Consider a 300 mm × 300 mm window in an aircraft. For a temperature difference of 80 ° C from the inner to the outer surface of the window, calculate the heat loss through L = 10 -mm-thick polycarbonate, soda lime glass, and aerogel windows, respectively. The thermal conductivities of the aerogel and polycarbonate are k a g = 0.014 W/m ⋅ K and k p c = 0.21 W/m ⋅ K, respectively. Evaluate the thermal conductivity of the soda lime glass at 300K. If the aircraft has 130 windows and the cost to heat the cabin air is $ 1 /kW ⋅ h, compare the costs associated with the heat Iossthrough the windows for an 8-hour intercontinental flight.
Consider a 300 mm × 300 mm window in an aircraft. For a temperature difference of 80 ° C from the inner to the outer surface of the window, calculate the heat loss through L = 10 -mm-thick polycarbonate, soda lime glass, and aerogel windows, respectively. The thermal conductivities of the aerogel and polycarbonate are k a g = 0.014 W/m ⋅ K and k p c = 0.21 W/m ⋅ K, respectively. Evaluate the thermal conductivity of the soda lime glass at 300K. If the aircraft has 130 windows and the cost to heat the cabin air is $ 1 /kW ⋅ h, compare the costs associated with the heat Iossthrough the windows for an 8-hour intercontinental flight.
Solution Summary: The author compares the cost of heat loss through polycarbonate, soda-lime glass and aerogel windows for an intercontinental flight.
Consider a
300
mm
×
300
mm
window in an aircraft. For a temperature difference of
80
°
C
from the inner to the outer surface of the window, calculate the heat loss through
L
=
10
-mm-thick
polycarbonate, soda lime glass, and aerogel windows, respectively. The thermal conductivities of the aerogel and polycarbonate are
k
a
g
=
0.014
W/m
⋅
K
and
k
p
c
=
0.21
W/m
⋅
K,
respectively. Evaluate the thermal conductivity of the soda lime glass at 300K. If the aircraft has 130 windows and the cost to heat the cabin air is
$
1
/kW
⋅
h,
compare the costs associated with the heat Iossthrough the windows for an 8-hour intercontinental flight.
Question 6
What kind of problem would arise if components of the strain tensor were defined
as v
Double counting of the normal strains.
Strain discontinuity.
Rotation would lead to a shear strain.
Double counting of the shear strains.
please show steps, thanks
You design a pin joint. The pin is made of a material with the yield strength of 325
MPa and ultimate strength of 500 MPa. The maximum allowed stress in service is
expressed as a tensor
0
100 0
σ
100
0
0 MPa
0
0
Evaluate the safety factor SF for stress in this design.
Write answer unitless rounding to 2 decimal places and enter decimals even if those
are zeros.
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