/*! 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 61 An object of irregular shape \(1... [FREE SOLUTION] | 91影视

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An object of irregular shape \(1 \mathrm{~m}\) long maintained at a constant temperature of \(100^{\circ} \mathrm{C}\) is suspended in an airstream having a free stream temperature of \(0^{\circ} \mathrm{C}\), a pressure of \(1 \mathrm{~atm}\), and a velocity of \(120 \mathrm{~m} / \mathrm{s}\). The air temperature measured at a point near the object in the airstream is \(80^{\circ} \mathrm{C}\). A second object having the same shape is \(2 \mathrm{~m}\) long and is suspended in an airstream in the same manner. The air free stream velocity is \(60 \mathrm{~m} / \mathrm{s}\). Both the air and the object are at \(50^{\circ} \mathrm{C}\), and the total pressure is \(1 \mathrm{~atm}\). A plastic coating on the surface of the object is being dried by this process. The molecular weight of the vapor is 82 , and the saturation pressure at \(50^{\circ} \mathrm{C}\) for the plastic material is \(0.0323 \mathrm{~atm}\). The mass diffusivity for the vapor in air at \(50^{\circ} \mathrm{C}\) is \(2.60 \times 10^{-5} \mathrm{~m}^{2} / \mathrm{s}\). (a) For the second object, at a location corresponding to the point of measurement on the first object, determine the vapor concentration and partial pressure. (b) If the average heat flux \(q^{\prime \prime}\) is \(2000 \mathrm{~W} / \mathrm{m}^{2}\) for the first object, determine the average mass flux \(n_{\mathrm{A}}^{\prime \prime}\left(\mathrm{kg} / \mathrm{s}^{\cdot} \mathrm{m}^{2}\right)\) for the second object.

Short Answer

Expert verified
In summary, we have found the vapor concentration \(C = 1.257 \times 10^{+20} \mathrm{~m}^{-3}\) and the partial pressure \(P_p = 6.3762 \times 10^{+21} \mathrm{~Pa}\) for the second object at the location corresponding to the point of measurement on the first object. However, to determine the average mass flux (\(n_A^{\prime \prime}\)), we need more information about the heat of vaporization or other unknown variables (Reynolds number, viscosity, and density).

Step by step solution

01

Write down the given information and find the Reynolds number.

We are given the following information: For object 1: - Length: \(L_1 = 1 \mathrm{~m}\) - Temperature: \(T_1 = 100^{\circ} \mathrm{C}\) - Airstream temperature: \(T_{a1} = 0^{\circ} \mathrm{C}\) - Airstream velocity: \(V_{a1} = 120 \mathrm{~m} / \mathrm{s}\) - Airstream pressure: \(P_{a1} = 1 \mathrm{~atm}\) - Temperature measured at a point: \(T_{m1} = 80^{\circ} \mathrm{C}\) For object 2: - Length: \(L_2 = 2 \mathrm{~m}\) - Temperature: \(T_2 = 50^{\circ} \mathrm{C}\) - Airstream temperature: \(T_{a2} = 50^{\circ} \mathrm{C}\) - Airstream velocity: \(V_{a2} = 60 \mathrm{~m} / \mathrm{s}\) - Airstream pressure: \(P_{a2} = 1 \mathrm{~atm}\) - Molecular weight of vapor: \(M_v = 82\) - Saturation pressure for the plastic material: \(P_v = 0.0323 \mathrm{~atm}\) - Mass diffusivity for the vapor in air: \(D_{m} = 2.60 \times 10^{-5} \mathrm{~m}^{2} / \mathrm{s}\) To analyze the flow of these objects, we should find the Reynolds numbers for both objects. Using the formula for the Reynolds number, we get: \[Re = \frac{蟻VD}{渭}\] However, we don't have enough information to calculate Reynolds numbers directly.
02

Calculate the vapor concentration C for the second object.

Using the given saturation pressure, we can find the vapor concentration (C) for the second object: \[C=\frac{P_{v}}{R_{u}T_{2}}\] Where \(R_u\) is the universal gas constant in J/(mol路K) and \(T_2\) is the temperature of the second object in Kelvin. Converting Celsius to Kelvin, we have: \[T_{2} = 50 + 273.15 = 323.15 \mathrm{~K}\] Using \(R_u = 8.314 \mathrm{~J/(mol \cdot K)}\), we can find the vapor concentration: \[C = \frac{0.0323 \mathrm{~atm} \cdot 101325 \mathrm{~Pa/atm}}{8.314 \mathrm{~J/(mol \cdot K)} \cdot 323.15 \mathrm{~K}}\] \[C = 1.257 \times 10^{+20} \mathrm{~m}^{-3}\]
03

Calculate the partial pressure for the second object.

Using the ideal gas law, we can find the partial pressure \(P_p\) of the vapor in the second object: \[P_p = CRT_v\] Where \(R_v\) is the specific gas constant for the vapor, which can be calculated using the universal gas constant and the molecular weight: \[R_v = \frac{R_u}{M_v}\] Substituting the values for \(R_u\) and \(M_v\), we get: \[R_v = \frac{8.314 \mathrm{~J/(mol \cdot K)}}{82} = 0.1014\frac{\mathrm{~J}}{\mathrm{g\cdot K}}\] Now, calculating the partial pressure: \[P_p = 1.257 \times 10^{+20} \mathrm{~m}^{-3} \cdot 0.1014\frac{\mathrm{~J}}{\mathrm{g\cdot K}} \cdot 50 \mathrm{~K}\] \[P_p = 6.3762 \times 10^{+21} \mathrm{~Pa}\]
04

Calculate the average mass flux for the second object.

We are given the average heat flux for the first object as \(q^{\prime \prime} = 2000 \mathrm{~W} / \mathrm{m}^2\). We can use this information to determine the average mass flux (\(n_A^{\prime \prime}\)) of the second object: \[n_{\mathrm{A}}^{\prime \prime}=h_q \frac{q^{\prime \prime}}{T_2},\] Where \(h_q\) is the heat of vaporization in J/kg. However, we don't have sufficient given information to calculate this value. This problem might be missing some necessary parameters or provided excess information. To obtain a valid solution, we need more data to calculate \(h_q\) or other unknown variables like the Reynolds number, viscosity (渭), and density (蟻).

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Key Concepts

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

Reynolds Number
Understanding the Reynolds number is crucial when examining fluid flow around objects. It helps determine whether the flow is laminar or turbulent. In our exercise, attempting to calculate the Reynolds number for the objects involves the formula \[Re = \frac{\rho VD}{\mu}\]where
  • \(\rho\) is the density of the fluid,
  • \(V\) is the velocity,
  • \(D\) is the characteristic length of the object,
  • \(\mu\) is the dynamic viscosity.
This dimensionless number highlights how forces are distributed within a fluid stream. However, to compute it accurately is challenging without viscosity and density values. Typically, for solving real-world problems, these values are estimated based on known fluid properties at particular temperatures and pressures.

Reynolds number shows how dominant inertial forces are compared to viscous forces in a flow, and it is a key indicator of flow type. Low values imply predominantly smooth, laminar flow. High values indicate more chaotic, turbulent flow.
Vapor Concentration
Vapor concentration measures how much vapor is present within a system's volume. To find the vapor concentration \(C\) for the second object in our exercise, we leverage the saturation pressure of vaporizing plastic material using the formula:\[C = \frac{P_v}{R_u T_2}\]In this calculation:
  • \(P_v\) is the saturation pressure,
  • \(R_u = 8.314\, J/(mol\cdot K)\) is the universal gas constant,
  • \(T_2\) is the temperature in Kelvin.
The formula relates vapor pressure to concentration, reflecting how gas expands across volume. Such calculations help in optimizing drying applications, like the one mentioned in the exercise, ensuring energy-efficient material processing.
Partial Pressure
Partial pressure is the pressure exerted by a single component in a mixture of gases. In our exercise, it involves calculating the partial pressure of vapor in the second object. This value helps predict how the vapor behaves within the airstream.

We find this pressure using the formula for ideal gas law: \[P_p = CRT_v\]where
  • \(C\) is the concentration of the vapor,
  • \(R_v\) is the specific gas constant for the vapor.
To find \(R_v\), we use:\[R_v = \frac{R_u}{M_v}\]where \(M_v\) is the molecular weight of the vapor. Partial pressure provides insight into how the vapor interacts with surrounding gases, crucial for engineering processes involving material evapotranspiration.
Mass Diffusivity
Mass diffusivity signifies the rate at which substances diffuse in response to concentration gradients in a medium. In terms of our problem, it helps in understanding how fast vapor spreads through air.

The mass diffusivity value \(D_m\) given鈥擻(2.60 \times 10^{-5} \; m^{2}/s\)鈥攄epicts this property for vapor in air at \(50^{\circ} C\). Essentially, it defines how quickly vapor particles mix with the air molecules. It's influenced by
  • temperature,
  • medium properties,
  • and particle interactions.
In a practical context, diffusion rates affect things like drying times of coatings. Understanding diffusivity allows for precise control in industries reducing operation costs and enhancing sustainability by fine-tuning conditions for optimal performance.

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Most popular questions from this chapter

Species A is evaporating from a flat surface into species B. Assume that the concentration profile for species A in the concentration boundary layer is of the form \(C_{\mathrm{A}}(y)=D y^{2}+E y+F\), where \(D, E\), and \(F\) are constants at any \(x\)-location and \(y\) is measured along a normal from the surface. Develop an expression for the mass transfer convection coefficient \(h_{w}\) in terms of these constants, the concentration of \(A\) in the free stream \(C_{\mathrm{A}, \infty}\) and the mass diffusivity \(D_{\mathrm{AB}}\). Write an expression for the molar flux of mass transfer by convection for species \(A\).

If laminar flow is induced at the surface of a disk due to rotation about its axis, the local convection coefficient is known to be a constant, \(h=C\), independent of radius. Consider conditions for which a disk of radius \(r_{o}=100 \mathrm{~mm}\) is rotating in stagnant air at \(T_{\infty}=20^{\circ} \mathrm{C}\) and a value of \(C=20 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\) is maintained. If an embedded electric heater maintains a surface temperature of \(T_{x}=50^{\circ} \mathrm{C}\), what is the local heat flux at the top surface of the disk? What is the total electric power requirement? What can you say about the nature of boundary layer development on the disk?

For laminar free convection from a heated vertical surface, the local convection coefficient may be expressed as \(h_{x}=C x^{-1 / 4}\), where \(h_{x}\) is the coefficient at a distance \(x\) from the leading edge of the surface and the quantity \(C\), which depends on the fluid properties, is independent of \(x\). Obtain an expression for the ratio \(\bar{h}_{x} / h_{x}\), where \(\bar{h}_{x}\) is the average coefficient between the leading edge \((x=0)\) and the \(x\)-location. Sketch the variation of \(h_{x}\) and \(\bar{h}_{x}\) with \(x\).

Forced air at \(T_{\infty}=25^{\circ} \mathrm{C}\) and \(V=10 \mathrm{~m} / \mathrm{s}\) is used to cool electronic elements on a circuit board. One such element is a chip, \(4 \mathrm{~mm} \times 4 \mathrm{~mm}\), located \(120 \mathrm{~mm}\) from the leading edge of the board. Experiments have revealed that flow over the board is disturbed by the elements and that convection heat transfer is correlated by an expression of the form Estimate the surface temperature of the chip if it is dissipating \(30 \mathrm{~mW}\).

Consider cross flow of gas \(\mathrm{X}\) over an object having a characteristic length of \(L=0.1 \mathrm{~m}\). For a Reynolds number of \(1 \times 10^{4}\), the average heat transfer coefficient is \(25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}\). The same object is then impregnated with liquid \(Y\) and subjected to the same flow conditions. Given the following thermophysical properties, what is the average convection mass transfer coefficient?

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