Air at 25 ° C flows at 30 × 10 − 6 k g / s within 1 00 − mm -long channels used to cool a high thermal conductivity metal mold. Assume the flow is hydro-dynamically and thermally fully developed (a) Determine the heat transferred to the air for a circular channel ( D = 10 mm ) when the mold temperature is 5 0 ° C (case A). (b) Using new manufacturing methods (see Problem 8.105), channels of complex cross section can readily fabricated within metal objects, such as molds. Consider air flowing under the same conditions as in case A. except now the channel is segmented into six smaller triangular sections. The flow area of case A is equal to the total (low area of case B. Determine the heat transferred to the air for the segmented channel. (c) Compare the pressure drops for cases A and B
Air at 25 ° C flows at 30 × 10 − 6 k g / s within 1 00 − mm -long channels used to cool a high thermal conductivity metal mold. Assume the flow is hydro-dynamically and thermally fully developed (a) Determine the heat transferred to the air for a circular channel ( D = 10 mm ) when the mold temperature is 5 0 ° C (case A). (b) Using new manufacturing methods (see Problem 8.105), channels of complex cross section can readily fabricated within metal objects, such as molds. Consider air flowing under the same conditions as in case A. except now the channel is segmented into six smaller triangular sections. The flow area of case A is equal to the total (low area of case B. Determine the heat transferred to the air for the segmented channel. (c) Compare the pressure drops for cases A and B
Solution Summary: The author describes the heat transferred to the air for a circular channel. The mass flow rate of air is m_a=pi
Air at
25
°
C
flows at
30
×
10
−
6
k
g
/
s
within
1
00
−
mm
-long channels used to cool a high thermal conductivity metal mold. Assume the flow is hydro-dynamically and thermally fully developed
(a) Determine the heat transferred to the air for a circular channel
(
D = 10 mm
)
when the mold temperature is
5
0
°
C
(case A). (b) Using new manufacturing methods (see Problem 8.105), channels of complex cross section can readily fabricated within metal objects, such as molds. Consider air flowing under the same conditions as in case A. except now the channel is segmented into six smaller triangular sections. The flow area of case A is equal to the total (low area of case B. Determine the heat transferred to the air for the segmented channel. (c) Compare the pressure drops for cases A and B
1. A 40 lb. force is applied at point E. There are pins at
A, B, C, D, and F and a roller at A.
a. Draw a FBD of member EFC showing all the known and
unknown forces acting on it.
b. Draw a FBD of member ABF showing all the known and
unknown forces acting on it.
c. Draw a FBD of member BCD showing all the known and
unknown forces acting on it.
d. Draw a FBD of the entire assembly ADE showing all the
known and unknown forces acting on it.
e. Determine the reactions at A and D.
f. Determine the magnitude of the pin reaction at C.
40 lbs.
B
A
6 in.
4 in.
D
F
-5 in.4 in 4.
A crude oil of specific gravity0.85 flows upward at a volumetric rate of flow of 70litres per
second through
a vertical
venturimeter,with an inlet diameter of 250 mm and a throat
diameter of 150mm. The coefficient
of discharge of venturimeter is 0.96. The vertical
differences betwecen the pressure toppings is
350mm.
i)
Draw a well labeled diagram to represent the above in formation
i)
If the two pressure gauges are connected at the tapings such that they are
positioned at the levels of their corresponding tapping points,
determine the
difference of readings in N/CM² of the two pressure gauges
ii)
If a mercury differential
manometer
is connected in place of pressure gauges,
to the tappings such that the connecting tube up to mercury are filled with oil
determine the difference in the level of mercury column.
Can you solve it analytically using laplace transforms and with Matlab code as well please. Thank You
Vector Mechanics for Engineers: Statics and Dynamics
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