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
Steam flows steadily through a turbine at a rate of 45,000 lbm/h, entering at 1000 psia and 900°F and leaving at 5 psia as saturated vapor. If the power generated by the turbine is 4.1 MW, determine the rate of heat loss from the steam. The enthalpies are h1 = 1448.6 Btu/lbm and h2 = 1130.7 Btu/lbm.
The rate of heat loss from the steam is Btu/s.
The A/D converter wit the specifications listed below is planned to be used in an environment in which the A/D
converter temperature may change by ± 10 °C. Estimate the contributions of conversion and quantization errors
to the uncertainty in the digital representation of an analog voltage by the converter.
FSO
N
Linearity error
Temperature drift error
Analog to Digital (A/D)
Converter
0-10 V
12 bits
± 3 bits
1 bit/5 °C
6-13. A smooth tube in the form of a circle of radius r rotates in its vertical plane with a
constant angular velocity w. The position of a particle of mass m that slides inside
the tube is given by the relative coordinate p. Find the differential equation for .
e
О
E
g
ω
Figure P6-13
Vector Mechanics for Engineers: Statics and Dynamics
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