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Fundamentals of Heat and Mass Transfer

Theodore L. Bergman, Adrienne S. Lavine, Frank P. Incropera

Chapter 6

Introduction to Convection - all with Video Answers

Educators


Chapter Questions

04:06

Problem 1

The temperature distribution within a laminar thermal boundary layer associated with flow over an isothermal flat plate is shown in the sketch. The temperature distribution shown is located at $x=x_{2}$.
(a) Is the plate being heated or cooled by the fluid?
(b) Carefully sketch the temperature distributions at $x=x_{1}$ and $x=x_{3}$. Based on your sketch, at which of the three $x$-locations is the local heat flux largest? At which location is the local heat flux smallest?
(c) As the free stream velocity increases, the velocity and thermal boundary layers both become thinner. Carefully sketch the temperature distributions at $x=x_{2}$ for (i) a low free stream velocity and (ii) a high free stream velocity. Based on your sketch, which velocity condition will induce the larger local convective heat flux?

Joseph Liao
Joseph Liao
Numerade Educator
05:46

Problem 2

In flow over a surface, velocity and temperature profiles are of the forms
$$
\begin{aligned}
&u(y)=A y+B y^{2}-C y^{3} \quad \text { and } \\
&T(y)=D+E y+F y^{2}-G y^{3}
\end{aligned}
$$
where the coefficients $A$ through $G$ are constants. Obtain expressions for the friction coefficient $C_{f}$ and the convection coefficient $h$ in terms of $u_{z}, T_{x}$, and appropriate profile coefficients and fluid properties.

Satpal Satpal
Satpal Satpal
Numerade Educator
04:06

Problem 3

In a particular application involving airflow over a heated surface, the boundary layer temperature distribution may be approximated as
$$
\frac{T-T_{s}}{T_{\infty}-T_{s}}=1-\exp \left(-\operatorname{Pr} \frac{u_{x c} y}{y}\right)
$$
where $y$ is the distance normal to the surface and the Prandtl number, $\operatorname{Pr}=c_{p} \mu / k=0.7$, is a dimensionless fluid property. If $T_{x}=400 \mathrm{~K}, T_{s}=300 \mathrm{~K}$, and $u_{s} / v=5000 \mathrm{~m}^{-1}$, what is the surface heat flux?

Joseph Liao
Joseph Liao
Numerade Educator
04:17

Problem 4

Water at a temperature of $T_{c}=25^{\circ} \mathrm{C}$ flows over one of the surfaces of a steel wall (AISI 1010) whose temperature is $T_{s, 1}=40^{\circ} \mathrm{C}$. The wall is $0.35 \mathrm{~m}$ thick, and its other surface temperature is $T_{s, 2}=100^{\circ} \mathrm{C}$. For steadystate conditions what is the convection coefficient associated with the water flow? What is the temperature gradient in the wall and in the water that is in contact with the wall? Sketch the temperature distribution in the wall and in the adjoining water.

Surendra Kumar
Surendra Kumar
Numerade Educator
02:01

Problem 5

For laminar flow over a flat plate, the local heat transfer coefficient $h_{x}$ is known to vary as $x^{-1 / 2}$, where $x$ is the distance from the leading edge $(x=0)$ of the plate. What is the ratio of the average coefficient between the leading edge and some location $x$ on the plate to the local coefficient at $x$ ?

Narayan Hari
Narayan Hari
Numerade Educator
02:01

Problem 6

A flat plate is of planar dimension $1 \mathrm{~m} \times 0.75 \mathrm{~m}$. For parallel laminar flow over the plate, calculate the ratio of the average heat transfer coefficients over the entire plate, $\bar{h}_{L, 1} / \bar{h}_{L, 2}$, for two cases. In Case 1, flow is in the short direction $(L=0.75 \mathrm{~m})$; in Case 2 , flow is in the long direction $(L=1 \mathrm{~m})$. Which orientation will result in the larger heat transfer rate? See Problem 6.5.

Narayan Hari
Narayan Hari
Numerade Educator
01:58

Problem 7

Parallel flow of atmospheric air over a flat plate of length $L=3 \mathrm{~m}$ is disrupted by an array of stationary rods placed in the flow path over the plate.
Laboratory measurements of the local convection coefficient at the surface of the plate are made for a prescribed value of $V$ and $T_{x}>T_{x}$. The results are correlated by an expression of the form $h_{x}=0.7+13.6 x-3.4 x^{2}$, where $h_{x}$ has units of $\mathrm{W} / \mathrm{m}^{2} \cdot \mathrm{K}$ and $x$ is in meters. Evaluate the average convection coefficient $\bar{h}_{L}$ for the entire plate and the ratio $\bar{h}_{L} / h_{L}$ at the trailing edge.

Narayan Hari
Narayan Hari
Numerade Educator
09:52

Problem 8

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 $x$.

Khoobchandra Agrawal
Khoobchandra Agrawal
Numerade Educator
02:17

Problem 9

A circular, hot gas jet at $T_{\mathrm{o}}$ is directed normal to a circular plate that has radius $r_{o}$ and is maintained at a uniform temperature $T_{x}$. Gas flow over the plate is axisymmetric, causing the local convection coefficient to have a radial dependence of the form $h(r)=a+b r^{n}$, where $a, b$, and $n$ are constants. Determine the rate of heat transfer to the plate, expressing your result in terms of $T_{x}, T_{s}, r_{o}, a$, $b$, and $n$.

Nicholas Mogoi
Nicholas Mogoi
Numerade Educator
03:37

Problem 10

Experiments have been conducted to determine local heat transfer coefficients for flow perpendicular to a long, isothermal bar of rectangular cross section. The bar is of width $c$ parallel to the flow, and height $d$ normal to the flow. For Reynolds numbers in the range $10^{4} \leq R_{d} \leq 5 \times 10^{4}$, the face-averaged Nusselt numbers are well correlated by an expression of the form The values of $C$ and $m$ for the front face, side faces, and back face of the rectangular rod are found to be the following:
\begin{tabular}{llll}
\hline Face & cld & $\boldsymbol{C}$ & $\boldsymbol{m}$ \\
\hline Front & $0.33 \leq$ cld $51.33$ & $0.674$ & $1 / 2$ \\
Side & $0.33$ & $0.153$ & $2 / 3$ \\
Side & $1.33$ & $0.107$ & $2 / 3$ \\
Back & $0.33$ & $0.174$ & $2 / 3$ \\
Back & $1.33$ & $0.153$ & $2 / 3$ \\
\hline
\end{tabular}
Determine the value of the average heat transfer coefficient for the entire exposed surface (that is, averaged over all four faces) of a $c=40$-mm-wide, $d=30$-mm-tall rectangular rod. The rod is exposed to air in cross flow at $V=10 \mathrm{~m} / \mathrm{s}, T_{x}=300 \mathrm{~K}$. Provide a plausible explanation of the relative values of the face-averaged heat transfer coefficients on the front, side, and back faces.

Manish Jain
Manish Jain
Numerade Educator
04:53

Problem 11

A concentrating solar collector consists of a parabolic reflector and a collector tube of diameter $D$, through which flows a working fluid that is heated with concentrated solar irradiation. Throughout the day, the reflector is slowly repositioned to track the sun. For wind conditions characterized by a steady, horizontal flow normal to the tube axis, the local heat transfer coefficient on the tube surface varies, as shown in the schematic for various reflector positions.
(a) Estimate the value of the average heat transfer coefficient over the entire collector tube surface for each of the three cases.
(b) Assuming the tube receives the same amount of solar irradiation in each case, which case would have the highest collector efficiency?

Eric Mockensturm
Eric Mockensturm
Numerade Educator
01:52

Problem 12

Air at a free stream temperature of $T_{a}=20^{\circ} \mathrm{C}$ is in parallel flow over a flat plate of length $L=5 \mathrm{~m}$ and temperature $T_{s}=90^{\circ} \mathrm{C}$. However, obstacles placed in the flow intensify mixing with increasing distance $x$ from the leading edge, and the spatial variation of temperatures measured in the boundary layer is correlated by an expression of the form $T\left({ }^{\circ} \mathrm{C}\right)=20+70$ $\exp (-600 x y)$, where $x$ and $y$ are in meters. Determine and plot the manner in which the local convection coefficient $h$ varies with $x$. Evaluate the average convection coefficient $\bar{h}$ for the plate.

Chai Santi
Chai Santi
Numerade Educator
02:01

Problem 13

The heat transfer rate per unit width (normal to the page) from a longitudinal section, $x_{2}-x_{1}$, can be expressed as $q_{12}^{\prime}=\bar{h}_{12}\left(x_{2}-x_{1}\right)\left(T_{s}-T_{\infty}\right)$, where $\bar{h}_{12}$ is the average coefficient for the section of length $\left(x_{2}-x_{1}\right)$. Consider laminar flow over a flat plate with a uniform temperature $T_{s}$. The spatial variation of the local convection coefficient is of the form $h_{x}=C x^{-1 / 2}$, where $C$ is a constant.
(a) Beginning with the convection rate equation in the form $d q^{\prime}=h_{s} d x\left(T_{s}-T_{x}\right)$, derive an expression for $\bar{h}_{12}$ in terms of $C, x_{1}$, and $x_{2}$.
(b) Derive an expression for $\bar{h}_{12}$ in terms of $x_{1}, x_{2}$, and the average coefficients $\bar{h}_{1}$ and $\bar{h}_{2}$, corresponding to lengths $x_{1}$ and $x_{2}$, respectively.

Narayan Hari
Narayan Hari
Numerade Educator
01:19

Problem 14

Experiments to determine the local convection heat transfer coefficient for uniform flow normal to a heated circular disk have yielded a radial Nusselt number distribution of the form
$$
N u_{D}=\frac{h(r) D}{k}=N u_{o}\left[1+a\left(\frac{r}{r_{o}}\right)^{n}\right]
$$
where both $n$ and $a$ are positive. The Nusselt number at the stagnation point is correlated in terms of the Reynolds $\left(R e_{D}=V D / v\right)$ and Prandtl numbers
$$
N u_{o}=\frac{h(r=0) D}{k}=0.814 \operatorname{Re}_{D}^{1 / 2} \mathrm{Pr}^{0.36}
$$
Obtain an expression for the average Nusselt number, $\overline{N u}_{D}=\bar{h} D / k$, corresponding to heat transfer from an isothermal disk. Typically, boundary layer development from a stagnation point yields a decaying convection coefficient with increasing distance from the stagnation point. Provide a plausible explanation for why the opposite trend is observed for the disk.

Manik Pulyani
Manik Pulyani
Numerade Educator
11:24

Problem 15

An experimental procedure for validating results of Problem $6.14$ involves preheating a copper disk to an initial elevated temperature $T_{i}$ and recording its temperature history $T(t)$ as it is subsequently cooled by the impinging flow to a final temperature $T_{f}$. The measured temperature decay may then be compared with predictions based on the correlation for $\overline{N u}_{D}$. Assume that values of $a=0.30$ and $n=2$ are associated with the correlation.

Consider experimental conditions for which a disk of diameter $D=50 \mathrm{~mm}$ and length $L=25 \mathrm{~mm}$ is preheated to $T_{i}=1000 \mathrm{~K}$ and cooled to $T_{f}=400 \mathrm{~K}$ by an impinging airflow at $T_{w}=300 \mathrm{~K}$. The cooled surface of the disk has an emissivity of $\varepsilon=0.8$ and is exposed to large, isothermal surroundings for which $T_{\text {sux }}=T_{\text {e. }}$. The remaining surfaces of the disk are well insulated, and heat transfer through the supporting rod may be neglected. Using results from Problem 6.14, compute and plot temperature histories corresponding to air velocities of $V=4,20$, and $50 \mathrm{~m} / \mathrm{s}$. Constant properties may be assumed for the copper $\left(\rho=8933 \mathrm{~kg} / \mathrm{m}^{3}, c_{P}=425 \mathrm{~J} / \mathrm{kg} \cdot \mathrm{K}, k=386 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right)$ and air $\left(\nu=38.8 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}, \quad k=0.0407 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}\right.$, $P r=0.684)$.

Nathan Prins
Nathan Prins
Numerade Educator
01:22

Problem 16

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?

Amany Waheeb
Amany Waheeb
Numerade Educator
02:17

Problem 17

Consider the rotating disk of Problem 6.16. A diskshaped, stationary plate is placed a short distance away from the rotating disk, forming a gap of width $g$. The stationary plate and ambient air are at $T_{x}=20^{\circ} \mathrm{C}$. If the flow is laminar and the gap-to-radius ratio, $G=g / r_{e}$, is small, the local radial Nusselt number distribution is of the form
$$
N u_{r}=\frac{h(r) r}{k}=70\left(1+e^{-140 \sigma}\right) R e_{\gamma_{s}}^{-0.456} R e_{r}^{0.478}
$$
where $R e_{,}=\Omega r^{2} / \nu$ [Pelle $\mathrm{J} .$, and $\mathrm{S}$. Harmand, Exp. Thermal Fluid Science, 31, 165, 2007]. Determine the value of the average Nusselt number, $\overline{N u}_{D}=\bar{h} D / k$ where $D=2 r_{a r}$. If the rotating disk temperature is $T_{s}=50^{\circ} \mathrm{C}$, what is the total heat flux from the disk's top surface for $g=1 \mathrm{~mm}, \Omega=150 \mathrm{rad} / \mathrm{s}$ ? What is the total electric power requirement? What can you say about the nature of the flow between the disks?

Dominador Tan
Dominador Tan
Numerade Educator
02:00

Problem 18

Consider airflow over a flat plate of length $L=1 \mathrm{~m}$ under conditions for which transition occurs at $x_{c}=0.5 \mathrm{~m}$ based on the critical Reynolds number, $R e_{x, c}=5 \times 10^{5}$.
(a) Evaluating the thermophysical properties of air at $350 \mathrm{~K}$, determine the air velocity.
(b) In the laminar and turbulent regions, the local convection coefficients are, respectively,
$h_{\text {lam }}(x)=C_{\text {lam }} x^{-05}$ and $h_{\text {marb }}=C_{\text {marb }} x^{-0.2}$
where, at $T=350 \mathrm{~K}, C_{\text {lum }}=8.845 \mathrm{~W} / \mathrm{m}^{3 / 2} \cdot \mathrm{K}, C_{\text {tub }}=$ $49.75 \mathrm{~W} / \mathrm{m}^{1.8} \cdot \mathrm{K}$, and $x$ has units of $\mathrm{m}$. Develop an expression for the average convection coefficient, $\bar{h}_{\mathrm{hm}}(x)$, as a function of distance from the leading edge, $x$, for the laminar region, $0 \leq x \leq x_{x}$.
(c) Develop an expression for the average convection coefficient, $\bar{h}_{\text {art }}(x)$, as a function of distance from the leading edge, $x$, for the turbulent region, $x_{c} \leq x \leq L$.
(d) On the same coordinates, plot the local and average convection coefficients, $h_{x}$ and $\bar{h}_{x}$, respectively, as a function of $x$ for $0 \leq x \leq L$.

Chai Santi
Chai Santi
Numerade Educator
01:29

Problem 19

A fan that can provide air speeds up to $50 \mathrm{~m} / \mathrm{s}$ is to be used in a low-speed wind tunnel with atmospheric air at $25^{\circ} \mathrm{C}$. If one wishes to use the wind tunnel to study flatplate boundary layer behavior up to Reynolds numbers of $R e_{x}=10^{8}$, what is the minimum plate length that should be used? At what distance from the leading edge would transition occur if the critical Reynolds number were $R e_{x, c}=5 \times 10^{5}$ ?

James Kiss
James Kiss
Numerade Educator
02:01

Problem 20

Consider the flow conditions of Example $6.4$ for two situations, one in which the flow is completely laminar, and the second for flow that is tripped to turbulence at the leading edge of the plate. Determine whether there is a plate length $L$ for which the average convection coefficient for laminar flow is the same as the average convection coefficient for turbulent flow. Assume a water temperature of $300 \mathrm{~K}$.

Narayan Hari
Narayan Hari
Numerade Educator
02:00

Problem 21

Assuming a transition Reynolds number of $5 \times 10^{5}$, determine the distance from the leading edge of a flat plate at which transition will occur for each of the following fluids when $u_{s}=1 \mathrm{~m} / \mathrm{s}$ : atmospheric air, engine oil, and mercury. In each case, calculate the transition location for fluid temperatures of $27^{\circ} \mathrm{C}$ and $77^{\circ} \mathrm{C}$.

Chai Santi
Chai Santi
Numerade Educator
01:35

Problem 22

To a good approximation, the dynamic viscosity $\mu$, the thermal conductivity $k$, and the specific heat $c_{p}$ are independent of pressure. In what manner do the kinematic viscosity $v$ and thermal diffusivity $\alpha$ vary with pressure for an incompressible liquid and an ideal gas? Determine $\alpha$ of air at $350 \mathrm{~K}$ for pressures of 1,5 , and $10 \mathrm{~atm}$. Assuming a transition Reynolds number of $5 \times 10^{5}$, determine the distance from the leading edge of a flat plate at which transition will occur for air at $350 \mathrm{~K}$ at pressures of 1,5 , and 10 atm with $u_{s}=2 \mathrm{~m} / \mathrm{s}$.

Manik Pulyani
Manik Pulyani
Numerade Educator
01:11

Problem 23

For the situation described in Example 6.4, the boundary layer can be tripped into a turbulent state by applying roughness to the surface of the flat plate at a particular $x$-location. Hence the location where transition occurs, $x_{c}$, can be moved upstream relative to the transition location associated with the smooth plate of the example. Calculate and plot the average convection coefficient over the entire plate $\bar{h}$ for roughness applied over the range $0 \leq x_{r} \leq L$. What values of $x_{r}$ provide the minimum and maximum values of $\bar{h}$ ? Assume the water temperature is $300 \mathrm{~K}$.c

Hast Aggarwal
Hast Aggarwal
Numerade Educator
02:43

Problem 24

Consider a laminar boundary layer developing over a flat plate. The flow is incompressible.
(a) Substitute Equations $6.31$ and $6.32$ into Equation $6.38$ to determine the boundary conditions in dimensional form associated with flow over a flat plate of length $L$.
(b) Substitute Equations $6.31,6.32$, as well as the definition of $R e_{L}$ into Equation 6.35, and compare the resulting expression with Equation 6.28. Note that for a flat plate, $d p / d x=0$ and $u_{s}=V$.

James Kiss
James Kiss
Numerade Educator
02:43

Problem 25

Consider a laminar boundary layer developing over an isothermal flat plate. The flow is incompressible, and viscous dissipation is negligible.
(a) Substitute Equations $6.31$ and $6.33$ into Equation $6.39$ to determine the thermal boundary conditions in dimensional form associated with flow over a flat plate of length $L$ and temperature $T_{s}$.
(b) Substitute Equations 6.31, 6.32, and 6.33, as well as the definitions of $\operatorname{Re}_{L}$ and $P r$, into Equation 6.36, and compare the resulting dimensional expression with Equation 6.29.

James Kiss
James Kiss
Numerade Educator
01:19

Problem 26

Experiments have shown that the transition from laminar to turbulent conditions for flow normal to the axis of a long cylinder occurs at a critical Reynolds number of $R e_{D,} \approx 2 \times 10^{5}$, where $D$ is the cylinder diameter. Moreover, the transition from incompressible to compressible flow occurs at a critical Mach number of $M a_{e}=0.3$. For air at a pressure of $p=1 \mathrm{~atm}$ and temperature $T=27^{\circ} \mathrm{C}$, determine the critical cylinder diameter $D_{c}$ below which, if the flow is turbulent, compressibility effects are likely to be important.

Penny Riley
Penny Riley
Numerade Educator
05:12

Problem 27

An object of irregular shape has a characteristic length of $L=1 \mathrm{~m}$ and is maintained at a uniform surface temperature of $T_{s}=400 \mathrm{~K}$. When placed in atmospheric air at a temperature of $T_{x}=300 \mathrm{~K}$ and moving with a velocity of $V=100 \mathrm{~m} / \mathrm{s}$, the average heat flux from the surface to the air is $20,000 \mathrm{~W} / \mathrm{m}^{2}$. If a second object of the same shape, but with a characteristic length of $L=5 \mathrm{~m}$, is maintained at a surface temperature of $T_{s}=400 \mathrm{~K}$ and is placed in atmospheric air at $T_{\infty}=300 \mathrm{~K}$, what will the value of the average convection coefficient be if the air velocity is $V=20 \mathrm{~m} / \mathrm{s}$ ?

Keshav Singh
Keshav Singh
Numerade Educator
05:33

Problem 28

Experiments have shown that, for airflow at $T_{\infty}=35^{\circ} \mathrm{C}$ and $V_{1}=100 \mathrm{~m} / \mathrm{s}$, the rate of heat transfer from a turbine blade of characteristic length $L_{1}=0.15 \mathrm{~m}$ and surface temperature $T_{\mathrm{s}, 1}=300^{\circ} \mathrm{C}$ is $q_{1}=1500 \mathrm{~W}$. What would be the heat transfer rate from a second turbine blade of characteristic length $L_{2}=0.3 \mathrm{~m}$ operating at $T_{s, 2}=400^{\circ} \mathrm{C}$ in airflow of $T_{x}=35^{\circ} \mathrm{C}$ and $V_{2}=50 \mathrm{~m} / \mathrm{s}$ ? The surface area of the blade may be assumed to be directly proportional to its characteristic length.

Eric Mockensturm
Eric Mockensturm
Numerade Educator
01:24

Problem 29

Experimental measurements of the convection heat transfer coefficient for a square bar in cross flow yielded the following values:
$$
\begin{array}{lll}
\bar{h}_{1}=50 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K} & \text { when } & V_{1}=20 \mathrm{~m} / \mathrm{s} \\
\bar{h}_{2}=40 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K} & \text { when } & V_{2}=15 \mathrm{~m} / \mathrm{s}
\end{array}
$$
Assume that the functional form of the Nusselt number is $\overline{N u}=C R e^{m} P r^{n t}$, where $C, m$, and $n$ are constants.
(a) What will be the convection heat transfer coefficient for a similar bar with $L=1 \mathrm{~m}$ when $V=15 \mathrm{~m} / \mathrm{s}$ ?
(b) What will be the convection heat transfer coefficient for a similar bar with $L=1 \mathrm{~m}$ when $V=30 \mathrm{~m} / \mathrm{s}$ ?
(c) Would your results be the same if the side of the bar, rather than its diagonal, were used as the characteristic length?

Linh Vu
Linh Vu
Numerade Educator
01:24

Problem 29

Experimental measurements of the convection heat transfer coefficient for a square bar in cross flow yielded the following values:
$\begin{array}{lll}\bar{h}_{1}=50 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K} & \text { when } & V_{1}=20 \mathrm{~m} / \mathrm{s} \\ \bar{h}_{2}=40 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K} & \text { when } & V_{2}=15 \mathrm{~m} / \mathrm{s}\end{array}$
Assume that the functional form of the Nusselt number is $\overline{N u}=C R e^{m} P r^{n}$, where $C, m$, and $n$ are constants.
(a) What will be the convection heat transfer coefficient for a similar bar with $L=1 \mathrm{~m}$ when $V=15 \mathrm{~m} / \mathrm{s}$ ?
(b) What will be the convection heat transfer coefficient for a similar bar with $L=1 \mathrm{~m}$ when $V=30 \mathrm{~m} / \mathrm{s}$ ?
(c) Would your results be the same if the side of the bar, rather than its diagonal, were used as the characteristic length?

Linh Vu
Linh Vu
Numerade Educator
07:24

Problem 30

To assess the efficacy of different liquids for cooling an object of given size and shape by forced convection, it is convenient to introduce a fure of merit, $F_{F}$, which combines the influence of all pertinent fluid properties on the convection coefficient. If the Nusselt number is governed by an expression of the form, $\overline{N u_{L}} \sim R e_{L}^{m} \operatorname{Pr} r^{n}$, obtain the corresponding relationship between $F_{F}$ and the fluid properties. For representative values of $m=0.80$ and $n=0.33$, calculate values of $F_{F}$ for air $\left(k=0.026 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \quad v=1.6 \times 10^{-5} \mathrm{~m}^{2} / \mathrm{s}, \quad P r=0.71\right)$, water $\left(k=0.600 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, v=10^{-6} \mathrm{~m}^{2} / \mathrm{s}, \operatorname{Pr}=5.0\right)$, and a dielectric liquid $\left(k=0.064 \mathrm{~W} / \mathrm{m}-\mathrm{K}, \nu=10^{-6} \mathrm{~m}^{2} / \mathrm{s}\right.$, $\operatorname{Pr}=25)$. Which fluid is the most effective cooling agent?

Mahnoor Amin
Mahnoor Amin
Numerade Educator
23:43

Problem 31

Gases are often used instead of liquids to cool electronics in avionics applications because of weight considerations. The cooling systems are often closed so that coolants other than air may be used. Gases with high figures of merit (see Problem 6.30) are desired. For representative values of $m=0.85$ and $n=0.33$ in the expression of Problem $6.30$, determine the figures of merit for air, pure helium, pure xenon $\left(k=0.006 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \mu=24.14 \times 10^{-6} \mathrm{~N} \cdot \mathrm{s} / \mathrm{m}^{2}\right)$, and an ideal He-Xe mixture containing $0.75$ mole fraction of helium $\left(k=0.0713 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \mu=25.95 \times 10^{-6} \mathrm{~N} \cdot \mathrm{s} / \mathrm{m}^{2}\right)$. Evaluate properties at $300 \mathrm{~K}$ and atmospheric pressure. For monatomic gases such as helium and xenon and their mixtures, the specific heat at constant pressure is well described by the relation $c_{p}=(5 / 2) \mathbb{R} / \mathrm{M}$.

CA
Chi-Chung Ai
Numerade Educator
04:48

Problem 33

Consider conditions for which a fluid with a free stream velocity of $V=1 \mathrm{~m} / \mathrm{s}$ flows over a surface with a characteristic length of $L=1 \mathrm{~m}$, providing an average convection heat transfer coefficient of $\bar{h}=100 \mathrm{Wm}^{2} \cdot \mathrm{K}$. Calculate the dimensionless parameters $\overline{N u}_{L}, R e_{L}, P r$, and $\bar{j}_{H}$ for the following fluids: air, engine oil, mercury, and water. Assume the fluids to be at $300 \mathrm{~K}$.

Chai Santi
Chai Santi
Numerade Educator
07:34

Problem 34

Consider the nanofluid of Example 2.2.
(a) Calculate the Prandtl numbers of the base fluid and nanofluid, using information provided in the example problem.
(b) For a geometry of fixed characteristic dimension $L$, and a fixed characteristic velocity $V$, determine the ratio of the Reynolds numbers associated with the two fluids, $R e_{\text {wf }} / R e_{\mathrm{w}_{\mathrm{d}}-}$ Calculate the ratio of the average Nusselt numbers, $\overline{N u}_{L, \text {, d }} / \overline{N u}_{\text {L, b }}$, that is associated with identical average heat transfer coefficients for the two fluids, $\bar{h}_{\mathrm{mf}}=\bar{h}_{\mathrm{bd}}$.
(c) The functional dependence of the average Nusselt number on the Reynolds and Prandtl numbers for a broad array of various geometries may be expressed in the general form
$$
\overline{N u}_{L}=\bar{h} L / k=C R e^{w N} P r^{1 / 3}
$$
where $C$ and $m$ are constants whose values depend on the geometry from or to which convection heat transfer occurs. Under most conditions the value of $m$ is positive. For positive $m$, is it possible for the base fluid to provide greater convection heat transfer rates than the nanofluid, for conditions involving a fixed geometry, the same characteristic velocities, and identical surface and ambient temperatures?

Eduard Sanchez
Eduard Sanchez
Numerade Educator
02:01

Problem 35

For flow over a flat plate of length $L$, the local heat transfer coefficient $h_{x}$ is known to vary as $x^{-1 / 2}$, where $x$ is the distance from the leading edge of the plate. What is the ratio of the average Nusselt number for the entire plate $\left(\overline{N u}_{L}\right)$ to the local Nusselt number at $x=L\left(N u_{L}\right)$ ?

Narayan Hari
Narayan Hari
Numerade Educator
01:05

Problem 36

For laminar boundary layer flow over a flat plate with air at $20^{\circ} \mathrm{C}$ and 1 atm, the thermal boundary layer thickness $\delta$, is approximately $13 \%$ larger than the velocity boundary layer thickness $\delta$. Determine the ratio $\delta / \delta$, if the fluid is ethylene glycol under the same flow conditions.

James Kiss
James Kiss
Numerade Educator
01:13

Problem 37

Sketch the variation of the velocity and thermal boundary layer thicknesses with distance from the leading edge of a flat plate for the laminar flow of air, water, engine oil, and mercury. For each case assume a mean fluid temperature of $300 \mathrm{~K}$.

Kratika Bhadauria
Kratika Bhadauria
Numerade Educator
06:06

Problem 38

Consider parallel flow over a flat plate for air at $300 \mathrm{~K}$ and engine oil at $380 \mathrm{~K}$. The free stream velocity is $u_{x}=2 \mathrm{~m} / \mathrm{s}$. The temperature difference between the surface and the free stream is the same in both cases, with $T_{s}>T_{m}$.
(a) Determine the location where transition to turbulence occurs, $x_{c}$, for both fluids.
(b) For laminar flow over a flat plate, the velocity boundary layer thickness is given by
$$
\frac{\delta}{x}=\frac{5}{\sqrt{R e_{x}}}
$$
Calculate and plot the velocity boundary layer thickness $\delta$ over the range $0 \leq x \leq x_{c}$ for each fluid.
(c) Calculate and plot the thermal boundary layer thickness $\delta_{r}$ for the two fluids over the same range of $x$ used in part (b). At an $x$-location where both fluids experience laminar flow conditions, explain which fluid has the largest temperature gradient at the plate surface, $-\partial T /\left.\partial y\right|_{y=0}$. Which fluid is associated with the largest local Nusselt number $N u$ ? Which fluid is associated with the largest local heat transfer coefficient $h$ ?

Manish Jain
Manish Jain
Numerade Educator
01:27

Problem 39

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 $30 \mathrm{~mW}$.

Mayukh Banik
Mayukh Banik
Numerade Educator
04:06

Problem 40

Consider the electronic elements that are cooled by forced convection in Problem 6.39. The cooling system is designed and tested at sea level $(p=1 \mathrm{~atm})$, but the circuit board is sold to a customer in Mexico City, with an elevation of $2250 \mathrm{~m}$ and atmospheric pressure of $76.5 \mathrm{kPa}$.
(a) Estimate the surface temperature of the chip located $120 \mathrm{~mm}$ from the leading edge of the board when the board is operated in Mexico City. The dependence of various thermophysical properties on pressure is noted in Problem 6.22.
(b) It is desirable for the chip operating temperature to be independent of the location of the customer. What air velocity is required for operation in Mexico City if the chip temperature is to be the same as at sea level?

TP
Tuan Pham
University of Wisconsin - Madison
01:27

Problem 41

Consider the chip on the circuit board of Problem $6.39$. To ensure reliable operation over extended periods, the chip temperature should not exceed $85^{\circ} \mathrm{C}$. Assuming the availability of forced air at $T_{\infty}=25^{\circ} \mathrm{C}$ and applicability of the prescribed heat transfer correlation, compute and plot the maximum allowable chip power dissipation $P_{c}$ as a function of air velocity for $1 \leq V \leq 25 \mathrm{~m} / \mathrm{s}$. If the chip surface has an emissivity of $0.80$ and the board is mounted in a large enclosure whose walls are at $25^{\circ} \mathrm{C}$. what is the effect of radiation on the $P=V$ plot?

Mayukh Banik
Mayukh Banik
Numerade Educator
05:09

Problem 42

The defroster of an automobile functions by discharging warm air on the inner surface of the windshield. To prevent condensation of water vapor on the surface, the temperature of the air and the surface convection coefficient $\left(T_{x, j}, \bar{h}_{j}\right)$ must be large enough to maintain a surface temperature $T_{s i}$ that is at least as high as the dewpoint $\left(T_{u, i} \geq T_{\text {dp }}\right)$.

Sarah Mccrumb
Sarah Mccrumb
Numerade Educator
05:04

Problem 42

A major contributor to product defects in electronic modules relates to stresses induced during thermal cycling (intermittent heating and cooling). For example, in circuit cards having active and passive components with materials of different thermal expansion coefficients, thermal stresses are the principal source of failure in component joints, such as soldered and wired connections. Although concern is generally for fatigue failure resulting from numerous excursions during the life of a product, it is possible to identify defective joints by performing accelerated thermal stress tests before the product is released to the customer. In such cases, it is important to achieve rapid thermal cycling to minimize disruptions to production schedules.

A manufacturer of circuit cards wishes to develop an apparatus for imposing rapid thermal transients on the cards by subjecting them to forced convection characterized by a relation of the form $\overline{N u_{L}}=C R e_{L}^{k \mathrm{e}} P r^{n}$, where $m=0.8$ and $n=0.33$. However, he does not know whether to use air $(k=0.026 \mathrm{~W} / \mathrm{m}=\mathrm{K}$, $\nu=1.6 \times 10^{-5} \mathrm{~m}^{2} / \mathrm{s}, \operatorname{Pr}=0.71$ ) or a dielectric liquid $\left(k=0.064 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, \quad y=10^{-6} \mathrm{~m}^{2} / \mathrm{s}, \quad P r=25\right)$ as the working fluid. Assuming equivalent air and liquid velocities and validity of the lumped capacitance model for the components, obtain a quantitative estimate of the ratio of the thermal time constants for the two fluids. What fluid provides the faster thermal response?

Suzanne W.
Suzanne W.
Numerade Educator
05:09

Problem 43

The defroster of an automobile functions by discharging warm air on the inner surface of the windshield. To prevent condensation of water vapor on the surface, the temperature of the air and the surface convection coefficient $\left(T_{\infty, j}, \overline{h_{i}}\right)$ must be large enough to maintain a surface temperature $T_{s i}$ that is at least as high as the dewpoint $\left(T_{s, i} \geq T_{d \mathrm{p}}\right)$.
Consider a windshield of length $L=800 \mathrm{~mm}$ and thickness $t=6 \mathrm{~mm}$ and driving conditions for which the vehicle moves at a velocity of $V=70 \mathrm{mph}$ in ambient air at $T_{\infty \rho}=-15^{\circ} \mathrm{C}$. From laboratory experiments performed on a model of the vehicle, the average convection coefficient on the outer surface of the windshield is known to be correlated by an expression of the form $\overline{N_{L}}=0.030 \operatorname{Re}_{L}^{0.8} \operatorname{Pr}^{1 / 3}$, where $R e_{L}=V L \nu$. Air properties may be approximated as $k=0.023 \mathrm{~W} / \mathrm{m}=\mathrm{K}$, $v=12.5 \times 10^{-6} \mathrm{~m}^{2} / \mathrm{s}$, and $\operatorname{Pr}=0.71$. If $T_{d p}=10^{\circ} \mathrm{C}$
and $T_{m, j}=50^{\circ} \mathrm{C}$, what is the smallest value of $\bar{h}_{j}$ required to prevent condensation on the inner surface?

Sarah Mccrumb
Sarah Mccrumb
Numerade Educator
05:50

Problem 44

A microscale detector monitors a steady flow $\left(T_{x}=27^{\circ} \mathrm{C}, V=10 \mathrm{~m} / \mathrm{s}\right)$ of air for the possible presence of small, hazardous particulate matter that may be suspended in the room. The sensor is heated to a slightly higher temperature to induce a chemical reaction associated with certain substances of interest that might impinge on the sensor's active surface. The active surface produces an electric current if such surface reactions occur; the electric current is then sent to an alarm. To maximize the sensor head's surface area and, in turn, the probability of capturing and detecting a particle, the sensor head is designed with a very complex shape. The value of the average heat transfer coefficient associated with the heated sensor must be known so that the required electrical power to the sensor can be determined.
Consider a sensor with a characteristic dimension of $L_{s}=80 \mu \mathrm{m}$. A scale model of the sensor is placed in a recirculating (closed) wind tunnel using hydrogen as the working fluid. If the wind tunnel operates at a hydrogen absolute pressure of $0.5 \mathrm{~atm}$ and velocity of $V=0.5 \mathrm{~m} / \mathrm{s}$, find the required hydrogen temperature and characteristic dimension of the scale model, $L_{\mathrm{w}}$.

Lottie Adams
Lottie Adams
Numerade Educator
03:02

Problem 45

A thin, flat plate that is $0.2 \mathrm{~m} \times 0.2 \mathrm{~m}$ on a side is oriented parallel to an atmospheric airstream having a velocity of $40 \mathrm{~m} / \mathrm{s}$. The air is at a temperature of $T_{s}=20^{\circ} \mathrm{C}$, while the plate is maintained at $T_{s}=120^{\circ} \mathrm{C}$. The airflows over the top and bottom surfaces of the plate, and measurement of the drag force reveals a value of $0.075 \mathrm{~N}$. What is the rate of heat transfer from both sides of the plate to the air?

Narayan Hari
Narayan Hari
Numerade Educator
01:25

Problem 46

Atmospheric air is in parallel flow $\left(u_{x}=15 \mathrm{~m} / \mathrm{s}\right.$, $T_{\infty}=15^{\circ} \mathrm{C}$ ) over a flat heater surface that is to be maintained at a temperature of $140^{\circ} \mathrm{C}$. The heater surface area is $0.25 \mathrm{~m}^{2}$, and the airflow is known to induce a drag force of $0.25 \mathrm{~N}$ on the heater. What is the electrical power needed to maintain the prescribed surface temperature?

Dading Chen
Dading Chen
Numerade Educator
02:13

Problem 47

Determine the drag force imparted to the top surface of the flat plate of Example $6.4$ for water temperatures of $300 \mathrm{~K}$ and $350 \mathrm{~K}$. Assume the plate dimension in the z-direction is $W=1 \mathrm{~m}$.

Kratika Bhadauria
Kratika Bhadauria
Numerade Educator
00:17

Problem 48

For flow over a flat plate with an extremely rough surface, convection heat transfer effects are known to be correlated by the expression of Problem 6.32. For airflow at $50 \mathrm{~m} / \mathrm{s}$, what is the surface shear stress at $x=1 \mathrm{~m}$ from the leading edge of the plate? Assume the air to be at a temperature of $300 \mathrm{~K}$.

Mayukh Banik
Mayukh Banik
Numerade Educator
05:13

Problem 49

A thin, flat plate that is $0.2 \mathrm{~m} \times 0.2 \mathrm{~m}$ on a side with rough top and bottom surfaces is placed in a wind tunnel so that its surfaces are parallel to an atmospheric airstream having a velocity of $30 \mathrm{~m} / \mathrm{s}$. The air is at a temperature of $T_{c}=20^{\circ} \mathrm{C}$ while the plate is maintained at $T_{s}=80^{\circ} \mathrm{C}$. The plate is rotated $45^{\circ}$ about its center point, as shown in the schematic. Airflows over the top and bottom surfaces of the plate, and measurement of the heat transfer rate is $2000 \mathrm{~W}$. What is the drag force on the plate?

Vikash Ranjan
Vikash Ranjan
Numerade Educator
03:55

Problem 50

As a means of preventing ice formation on the wings of a small, private aircraft, it is proposed that electric resistance heating elements be installed within the wings. To determine representative power requirements, consider nominal flight conditions for which the plane moves at $100 \mathrm{~m} / \mathrm{s}$ in air that is at a temperature of $-23^{\circ} \mathrm{C}$. If the characteristic length of the airfoil is $L=2 \mathrm{~m}$ and wind tunnel measurements indicate an average friction coefficient of $\bar{C}_{f}=0.0025$ for the nominal conditions, what is the average heat flux needed to maintain a surface temperature of $T_{s}=5^{\circ} \mathrm{C}$ ?

Narayan Hari
Narayan Hari
Numerade Educator
04:22

Problem 51

A circuit board with a dense distribution of integrated circuits (ICs) and dimensions of $120 \mathrm{~mm} \times 120 \mathrm{~mm}$ on a side is cooled by the parallel flow of atmospheric air with a velocity of $2 \mathrm{~m} / \mathrm{s}$.
From wind tunnel tests under the same flow conditions, the average frictional shear stress on the upper surface is determined to be $0.0625 \mathrm{~N} / \mathrm{m}^{2}$. What is the allowable power dissipation from the upper surface of the board if the average surface temperature of the ICs must not exceed the ambient air temperature by more than $25^{\circ} \mathrm{C}$ ? Evaluate the thermophysical properties of air at $300 \mathrm{~K}$.

Dading Chen
Dading Chen
Numerade Educator
27:48

Problem 52

On a summer day the air temperature is $27^{\circ} \mathrm{C}$ and the relative humidity is $30 \%$. Water evaporates from the surface of a lake at a rate of $0.10 \mathrm{~kg} / \mathrm{h}$ per square meter of water surface area. The temperature of the water is also $27^{\circ} \mathrm{C}$. Determine the value of the convection mass transfer coefficient.
6.53 It is observed that a 230 -mm-diameter pan of water at $23^{\circ} \mathrm{C}$ has a mass loss rate of $1.5 \times 10^{-5} \mathrm{~kg} / \mathrm{s}$ when the ambient air is dry and at $23^{\circ} \mathrm{C}$.
(a) Determine the convection mass transfer coefficient for this situation.
(b) Estimate the evaporation mass loss rate when the ambient air has a relative humidity of $50 \%$.
(c) Estimate the evaporation mass loss rate when the water and ambient air temperatures are $47^{\circ} \mathrm{C}$, assuming that the convection mass transfer coefficient remains unchanged and the ambient air is dry.

Chareen Guzman
Chareen Guzman
Numerade Educator
08:04

Problem 54

The rate at which water is lost because of evaporation from the surface of a body of water may be determined by measuring the surface recession rate. Consider a summer day for which the temperature of both the water and the ambient air is $305 \mathrm{~K}$ and the relative humidity of the air is $40 \%$. If the surface recession rate is known to be $0.1 \mathrm{~mm} / \mathrm{h}$, what is the rate at which mass is lost because of evaporation per unit surface area? What is the convection mass transfer coefficient?

Mohammad Mehran
Mohammad Mehran
Numerade Educator
03:06

Problem 55

Photosynthesis, as it occurs in the leaves of a green plant, involves the transport of carbon dioxide $\left(\mathrm{CO}_{2}\right)$ from the atmosphere to the chloroplasts of the leaves. The rate of photosynthesis may be quantified in terms of the rate of $\mathrm{CO}_{2}$ assimilation by the chloroplasts. This assimilation is strongly influenced by $\mathrm{CO}_{2}$ transfer through the boundary layer that develops on the leaf surface. Under conditions for which the density of $\mathrm{CO}_{2}$ is $6 \times 10^{-4} \mathrm{~kg} / \mathrm{m}^{3}$ in the air and $5 \times 10^{-4} \mathrm{~kg} / \mathrm{m}^{3}$ at the leaf surface and the convection mass transfer coefficient is $10^{-2} \mathrm{~m} / \mathrm{s}$, what is the rate of photosynthesis in terms of kilograms of $\mathrm{CO}_{2}$ assimilated per unit time and area of leaf surface?

Pawan Yadav
Pawan Yadav
Numerade Educator
01:37

Problem 56

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 $A$.

Penny Riley
Penny Riley
Numerade Educator
01:45

Problem 57

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?

Narayan Hari
Narayan Hari
Numerade Educator
02:20

Problem 58

Consider conditions for which a fluid with a free stream velocity of $V=1 \mathrm{~m} / \mathrm{s}$ flows over an evaporating or subliming surface with a characteristic length of $L=1 \mathrm{~m}$, providing an average mass transfer convection coefficient of $\bar{h}_{\mathrm{m}}=10^{-2} \mathrm{~m} / \mathrm{s}$. Calculate the dimensionless parameters $\overline{S h}_{L}, R e_{L}, S c$, and $j_{m}$ for the following combinations: airflow over water, airflow over naphthalene, and warm glycerol over ice. Assume a fluid temperature of $300 \mathrm{~K}$ and a pressure of $1 \mathrm{~atm}$.

Ajay Singhal
Ajay Singhal
Numerade Educator
04:58

Problem 59

An object of irregular shape has a characteristic length of $L=1 \mathrm{~m}$ and is maintained at a uniform surface temperature of $T_{s}=325 \mathrm{~K}$. It is suspended in an airstream that is at atmospheric pressure $(p=1 \mathrm{~atm})$ and has a velocity of $V=100 \mathrm{~m} / \mathrm{s}$ and a temperature of $T_{x}=275 \mathrm{~K}$. The average heat flux from the surface to the air is $12,000 \mathrm{~W} / \mathrm{m}^{2}$. Referring to the foregoing situation as case 1 , consider the following cases and determine whether conditions are analogous to those of case 1. Each case involves an object of the same shape, which is suspended in an airstream in the same manner. Where analogous behavior does exist, determine the corresponding value of the average convection coefficient.
(a) The values of $T_{s}, T_{x}$, and $p$ remain the same, but $L=2 \mathrm{~m}$ and $V=50 \mathrm{~m} / \mathrm{s}$.
(b) The values of $T_{x}$ and $T_{\infty}$ remain the same, but $L=2 \mathrm{~m}, V=50 \mathrm{~m} / \mathrm{s}$, and $p=0.2 \mathrm{~atm}$.
(c) The surface is coated with a liquid film that evaporates into the air. The entire system is at $300 \mathrm{~K}$, and the diffusion coefficient for the air-vapor mixture is $D_{\mathrm{AB}}=1.12 \times 10^{-4} \mathrm{~m}^{2} / \mathrm{s}$. Also, $L=2 \mathrm{~m}$, $V=50 \mathrm{~m} / \mathrm{s}$, and $p=1 \mathrm{~atm}$.
(d) The surface is coated with another liquid film for which $D_{\mathrm{AB}}=1.12 \times 10^{-4} \mathrm{~m}^{2} / \mathrm{s}$, and the system is at $300 \mathrm{~K}$. In this case $L=2 \mathrm{~m}, V=250 \mathrm{~m} / \mathrm{s}$, and $p=0.2$ atm.

Khoobchandra Agrawal
Khoobchandra Agrawal
Numerade Educator
06:41

Problem 60

On a cool day in April a scantily clothed runner is known to lose heat at a rate of $500 \mathrm{~W}$ because of convection to the surrounding air at $T_{x}=10^{\circ} \mathrm{C}$. The runner's skin remains dry and at a temperature of $T_{s}=30^{\circ} \mathrm{C}$. Three months later, the runner is moving at the same speed, but the day is warm and humid with a temperature of $T_{x}=30^{\circ} \mathrm{C}$ and a relative humidity of $\phi_{x}=60 \%$. The runner is now drenched in sweat and has a uniform surface temperature of $35^{\circ} \mathrm{C}$. Under both conditions constant air properties may be assumed with $\nu=1.6 \times 10^{-5} \mathrm{~m}^{2} / \mathrm{s}, k=0.026 \mathrm{~W} / \mathrm{m} \cdot \mathrm{K}, P r=0.70$, and $D_{\mathrm{AB}}$ (water vapor-air) $=2.3 \times 10^{-5} \mathrm{~m}^{2} / \mathrm{s}$.
(a) What is the rate of water loss due to evaporation on the summer day?
(b) What is the total convective heat loss on the summer day?

Emily Anderson
Emily Anderson
Numerade Educator
02:47

Problem 61

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.

Lottie Adams
Lottie Adams
Numerade Educator
01:06

Problem 62

An industrial process involves the evaporation of water from a liquid film that forms on a contoured surface. Dry air is passed over the surface, and from laboratory measurements the convection heat transfer correlation is of the form
$$
\overline{N_{L}}=0.43 \operatorname{Re}_{L}^{0.58} P r r^{\Omega .4}
$$
(a) For an air temperature and velocity of $27^{\circ} \mathrm{C}$ and $10 \mathrm{~m} / \mathrm{s}$, respectively, what is the rate of evaporation from a surface of $1-\mathrm{m}^{2}$ area and characteristic length $L=1 \mathrm{~m}$ ? Approximate the density of saturated vapor as $\rho_{A, \text { sat }}=0.0077 \mathrm{~kg} / \mathrm{m}^{3}$.
(b) What is the steady-state temperature of the liquid film?

Manik Pulyani
Manik Pulyani
Numerade Educator
01:22

Problem 63

The naphthalene sublimation technique involves the use of a mass transfer experiment coupled with an analysis based on the heat and mass transfer analogy to obtain local or average convection heat transfer coefficients for complex surface geometries. A coating of naphthalene, which is a volatile solid at room temperature, is applied to the surface and is then subjected to airflow in a wind tunnel. Alternatively, solid objects may be cast from liquid naphthalene. Over a designated time interval, $\Delta t$, there is a discernible loss of naphthalene due to sublimation, and by measuring the surface recession at locations of interest or the mass loss of the sample, local or average mass transfer coefficients may be determined.

Consider a rectangular rod of naphthalene exposed to air in cross flow at $V=10 \mathrm{~m} / \mathrm{s}, T_{\mathrm{s}}=300 \mathrm{~K}$, as in Problem 6.10, except now $c=10 \mathrm{~mm}$ and $d=30 \mathrm{~mm}$. Determine the change in mass of the $L=500$-mm-long rod over a time period of $\Delta t=30 \mathrm{~min}$. Naphthalene has a molecular weight of $M_{\mathrm{A}}=128.16 \mathrm{~kg} / \mathrm{kmol}$, and its solid-vapor saturation pressure at $27^{\circ} \mathrm{C}$ and $1 \mathrm{ltm}$ is $p_{\text {A, } a t}=1.33 \times 10^{-4}$ bar.

Manish Jain
Manish Jain
Numerade Educator
03:31

Problem 64

Consider application of the naphthalene sublimation technique (Problem 6.63) to a gas turbine blade that is coated with naphthalene and has a surface area of $A_{x}=0.05 \mathrm{~m}^{2}$.
To determine the average convection heat transfer coefficient for a representative operating condition, an experiment is performed in which the coated blade is exposed for $30 \mathrm{~min}$ to atmospheric air at the desired velocity and a temperature of $T_{\infty}=27^{\circ} \mathrm{C}$. During the experiment the surface temperature is $T_{s}=27^{\circ} \mathrm{C}$, and at its conclusion the mass of the blade is reduced by $\Delta m=8 \mathrm{~g}$. What is the average convection heat transfer coefficient associated with the operating condition?

Chai Santi
Chai Santi
Numerade Educator
06:20

Problem 65

A manufacturer of ski equipment wishes to develop headgear that will offer enhanced thermal protection for skiers on cold days at the slopes. Headgear can be made with good thermal insulating characteristics, but it tends to be bulky and cumbersome. Skiers prefer comfortable, lighter gear that offers good visibility, but such gear tends to have poor thermal insulating characteristics. The manufacturer decides to take a new approach to headgear design by concentrating the insulation in areas about the head that are prone to the highest heat losses from the skier and minimizing use of insulation in other locations. Hence, the manufacturer must determine the local heat transfer coefficients associated with the human head with a velocity of $V=10 \mathrm{~m} / \mathrm{s}$ directed normal to the face and an air temperature of $-13^{\circ} \mathrm{C}$. A young engineer decides to make use of the heat and mass transfer analogy and the naphthalene sublimation technique (see Problem 6.63) and casts head shapes of solid naphthalene with characteristic dimensions that are half-scale (that is, the models are half as large as the full-scale head).
(a) What wind tunnel velocity $\left(T_{\mathrm{x}}=300 \mathrm{~K}\right)$ is needed to apply the experimental results to the human head associated with $V=10 \mathrm{~m} / \mathrm{s}$ ?
(b) A wind tunnel experiment is performed for $\Delta t=120 \mathrm{~min}, T_{x}=27^{\circ} \mathrm{C}$. The engineer finds that the naphthalene has receded by $\delta_{1}=0.1 \mathrm{~mm}$ at the back of the head, $\delta_{2}=0.32 \mathrm{~mm}$ in the middle of the forehead, and $\delta_{3}=0.64 \mathrm{~mm}$ on the ear. Determine the heat transfer coefficients at these locations for the full-scale head at $-13^{\circ} \mathrm{C}$. The density of solid naphthalene is $\rho_{\mathrm{A}, \text { sol }}=1025 \mathrm{~kg} / \mathrm{m}^{3}$.
(c) After the new headgear is designed, the models are fitted with the new gear (half-scale) and the experiments are repeated. Some areas of the model that were found to have small local heat transfer coefficients are left uncovered since insulating these areas would have little benefit in reducing overall heat losses during skiing. Would you expect the local heat transfer coefficients for these exposed areas to remain the same as prior to fitting the model with the headgear? Explain why.

Mayukh Banik
Mayukh Banik
Numerade Educator
05:23

Problem 66

A streamlined strut supporting a bearing housing is exposed to a hot airflow from an engine exhaust. It is necessary to run experiments to determine the average convection heat transfer coefficient $\bar{h}$ from the air to the strut in order to be able to cool the strut to the desired surface temperature $T_{x}$. It is decided to run mass transfer experiments on an object of the same shape and to obtain the desired heat transfer results by using the heat and mass transfer analogy.
The mass transfer experiments were conducted using a half-size model strut constructed from naphthalene exposed to an airstream at $27^{\circ} \mathrm{C}$. Mass transfer measurements yielded these results:
\begin{tabular}{rr}
\hline \multicolumn{1}{c}{$\boldsymbol{\boldsymbol { e } _ { \boldsymbol { L } }}$} & $\overline{\boldsymbol{S h}}_{\boldsymbol{L}}$ \\
\hline 60,000 & 282 \\
120,000 & 491 \\
144,000 & 568 \\
288,000 & 989 \\
\hline
\end{tabular}
(a) Using the mass transfer experimental results, determine the coefficients $C$ and $m$ for a correlation of the form $\overline{S h}_{L}=C R e_{L}^{m} S c^{1 / 3}$.
(b) Determine the average convection heat transfer coefficient $\bar{h}$ for the full-sized strut, $L_{H}=60 \mathrm{~mm}$, when exposed to a free stream airflow with $V=60 \mathrm{~m} / \mathrm{s}$, $T_{\infty}=184^{\circ} \mathrm{C}$, and $p_{\infty}=1 \mathrm{~atm}$ when $T_{s}=70^{\circ} \mathrm{C}$.
(c) The surface area of the strut can be expressed as $A_{s}=2.2 L_{H} \cdot l$, where $l$ is the length normal to the page. For the conditions of part (b), what is the change in the rate of heat transfer to the strut if the characteristic length $L_{H}$ is doubled?

Khoobchandra Agrawal
Khoobchandra Agrawal
Numerade Educator
01:06

Problem 67

Consider the conditions of Problem 6.3, but with a thin film of water on the surface. If the air is dry and the Schmidt number $S c$ is $0.6$, what is the evaporative mass flux? Is there net energy transfer to or from the water?

Hast Aggarwal
Hast Aggarwal
Numerade Educator
02:34

Problem 68

Consider the conditions of Problem 6.7, for which a heat transfer experiment yielded the prescribed distribution of the local convection coefficient, $h_{x}(x)$. The experiment was performed for surface and free stream temperatures of 310 and $290 \mathrm{~K}$, respectively. Now consider repeating the experiment under conditions for which the surface is coated with a thin layer of naphthalene and both the surface and air are at $300 \mathrm{~K}$. What is the corresponding value of the average convection mass transfer coefficient, $\bar{h}_{m, L}$ ?

Naman Kumar
Naman Kumar
Numerade Educator
13:04

Problem 69

Using the naphthalene sublimation technique, the radial distribution of the local convection mass transfer coefficient for uniform flow normal to a circular disk has been correlated by an expression of the form
$$
S h_{D}=\frac{h_{\mathrm{m}}(r) D}{D_{\mathrm{AB}}}=S h_{o}\left[1+a\left(\frac{r}{r_{o}}\right)^{n}\right]
$$
The stagnation point Sherwood number $\left(S h_{e}\right)$ depends on the Reynolds $\left(R_{e_{D}}=V D / v\right)$ and $S c h m i d t\left(S c=v / D_{\mathrm{AB}}\right)$ numbers, and data have been correlated by the following expression:

Obtain an expression for the average Nusselt number $\left(\overline{N u}_{D}=\bar{h} D / k\right)$ corresponding to heat transfer from an isothermal disk exposed to the foregoing flow conditions. If $a=1.2$ and $n=5.5$, what is the rate of heat transfer from a disk of diameter $D=20 \mathrm{~mm}$ and surface temperature $T_{s}=125^{\circ} \mathrm{C}$ to an airstream for which $R e_{D}=5 \times 10^{4}$ and $T_{=}=25^{\circ} \mathrm{C}$ ? Typically, boundary layer development from a stagnation point yields a decaying convection coefficient with increasing distance from the stagnation point. Provide a plausible explanation for why the opposite trend is observed for the disk.

Brianna Orr
Brianna Orr
Numerade Educator
11:16

Problem 70

To reduce the threat of predators, the sand grouse, a bird of Kenya, will lay its eggs in locations well removed from sources of groundwater. To bring water to its chicks, the grouse will then fly to the nearest source and, by submerging the lower part of its body, will entrain water within its plumage. The grouse will then return to its nest, and the chicks will imbibe water from the plumage. Of course, if the time of flight is too long, evaporative losses could cause a significant reduction in the water content of the plumage, and the chicks could succumb to dehydration.

To gain a better understanding of convective transfer during flight, wind tunnel studies were performed using molded models of the grouse. By heating the portion of the model that corresponds to the water-encapsulating plumage, an average convection heat transfer coefficient was determined. Results for different air speeds and model sizes were then used to develop an empirical correlation of the form
$$
\overline{N u}_{L}=0.034 \operatorname{Re}_{L}^{4 / 5} \operatorname{Pr}^{1 / 3}
$$
The effective surface area of the water-encapsulating portion of the plumage is designated as $A_{x}$, and the characteristic length is defined as $L=\left(A_{s}\right)^{1 / 2}$.

Consider conditions for which a grouse has entrained $0.05 \mathrm{~kg}$ of water within plumage of $A_{x}=0.04 \mathrm{~m}^{2}$ and is retuming to its nest at a constant speed of $V=30 \mathrm{~m} / \mathrm{s}$. The ambient air is stagnant and at a temperature and relative humidity of $T_{x}=37^{\circ} \mathrm{C}$ and $\phi_{x}=25 \%$, respectively. If, throughout the flight, the surface $A_{s}$ is covered with a liquid water film at $T_{s}=32^{\circ} \mathrm{C}$, what is the maximum allowable distance of the nest from the water source, if the bird must return with at least $50 \%$ of its initial water supply?

Jacquelyn Trost
Jacquelyn Trost
Numerade Educator
04:01

Problem 71

A laboratory experiment involves simultaneous heat and mass transfer from a water-soaked towel experiencing irradiation from a bank of radiant lamps and parallel flow of air over its surface. Using a convection correlation to be introduced in Chapter 7 , the average heat transfer convection coefficient is estimated to be $\bar{h}=28.7 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. Assume that the radiative properties of the towel are those of water, for which $\alpha=\varepsilon=$ $0.96$, and that the surroundings are at $300 \mathrm{~K}$.
(a) Determine the rate at which water evaporates from the towel, $n_{\mathrm{A}}(\mathrm{kg} / \mathrm{s})$.
(b) Perform an energy balance on the towel to determine the net rate of radiation transfer, $q_{\mathrm{nal}}(\mathrm{W})$, to the towel. Determine the irradiation $G\left(\mathrm{~W} / \mathrm{m}^{2}\right)$.

Ren Jie Tuieng
Ren Jie Tuieng
Numerade Educator
01:05

Problem 71

In the spring, concrete surfaces such as sidewalks and driveways are sometimes very wet in the morning, even when it has not rained during the night. Typical nighttime conditions are shown in the sketch.
(a) Determine the heat fluxes associated with convection, $q_{\text {com }}$, evaporation, $q_{\text {evap }}$, and radiation exchange with the sky, $q_{\text {rad- }}^{n}$
(b) Do your calculations suggest why the concrete is wet instead of dry? Explain briefly.
(c) Is heat flowing from the liquid layer to the concrete? Or from the concrete to the liquid layer? Determine the heat flux by conduction into or out of the concrete.

Manik Pulyani
Manik Pulyani
Numerade Educator
02:17

Problem 73

Dry air at $32^{\circ} \mathrm{C}$ flows over a wetted (water) plate of $0.2 \mathrm{~m}^{2}$ area. The average convection coefficient is $\bar{h}=20 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$, and the heater power required to maintain the plate at a temperature of $27^{\circ} \mathrm{C}$ is $432 \mathrm{~W}$. Estimate the power required to maintain the wetted plate at a temperature of $37^{\circ} \mathrm{C}$ in dry air at $32^{\circ} \mathrm{C}$ if the convection coefficients remain unchanged.

Nicholas Mogoi
Nicholas Mogoi
Numerade Educator
12:25

Problem 74

Dry air at $32^{\circ} \mathrm{C}$ flows over a wetted plate of length $200 \mathrm{~mm}$ and width $1 \mathrm{~m}$ (case A). An embedded electrical heater supplies $432 \mathrm{~W}$ and the surface temperature is $27^{\circ} \mathrm{C}$
(a) What is the evaporation rate of water from the plate $(\mathrm{kg} / \mathrm{h})$ ?
(b) After a long period of operation, all the water is evaporated from the plate and its surface is dry (case B). For the same free stream conditions and the same heater power as case $A$, estimate the temperature of the plate, $T_{x}$.

Chareen Guzman
Chareen Guzman
Numerade Educator
03:02

Problem 75

A 20 -mm-diameter sphere is suspended in a dry airstream with a temperature of $22^{\circ} \mathrm{C}$. The power supplied to an embedded electrical heater within the sphere is $2.51 \mathrm{~W}$ when the surface temperature is $32^{\circ} \mathrm{C}$. How much power is required to maintain the sphere at $32^{\circ} \mathrm{C}$ if its outer surface has a thin porous covering saturated with water? Evaluate the properties of air and the diffusion coefficient of the air-water vapor mixture at $300 \mathrm{~K}$.

Khoobchandra Agrawal
Khoobchandra Agrawal
Numerade Educator
02:36

Problem 76

A successful California engineer has installed a circular hot tub in his backyard and finds that, for the typical operating conditions shown in the sketch, water must be added at a rate of $0.001 \mathrm{~kg} / \mathrm{s}$ to maintain a fixed water level in the tub.
If the tub is well insulated on its sides and bottom and if the temperature of the makeup water is equal to that of the tub water, at what rate must electrical heaters supply energy to maintain the tub water at $310 \mathrm{~K}$ ?

Keshav Singh
Keshav Singh
Numerade Educator
27:48

Problem 77

It is known that on clear nights the air temperature need not drop below $0^{\circ} \mathrm{C}$ before a thin layer of water on the ground will freeze. Consider such a layer of water on a clear night for which the effective sky temperature is $-30^{\circ} \mathrm{C}$ and the convection heat transfer coefficient due to wind motion is $h=25 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$. The water may be assumed to have an emissivity of $1.0$ and to be insulated from the ground as far as conduction is concerned.
(a) Neglecting evaporation, determine the lowest temperature the air can have without the water freezing.
(b) For the conditions given, estimate the mass transfer coefficient for water evaporation $h_{\mathrm{m}}(\mathrm{m} / \mathrm{s})$.
(c) Accounting now for the effect of evaporation, what is the lowest temperature the air can have without the water freezing? Assume the air to be dry.

Chareen Guzman
Chareen Guzman
Numerade Educator
03:05

Problem 78

An expression for the actual water vapor partial pressure in terms of wet-bulb and dry-bulb temperatures, referred to as the Carrier equation, is given as
$$
p_{v}=p_{g w}-\frac{\left(p-p_{g w}\right)\left(T_{d b}-T_{\mathrm{wb}}\right)}{1810-T_{\mathrm{wb}}}
$$
where $p_{v}, p_{g w}$ and $p$ are the actual partial pressure, the saturation pressure at the wet-bulb temperature, and the total pressure (all in bars), while $T_{\mathrm{db}}$ and $T_{\mathrm{wb}}$ are the dry- and wet-bulb temperatures in kelvins. Consider air at $1 \mathrm{~atm}$ and $37.8^{\circ} \mathrm{C}$ flowing over a wet-bulb thermometer that indicates $21.1^{\circ} \mathrm{C}$.
(a) Using Carrier's equation, calculate the partial pressure of the water vapor in the free stream. What is the relative humidity?
(b) Refer to a psychrometric chart and obtain the relative humidity directly for the conditions indicated. Compare the result with part (a).
(c) Use Equation $6.65$ to determine the relative humidity. Compare the result to parts (a) and (b).

Manik Pulyani
Manik Pulyani
Numerade Educator
27:48

Problem 79

A mist cooler is used to provide relief for a fatigued athlete. Water at $T_{i}=10^{\circ} \mathrm{C}$ is injected as a mist into a fan airstream with ambient temperature of $T_{=}=32^{\circ} \mathrm{C}$. The droplet diameters are $100 \mu \mathrm{m}$. For small droplets the average Nusselt number is correlated by an expression of the form
$$
\overline{N u}_{D}=\bar{h} D / k=2
$$
(a) At the initial time, calculate the rate of convection heat transfer to the droplet, the rate of evaporative heat loss, and the rate of change of temperature of the droplet for two values of the relative humidity of the fan airstream, $\phi_{x}=0.20$ and $0.95$. Explain what is happening to the droplet in each case.
(b) Calculate the steady-state droplet temperature for each of the two relative humidity values in part (a).

Chareen Guzman
Chareen Guzman
Numerade Educator
03:01

Problem 80

A wet-bulb thermometer consists of a mercury-in-glass thermometer covered with a wetted (water) fabric. When suspended in a stream of air, the steady-state thermometer reading indicates the wet-bulb temperature $T_{\mathrm{ub}}$. Obtain an expression for determining the relative humidity of the air from knowledge of the air temperature $\left(T_{\infty}\right)$, the wet-bulb temperature, and appropriate air and water vapor properties. If $T_{\infty}=45^{\circ} \mathrm{C}$ and $T_{w b}=25^{\circ} \mathrm{C}$, what is the relative humidity of the airstream?

Nick Johnson
Nick Johnson
Numerade Educator
04:34

Problem 81

An industrial process involves evaporation of a thin water film from a contoured surface by heating it from below and forcing air across it. Laboratory measurements for this surface have provided the following heat transfer correlation:
$$
\overline{N u_{L}}=0.43 R e_{L}^{0.58} P r^{0.4}
$$
The air flowing over the surface has a temperature of $290 \mathrm{~K}$, a velocity of $10 \mathrm{~m} / \mathrm{s}$, and is completely dry $\left(\phi_{\infty}=0\right)$. The surface has a length of $1 \mathrm{~m}$ and a surface area of $1 \mathrm{~m}^{2}$. Just enough energy is supplied to maintain its steady-state temperature at $310 \mathrm{~K}$.
(a) Determine the heat transfer coefficient and the rate at which the surface loses heat by convection.
(b) Determine the mass transfer coefficient and the evaporation rate $(\mathrm{kg} / \mathrm{h})$ of the water on the surface.
(c) Determine the rate at which heat must be supplied to the surface for these conditions.

Manne Andergronde
Manne Andergronde
Numerade Educator
04:34

Problem 82

A 2-mm-thick layer of water on an electrically heated plate is maintained at a temperature of $T_{w}=340 \mathrm{~K}$, as dry air at $T_{\infty}=300 \mathrm{~K}$ flows over the surface of the water (case A). The arrangement is in large surroundings that are also at $300 \mathrm{~K}$.
(a) If the evaporative flux from the surface of the water to the air is $n_{\mathrm{A}}^{\prime \prime}=0.030 \mathrm{~kg} / \mathrm{s} \cdot \mathrm{m}^{2}$, what is the corresponding value of the convection mass transfer coefficient? How long will it take for the water to completely evaporate?
(b) What is the corresponding value of the convection heat transfer coefficient and the rate at which electrical power must be supplied per unit area of the plate to maintain the prescribed temperature of the water? The emissivity of water is $\varepsilon_{w}=0.95$.
(c) If the electrical power determined in part (b) is maintained after complete evaporation of the water (case B), what is the resulting temperature of the plate, whose emissivity is $\varepsilon_{p}=0.60$ ?

Manne Andergronde
Manne Andergronde
Numerade Educator
27:48

Problem 83

A disk of 20-mm diameter is covered with a water film. Under steady-state conditions, a heater power of $200 \mathrm{~mW}$ is required to maintain the disk-water film at $305 \mathrm{~K}$ in dry air at $295 \mathrm{~K}$ and the observed evaporation rate is $2.55 \times 10^{-4} \mathrm{~kg} / \mathrm{h}$.
(a) Calculate the average mass transfer convection coefficient $\bar{h}_{s}$ for the evaporation process.
(b) Calculate the average heat transfer convection coefficient $\bar{h}$.
(c) Do the values of $\bar{h}_{\mathrm{m}}$ and $\bar{h}$ satisfy the heat-mass analogy?
(d) If the relative humidity of the ambient air at $295 \mathrm{~K}$ were increased from 0 (dry) to $0.50$, but
the power supplied to the heater was maintained at $200 \mathrm{~mW}$, would the evaporation rate increase or decrease? Would the disk temperature increase or decrease?

Chareen Guzman
Chareen Guzman
Numerade Educator
27:48

Problem 84

An experiment is conducted to determine the average mass transfer convection coefficient of a small droplet using a heater controlled to operate at a constant temperature. The power history required to completely evaporate the droplet at a temperature of $37^{\circ} \mathrm{C}$ is shown in the sketch. It was observed that, as the droplet dried, its wetted diameter on the heater surface remained nearly constant at a value of $4 \mathrm{~mm}$.
(a) Calculate the average mass transfer convection coefficient based on the wetted area during the evaporation process when the droplet, heater, and the $d r y$ ambient air are at $37^{\circ} \mathrm{C}$.
(b) How much energy will be required to evaporate the droplet if the dry ambient air temperature is $27^{\circ} \mathrm{C}$, while the droplet-heater temperature remains at $37^{\circ} \mathrm{C}$ ?

Chareen Guzman
Chareen Guzman
Numerade Educator
05:01

Problem 85

It is desired to develop a simple model for predicting the temperature-time history of a plate during the drying cycle in a dishwasher. Following the wash cycle the plate is at $T_{p}(t)=T_{p}(0)=65^{\circ} \mathrm{C}$ and the air in the dishwasher is completely saturated $\left(\phi_{x}=1.0\right)$ at $T_{x}=55^{\circ} \mathrm{C}$. The values of the plate surface area $A_{s}$, mass $M$, and specific heat $c$ are such that $M c / A_{s}=1600 \mathrm{~J} / \mathrm{m}^{2} \cdot \mathrm{K}$.
(a) Assuming the plate is completely covered by a thin film of water and neglecting the thermal resistances of the film and plate, derive a differential equation for predicting the plate temperature as a function of time.
(b) For the initial conditions $(t=0)$ estimate the change in plate temperature with time, $d T / d t\left({ }^{\circ} \mathrm{C} / \mathrm{s}\right)$, assuming that the average heat transfer coefficient on the plate is $3.5 \mathrm{~W} / \mathrm{m}^{2} \cdot \mathrm{K}$.

Keshav Singh
Keshav Singh
Numerade Educator