W/kg\) So, when the tube is full of water, the heat loss per unit mass is approximately 0.025 W/kg.

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Key Concepts

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

Convection
Convection is a crucial heat transfer process that involves the movement of fluid over a surface, which facilitates the transfer of heat. This can occur naturally, due to density differences caused by temperature variations, or can be forced, as seen when a fan blows air across a surface. In the given exercise, air moving over the copper tube causes forced convection, aiding in the transfer of heat from the tube to the surrounding air.
  • The strength of convection is influenced by the velocity of the fluid, the properties of the fluid, and the surface geometry.
  • In our example, the relationship between the external air moving over the tube and the temperature difference between the inner water and outer air establishes the rate of heat transfer.
Understanding convection helps in calculating how effectively heat is removed from or added to surfaces, which is represented by the heat transfer coefficient in calculations.
Thermal Conductivity
Thermal conductivity is a material's ability to conduct heat. It serves as a measure of how quickly heat energy flows through a material due to a temperature gradient.
In our exercise, copper's high thermal conductivity (\(k_t \approx 391 \, ext{W/m}\cdot\text{K}\)) allows for effective transfer of heat from the water inside the tube to its outer surface.
  • High thermal conductivity materials like copper are used in situations where efficient heat transfer is needed, such as in heat exchangers.
  • Water also has a notable thermal conductivity (\(k \approx 0.555 \, ext{W/m}\cdot\text{K}\)) which plays a crucial role in transferring energy from its middle to the tube wall.
A good understanding of thermal conductivity allows engineers to design systems that manage heat effectively, considering both material properties and thickness.
Reynolds Number
The Reynolds number (\(Re\)) is a dimensionless value used to predict flow patterns in fluid dynamics. It determines whether the flow will be laminar or turbulent.
In the exercise, the Reynolds number was calculated to be approximately 645.98 for air moving over the tube, indicating a laminar flow.
  • Laminar flow means that the fluid flows in parallel layers with no disruption between them, ideal for precise heat transfer predictions.
  • \(Re = \dfrac{\rho V (D_o - D_i)}{\mu}\)
  • This calculation uses density (\(\rho\)), velocity (\(V\)), characteristic length (\(D_o - D_i\)), and dynamic viscosity (\(\mu\)).
Knowing the Reynolds number helps in selecting the right correlations for calculating heat transfer coefficients and in determining flow characteristics.
Thermal Resistance
Thermal resistance quantifies a material's opposition to heat flow, analogous to electrical resistance in circuits. It's an important concept when evaluating how different layers in an assembly impact overall heat transfer.
In this problem, thermal resistance is used to determine the overall heat transfer coefficient (\(U\)).
  • It is calculated as the sum of the resistances through the tube and the convective boundaries.
  • The formula involves conduction through the material and convection at the surfaces: \(\dfrac{1}{U} = \dfrac{1}{h_{wi}} + \dfrac{t}{k_t \cdot A_i} + \dfrac{1}{h_{oa}}\).
Understanding thermal resistance helps in determining efficiency and identifying which parts of the system limit heat transfer, thus guiding material and geometry choices for optimizing thermal performance.

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Most popular questions from this chapter

Consider water at \(27^{\circ} \mathrm{C}\) in parallel flow over an isother\(\mathrm{mal}, 1\)-m-long flat plate with a velocity of \(2 \mathrm{~m} / \mathrm{s}\). (a) Plot the variation of the local heat transfer coefficient, \(h_{x}(x)\), with distance along the plate for three flow conditions corresponding to transition Reynolds numbers of (i) \(5 \times 10^{5}\), (ii) \(3 \times 10^{5}\), and (iii) 0 (the flow is fully turbulent). (b) Plot the variation of the average heat transfer coefficient \(\bar{h}_{x}(x)\) with distance for the three flow conditions of part (a). (c) What are the average heat transfer coefficients for the entire plate \(\bar{h}_{L}\) for the three flow conditions of part (a)?

Consider a liquid metal \((\operatorname{Pr} \leqslant 1)\), with free stream conditions \(u_{\infty}\) and \(T_{\infty}\), in parallel flow over an isothermal flat plate at \(T_{s}\). Assuming that \(u=u_{\infty}\) throughout the thermal boundary layer, write the corresponding form of the boundary layer energy equation. Applying appropriate initial \((x=0)\) and boundary conditions, solve this equation for the boundary layer temperature field, \(T(x, y)\). Use the result to obtain an expression for the local Nusselt number \(\mathrm{Nu}_{x}\). Hint: This problem is analogous to one-dimensional heat transfer in a semiinfinite medium with a sudden change in surface temperature.

A circular pipe of 25 -mm outside diameter is placed in an airstream at \(25^{\circ} \mathrm{C}\) and 1 -atm pressure. The air moves in cross flow over the pipe at \(15 \mathrm{~m} / \mathrm{s}\), while the outer surface of the pipe is maintained at \(100^{\circ} \mathrm{C}\). What is the drag force exerted on the pipe per unit length? What is the rate of heat transfer from the pipe per unit length?

Consider an air-conditioning system composed of a bank of tubes arranged normal to air flowing in a duct at a mass rate of \(\dot{m}_{a}(\mathrm{~kg} / \mathrm{s})\). A coolant flowing through the tubes is able to maintain the surface temperature of the tubes at a constant value of \(T_{s}

The cylindrical chamber of a pebble bed nuclear reactor is of length \(L=10 \mathrm{~m}\), and diameter \(D=3 \mathrm{~m}\). The chamber is filled with spherical uranium oxide pellets of core diameter \(D_{p}=50 \mathrm{~mm}\). Each pellet generates thermal energy in its core at a rate of \(\dot{E}_{g}\) and is coated with a layer of non-heat-generating graphite, which is of uniform thickness \(\delta=5 \mathrm{~mm}\), to form a pebble. The uranium oxide and graphite each have a thermal conductivity of \(2 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\). The packed bed has a porosity of \(\varepsilon=0.4\). Pressurized helium at 40 bars is used to absorb the thermal energy from the pebbles. The helium enters the packed bed at \(T_{i}=450^{\circ} \mathrm{C}\) with a velocity of \(3.2 \mathrm{~m} / \mathrm{s}\). The properties of the helium may be assumed to be \(c_{p}=5193 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}\), \(k=0.3355 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \rho=2.1676 \mathrm{~kg} / \mathrm{m}^{3}, \mu=4.214 \times\) \(10^{-5} \mathrm{~kg} / \mathrm{s} \cdot \mathrm{m}, \operatorname{Pr}=0.654\). (a) For a desired overall thermal energy transfer rate of \(q=125 \mathrm{MW}\), determine the mean outlet temperature of the helium leaving the bed, \(T_{o}\), and the amount of thermal energy generated by each pellet, \(\dot{E}_{g^{*}}\) (b) The amount of energy generated by the fuel decreases if a maximum operating temperature of approximately \(2100^{\circ} \mathrm{C}\) is exceeded. Determine the maximum internal temperature of the hottest pellet in the packed bed. For Reynolds numbers in the range \(4000 \leq R e_{D} \leq 10,000\), Equation \(7.81\) may be replaced by \(\varepsilon \bar{j}_{H}=2.876 R e_{D}^{-1}+0.3023 R e_{D}^{-0.35}\).

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