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 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 mm and length L = 25 mm is preheated to T i = 1000 K and cooled to T f = 400 K by an impinging airflow at T ∞ = 300 K . The cooled surface of the disk has an emissivity of ε = 0.8 and is exposed to large, isothermal surroundings for which T s u r = T ∞ . 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 m/s . Constant properties may be assumed for the copper ( ρ = 8933 kg/m 3 , c p = 425 J/kg ⋅ K, k = 386 W/m ⋅ K ) and air ( v = 38.8 × 10 − 6 m 2 /s, k = 0.0407 W/m ⋅ k, Pr = 0.684 ) .
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 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 mm and length L = 25 mm is preheated to T i = 1000 K and cooled to T f = 400 K by an impinging airflow at T ∞ = 300 K . The cooled surface of the disk has an emissivity of ε = 0.8 and is exposed to large, isothermal surroundings for which T s u r = T ∞ . 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 m/s . Constant properties may be assumed for the copper ( ρ = 8933 kg/m 3 , c p = 425 J/kg ⋅ K, k = 386 W/m ⋅ K ) and air ( v = 38.8 × 10 − 6 m 2 /s, k = 0.0407 W/m ⋅ k, Pr = 0.684 ) .
Solution Summary: The author explains how to calculate and plot the effect of jet velocity on temperature.
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
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
mm
and length
L
=
25
mm
is preheated to
T
i
=
1000
K
and cooled to
T
f
=
400
K
by an impinging airflow at
T
∞
=
300
K
.
The cooled surface of the disk has an emissivity of
ε
=
0.8
and is exposed to large, isothermal surroundings for which
T
s
u
r
=
T
∞
.
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
m/s
.
Constant properties may be assumed for the copper
(
ρ
=
8933
kg/m
3
,
c
p
=
425
J/kg
⋅
K,
k
=
386
W/m
⋅
K
)
and air
(
v
=
38.8
×
10
−
6
m
2
/s,
k
=
0.0407
W/m
⋅
k,
Pr
=
0.684
)
.
The TPD method measures temperature elevations in a tissue region during a heating pulse
and its later temperature decay after the pulse. It is then using the Pennes bioheat equation to perform a
curve fitting to determine the local blood perfusion rate. If the TPD probe is placed in the vicinity of very
large blood vessel, will the TPD technique provide an accurate measurement of the local blood perfusion
in the vicinity of this large blood vessel? Explain briefly. (Hint: Is the Pennes bioheat equation accurate
surrounding a large blood vessel?)
The principles of Newton’s Law of Cooling.
You can imagine and create your own data.
Discuss the nature and origin of the four (4) types of coffee where it originates. Various settings, formulations, containers, and the number of trials will be properly discussed in their methodology. Once the experimentation has been done, the thermal coefficient shall be computed and recorded. The temperature coefficient acquired at t=0 and t= 5 mins, will be tested at t = 6,7,8,9 and 10 minutes.
If you could really show step by step my professor was out of town during this subject and I am struggling with this concept.
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