Air at p = 1 a t m enters a thin-walled ( D = 5-mm diameter) long tube ( L = 2 m ) at an inlet temperature of T m . i = 100 ° C . A constant heat flux is applied to the air from the tube surface. The air mass flow rate is m ˙ = 135 × 10 − 6 k g / s . (a) If the tube surface temperature at the exit is T s , o = 160 ° C , determine the heat rate entering the tube. Evaluate properties at T = 400 K . (b) It the tube length of’ part (a) were reduced to L = 0.2 m , how would flow conditions at the tube exit be affected? Would the value of the heat transfer coefficient at the tube exit be greater than, equal to, or smaller than the heat transfer coefficient for part (a)? (c) If the flow rate of part (a) were increased by a factor of 10, would there be a difference in flow conditions at the lube exit? Would the value of the heat transfer coefficient at the tube exit be greater than, equal to, or smaller than the heat transfer coefficient for part (a)?
Air at p = 1 a t m enters a thin-walled ( D = 5-mm diameter) long tube ( L = 2 m ) at an inlet temperature of T m . i = 100 ° C . A constant heat flux is applied to the air from the tube surface. The air mass flow rate is m ˙ = 135 × 10 − 6 k g / s . (a) If the tube surface temperature at the exit is T s , o = 160 ° C , determine the heat rate entering the tube. Evaluate properties at T = 400 K . (b) It the tube length of’ part (a) were reduced to L = 0.2 m , how would flow conditions at the tube exit be affected? Would the value of the heat transfer coefficient at the tube exit be greater than, equal to, or smaller than the heat transfer coefficient for part (a)? (c) If the flow rate of part (a) were increased by a factor of 10, would there be a difference in flow conditions at the lube exit? Would the value of the heat transfer coefficient at the tube exit be greater than, equal to, or smaller than the heat transfer coefficient for part (a)?
Air at
p
=
1
a
t
m
enters a thin-walled (
D
= 5-mm
diameter) long tube
(
L
=
2
m
)
at an inlet temperature of
T
m
.
i
=
100
°
C
. A constant heat flux is applied to the air from the tube surface. The air mass flow rate is
m
˙
=
135
×
10
−
6
k
g
/
s
. (a) If the tube surface temperature at the exit is
T
s
,
o
=
160
°
C
, determine the heat rate entering the tube. Evaluate properties at
T
=
400
K
. (b) It the tube length of’ part (a) were reduced to
L
=
0.2
m
, how would flow conditions at the tube exit be affected? Would the value of the heat transfer coefficient at the tube exit be greater than, equal to, or smaller than the heat transfer coefficient for part (a)? (c) If the flow rate of part (a) were increased by a factor of 10, would there be a difference in flow conditions at the lube exit? Would the value of the heat transfer coefficient at the tube exit be greater than, equal to, or smaller than the heat transfer coefficient for part (a)?
Please help. I am not sure how to approach this problem. This problem involves heat transfer and internal flow within a pipe. Thank you.
Q=2000J
Tout=?
V(m/s) D=0.1m
air
Air at (2.95x10^2) K is entering in a circular pipe at 101325 Pa as shown in Figure. The velocity of
the air at the pipe entrance is (1.000x10^0) m/s. The diameter of the pipe is 0.1m. Specific gas
constant of air is 287 J/kg-K. Specific heat of air is 1000 J/kg-K. Find the outlet temperature if 2000
J of heat is added to the pipe.
Note: Your answer is assumed to be reduced to the highest power possible.
Your Answer:
x10
Answer
5.0 Air at p=p= 1 atm enters a thin-walled (D=D= 5-mm diameter) long tube (L=L= 2 m) at an inlet temperature of Tm,i=Tm,i= 100°C. A constant heat flux is applied to the air from the tube surface. The air mass flow rate is m˙ =m˙ = 125 × 10-6 kg/s. If the tube surface temperature at the exit is Ts,o=Ts,o= 160°C, determine the heat rate entering the tube, in W. Evaluate properties at T=T=400 K.
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