Heat Transfer HW8a
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California State University, Fullerton *
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Course
4123
Subject
Aerospace Engineering
Date
Jan 9, 2024
Type
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10
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Which fluid at room temperature requires a larger pump to move at a specified velocity in a given tube?
Water
Castor oil
Coconut oil
Engine oil
Engine oil requires a larger pump because of its much larger density.
Hint #1
References
Multiple Choice
Difficulty: Easy
Previous attempt
In fluid flow, which of the following is convenient to work with?
V
initial
,
T
final
V
final
,
T
initial
V
avg
,
T
m
V
avg,
T
final
In fluid flow, it is convenient to work with an average or mean velocity
V
avg
and an average or mean temperature
T
m
which remain constant in incompressible flow when the cross-sectional area of the tube is
constant.
Hint #1
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Multiple Choice
Difficulty: Easy
Previous attempt
The
V
avg
and
T
m
represent the velocity and temperature, respectively, at a cross section if all the particles were at the same velocity and different temperature.
True
False
The
V
avg
and
T
m
represent the velocity and temperature, respectively, at a cross section if all the particles were at the same velocity and temperature.
References
True / False
Difficulty: Easy
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Given are the values of Reynolds number Re
of various flows. Identify the flow which is turbulent.
Re
= 2100
Re
= 1100
Re
= 3990
Re
= 4010
Flow in a smooth pipe is turbulent when the Reynolds number is above 4000.
Hint #1
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Multiple Choice
Difficulty: Easy
Previous attempt
Define hydraulic diameter.
References
Section Break
Difficulty: Easy
The hydraulic diameter is defined such that it reduces to ordinary diameter
D
for non-circular tubes.
True
False
The hydraulic diameter is defined such that it reduces to ordinary diameter
D
for circular tubes since Nu =
hD
h
k
= 0.023Re
0.8
Pr
0.4
.
Hint #1
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True / False
Difficulty: Easy
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How is hydraulic diameter defined in non-circular tubes?
D
h
=
4
A
c
/
p
Hint #1
References
Numeric Response
Difficulty: Easy
Previous attempt
How is hydraulic diameter defined in non-circular tubes?
D
h
=
4
A
c
/
p
Explanation:
For flow-through non-circular tubes, the Reynolds number, as well as the Nusselt number and the friction factor, are based on the hydraulic diameter
D
h
defined as
D
h
= 4
A
c
/
p
, where
A
c
is the cross-sectional
area of the tube and
p
is its perimeter.
Identify the fluid property responsible for the development of the velocity boundary layer and the kinds of fluids.
References
Section Break
Difficulty: Easy
What fluid property is responsible for the development of the velocity boundary layer?
Viscosity of a fluid
Mass density of a fluid
Specific weight of a fluid
Volume of a fluid
The fluid viscosity is responsible for the development of the velocity boundary layer.
Hint #1
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Multiple Choice
Difficulty: Easy
Previous attempt
For the idealized inviscid fluids, there is no velocity boundary layer .
True
False
The fluid viscosity is responsible for the development of the velocity boundary layer. For the idealized inviscid fluids(fluids with zero viscosity), there will be no velocity boundary layer.
Hint #1
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True / False
Difficulty: Easy
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Consider the fully developed region of flow in a circular tube. Identify the correct statements in this context. (Check all that apply.)
The velocity profile will not change in the flow direction.
The velocity profile will change in the flow direction.
The temperature profile will not change in the flow direction.
The temperature profile may change in the flow direction.
In the fully developed region of flow in a circular tube, the velocity profile will not change in the flow direction but the temperature profile may.
Hint #1
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Check All That Apply
Difficulty: Easy
Previous attempt
Which of the following statements is true in case of the fully developed region of flow in a circular tube?
The friction factor is highest at the tube inlet where the thickness of the boundary layer is zero.
The friction factor decreases gradually to the fully developed value.
The friction factor increases gradually to the fully developed value.
The friction factor is lowest at the tube inlet where the thickness of the boundary layer is zero.
The friction factor is highest at the tube inlet where the thickness of the boundary layer is zero, and decreases gradually to the fully developed value. The same is true for turbulent flow.
Hint #1
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Check All That Apply
Difficulty: Easy
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How does the friction factor
f
vary along the flow direction in the fully developed region in laminar flow and turbulent flow?
The friction factor
f
remains constant along the flow direction in the fully developed region in both laminar and turbulent flow.
The friction factor
f
varies along the flow direction in the fully developed region in both laminar and turbulent flow.
The friction factor
f
remains constant along the flow direction in the fully developed region in laminar flow and varies in turbulent flow.
The friction factor
f
varies along the flow direction in the fully developed region in laminar flow and remains constant in turbulent flow.
The friction factor
f
remains constant along the flow direction in the fully developed region in both laminar and turbulent flow.
Hint #1
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Multiple Choice
Difficulty: Easy
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Identify the correct statements in the context of friction factors of laminar and turbulent flows. (Check all that apply.)
In turbulent flow, the tubes with rough surfaces have much higher friction factors than the tubes with smooth surfaces.
In turbulent flow, the tubes with rough surfaces have much lower friction factors than the tubes with smooth surfaces.
In laminar flow, the friction factor is dependent on the surface roughness.
In laminar flow, the friction factor is independent of the surface roughness.
In turbulent flow, the tubes with rough surfaces have much higher friction factors than the tubes with smooth surfaces. In the case of laminar flow, the effect of surface roughness on the friction factor is negligible.
Hint #1
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Check All That Apply
Difficulty: Easy
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Identify the correct expression for hydrodynamic entry length
L
h
for Reynolds number = 20, given that
D
is the tube diameter.
L
h
= 1.3
D
L
h
=
D
L
h
= 1.6
D
L
h
=1.4
D
L
h
= 0.05 × Re ×
D
= 0.05 × 20 ×
D
= 1
D
Hint #1
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Multiple Choice
Difficulty: Easy
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L
h
= 0.05Re
D
L
t
= 0.05RePr
D
L
t
≈
10
D
L
h
≈
10
D
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Match the turbulent and laminar flows (in the left column) to their hydrodynamic and thermal entry lenghts (in the right column).
1. Thermal entry length of laminar flow
2. Hydrodynamic length of turbulent flow
3. Hydrodynamic entry length of laminar flow
4. Thermal entry length of turbulent flow
The hydrodynamic and thermal entry lengths are given as
L
h
= 0.05Re
D
and
L
t
= 0.05RePr
D
for laminar flow, and
L
h
≈
L
t
≈
10
D
in turbulent flow. Noting that Pr >> 1 for oils, the thermal entry length is larger than the
hydrodynamic entry length in laminar flow. In turbulent, the hydrodynamic and thermal entry lengths are independent of Re or Pr numbers, and are comparable in magnitude.
Hint #1
References
Matching
Difficulty: Easy
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Which of the following statements are true for laminar and turbulent flows? (Check all that apply.)
Pr >> 1 for oils, the thermal entry length is larger than the hydrodynamic entry length in laminar flow.
Pr << 1 for oils, the hydrodynamic entry length is larger than the thermal entry length in laminar flow.
Pr << 1 for liquid metals, the thermal entry length is smaller than the hydrodynamic entry length in laminar flow.
Pr << 1 for liquid metals, the hydrodynamic entry length is smaller than the thermal entry length in laminar flow.
In turbulent, the hydrodynamic and thermal entry lengths are independent of Re or Pr numbers, and are comparable in magnitude.
In turbulent, the hydrodynamic and thermal entry lengths are dependent of Re or Pr numbers, and are not comparable in magnitude.
Pr >> 1 for oils, the thermal entry length is larger than the hydrodynamic entry length in laminar flow.
Pr << 1 for liquid metals, the thermal entry length is smaller than the hydrodynamic entry length in laminar flow.
In turbulent, the hydrodynamic and thermal entry lengths are independent of Re or Pr numbers and are comparable in magnitude.
Hint #1
References
Check All That Apply
Difficulty: Easy
Previous attempt
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The region in which the flow is both hydrodynamically and thermally developed is called the _____ region.
hydro-thermal entrance
fully developed
boundary layer
irrotational flow
The region in which the flow is both hydrodynamically (the velocity profile is fully developed and remains unchanged) and thermally (the dimensionless temperature profile remains unchanged) developed is called the
fully developed region.
Hint #1
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Multiple Choice
Difficulty: Easy
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Consider laminar forced convection in a circular tube. The heat transfer coefficient is highest _____.
at the outlet of the tube
at a distance one-fourth of the length of the tube from the tube inlet
at the mid of the tube
at the inlet of the tube
The heat transfer coefficient is highest at the tube inlet where the thickness of thermal boundary layer is zero.
Hint #1
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Multiple Choice
Difficulty: Easy
Previous attempt
For turbulent forced convection in a circular tube, the heat flux will be higher near the inlet because the heat transfer coefficient is highest at the tube inlet where the thickness of thermal boundary layer is zero, and
decreases gradually to the fully developed value.
True
False
For turbulent forced convection in a circular tube, the heat flux will be higher near the inlet because the heat transfer coefficient is highest at the tube inlet where the thickness of thermal boundary layer is zero, and
decreases gradually to the fully developed value.
Hint #1
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True / False
Difficulty: Easy
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Which of the following is an exact representation of the average temperature difference between the fluid and the surface for an entire tube?
∆
T
ln
∆
T
e
∆
T
m
∆
T
diff
The logarithmic mean temperature difference
∆
T
ln
is an exact representation of the average temperature difference between the fluid and the surface for an entire tube. It truly reflects the exponential decay of the
local temperature difference.
Hint #1
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Multiple Choice
Difficulty: Easy
Previous attempt
Consider fluid flow in a tube whose surface temperature remains constant. Identify the appropriate temperature difference for use in Newton’s law of cooling with an average heat transfer coefficient.
∆
T
lm
= (
∆
T
e
–
∆
T
i
)/ ln(
∆
T
e
/
∆
T
i
)
∆
T
lm
= ln(
∆
T
e
–
∆
T
i
)/ (
∆
T
e
/
∆
T
i
)
∆
T
lm
= (
∆
T
e
–
∆
T
i
)/ ln(
∆
T
i
–
∆
T
e
)
∆
T
lm
= ln(
∆
T
e
–
∆
T
i
)/ (
∆
T
i
–
∆
T
e
)
When the surface temperature of a tube is constant, the appropriate temperature difference for use in the Newton's law of cooling is the logarithmic mean temperature difference that can be expressed as
∆
T
lm
= (
∆
T
e
–
∆
T
i
)/ ln(
∆
T
e
/
∆
T
i
)
Hint #1
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Multiple Choice
Difficulty: Easy
Previous attempt
What do small and large NTU values tell about a heat transfer system?
A small value of NTU (NTU < 5) indicates that heat transfer will not increase no matter how much we extend the length of a tube, whereas a large NTU value (NTU > 5) indicates more opportunities for
heat transfer.
A small value of NTU (NTU < 10) indicates that heat transfer will not increase no matter how much we extend the length of a tube, whereas a large NTU value (NTU >10) indicates more opportunities for
heat transfer.
A small value of NTU (NTU < 10) indicates more opportunities for heat transfer, whereas a large NTU value (NTU > 10) indicates that heat transfer will not increase no matter how much we extend the
length of a tube.
A small value of NTU (NTU < 5) indicates more opportunities for heat transfer, whereas a large NTU value (NTU > 5) indicates that heat transfer will not increase no matter how much we extend the
length of a tube.
The number of transfer units NTU is a measure of the heat transfer area and effectiveness of a heat transfer system. A small value of NTU (NTU < 5) indicates more opportunities for heat transfer, whereas a large
NTU value (NTU >5) indicates that heat transfer will not increase no matter how much we extend the length of a tube.
Hint #1
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Multiple Choice
Difficulty: Easy
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Air enters an 18-cm-diameter, 12-m-long underwater duct at 50°C and 1 atm at a mean velocity of 7 m/s and is cooled by the water outside. If the average heat transfer coefficient is 65 W/ m
2
·
K and the tube
temperature is nearly equal to the water temperature of 7°C, determine the exit temperature of air and the rate of heat transfer. The properties of air at a bulk mean temperature of 30°C are
ρ
= 1.164 kg/m
3
and
c
p
= 1007 J/kg·°C. Is this a good assumption?
The exit temperature of air is
12.18
°C.
The rate of heat transfer is
7.88
kW.
30°C
is
an appropriate temperature to evaluate the fluid properties.
Hint #1
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Multi-Answer
Difficulty: Medium
Previous attempt
Air enters an 18-cm-diameter, 12-m-long underwater duct at 50°C and 1 atm at a mean velocity of 7 m/s and is cooled by the water outside. If the average heat transfer coefficient is 65 W/ m
2
·
K and the tube
temperature is nearly equal to the water temperature of 7°C, determine the exit temperature of air and the rate of heat transfer. The properties of air at a bulk mean temperature of 30°C are
ρ
= 1.164 kg/m
3
and
c
p
= 1007 J/kg·°C. Is this a good assumption?
The exit temperature of air is
12.1976 ± 2%
°C.
The rate of heat transfer is
7.8913 ± 2%
kW.
30°C is
an appropriate temperature to evaluate the fluid properties.
Explanation:
The following assumptions have been made here:
1. Steady operating conditions exist.
2. The surface temperature of the duct is constant.
3. The thermal resistance of the duct is negligible.
The mass flow rate of water is
˙
m
=
ρA
c
V
avg
=
ρ
π
D
2
4
V
avg
˙
m
=
1.164 kg/m
3
π
0.18 m)
2
4
(7 m/s)
˙
m
= 0.2073 kg/s
A
s
= π
DL
= π
0.18 m)
12 m
A
s
= 6.786 m
2
The exit temperature of air is determined from
T
e
=
T
s
−
T
s
−
T
i
e
−
hA
s
˙
mc
p
T
e
= 7 −
7 − 50
e
−
(65 ) (6.786)
(0.2073) (1007 )
T
e
= 12.1976°C
The logarithmic mean temperature difference and the rate of heat transfer are
ΔT
lm
=
T
e
−
T
i
ln
T
s
−
T
e
T
s
−
T
i
ΔT
lm
=
12.1976 −50
ln
7 −12.1976
7−50
ΔT
lm
= 17.8904°C
˙
Q
=
hA
s
ΔT
lm
˙
Q
=
65 W/m
2
·°C
6.786 m
2
(17.8904°C)
˙
Q
= 7.8913 kW
The bulk mean temperature here is
( 12.1976 +50 ) °C
2
= 31.1°C.
This is close to 30ºC. Hence, the assumption made here is correct.
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Which of the following is used to determine the volume flow rate in a circular pipe with laminar flow?
.
V
=
V
avg
/2
A
c
.
V
=
V
avg
A
c
=
V
max
/2
A
c
.
V
= 4
V
max
3
.
V
=
3
V
max
4
The volume flow rate in a circular pipe with laminar flow can be determined by measuring the velocity at the centerline in the fully developed region, multiplying it by the cross-sectional area, and dividing the result by
2 since
.
V
=
V
avg
A
c
=
V
max
/2
A
c
Hint #1
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Multiple Choice
Difficulty: Easy
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The average velocity in a circular pipe in fully developed laminar flow can be determined by simply measuring the velocity at
R
/2.
True
False
The average velocity in a circular pipe in fully developed laminar flow cannot be determined by simply measuring the velocity at
R
/2 (midway between the wall surface and the centerline). The mean velocity is
V
max
/2,
but the velocity at
R
/2 is
V R
/2 =
V
max
1
−
r
2
R
2
r
=
R
/ 2
= 3
V
max
/ 4
References
True / False
Difficulty: Easy
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