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)?
True and False
Indicate if each statement is true or false.
T/F 1. Rule #1 protects the function of assembly.
T/F 2. One of the fundamental dimensioning rules
requires all dimensions apply in the free-state
condition for rigid parts.
T/F 3. The fundamental dimensioning rules that apply
on a drawing must be listed in the general
notes.
T/F 4. Where Rule #1 applies to a drawing, it limits
the form of every feature of size on the
drawing.
T/F 5. Rule #1 limits the variation between features of
size on a part.
T/F 6. The designer must specify on the drawing
which features of size use Rule #1.
T/F
T/F
T/F
7. Rule #1 applies to nonrigid parts (in the
unrestrained state).
8. A GO gage is a fixed-limit gage.
9. Rule #1 requires that the form of an individual
regular feature of size is controlled by its limits
of size
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