Coated metallic disks are cured by placing them at the top of a cylindrical furnace whose bottom surface is electrically heated and whose sidewall may be approximated as a reradiating surface. Curing is accomplished by maintaining a disk at T 2 = 400 K for an extended period. The electrically heated surface is maintained at T 1 = 800 K and is mounted on a ceramic base material of thermal conductivity k = 20 W/m ⋅ K . The bottom of the base material, as well as the ambient air and large surroundings above the disk, are maintained at a temperature of 300 K. Emissivities of the heater and the disk inner and outer surfaces are ε 1 = 0.9 , ε 2 , i = 0.5 , and ε 2 , o = 0.9 , respectively. Assuming steady-state operation and neglecting convection within the cylindrical cavity, determine the electrical power that must be supplied to the heater and the convection coefficient h that must be maintained at the outer surface of the disk in order to satisfy the prescribed conditions.
Coated metallic disks are cured by placing them at the top of a cylindrical furnace whose bottom surface is electrically heated and whose sidewall may be approximated as a reradiating surface. Curing is accomplished by maintaining a disk at T 2 = 400 K for an extended period. The electrically heated surface is maintained at T 1 = 800 K and is mounted on a ceramic base material of thermal conductivity k = 20 W/m ⋅ K . The bottom of the base material, as well as the ambient air and large surroundings above the disk, are maintained at a temperature of 300 K. Emissivities of the heater and the disk inner and outer surfaces are ε 1 = 0.9 , ε 2 , i = 0.5 , and ε 2 , o = 0.9 , respectively. Assuming steady-state operation and neglecting convection within the cylindrical cavity, determine the electrical power that must be supplied to the heater and the convection coefficient h that must be maintained at the outer surface of the disk in order to satisfy the prescribed conditions.
Solution Summary: The author explains the electrical power that must be supplied to the heater and the heat transfer coefficient.
Coated metallic disks are cured by placing them at the top of a cylindrical furnace whose bottom surface is electrically heated and whose sidewall may be approximated as a reradiating surface. Curing is accomplished by maintaining a disk at
T
2
=
400
K
for an extended period. The electrically heated surface is maintained at
T
1
=
800
K
and is mounted on a ceramic base material of thermal conductivity
k
=
20
W/m
⋅
K
. The bottom of the base material, as well as the ambient air and large surroundings above the disk, are maintained at a temperature of 300 K. Emissivities of the heater and the disk inner and outer surfaces are
ε
1
=
0.9
,
ε
2
,
i
=
0.5
, and
ε
2
,
o
=
0.9
, respectively.
Assuming steady-state operation and neglecting convection within the cylindrical cavity, determine the electrical power that must be supplied to the heater and the convection coefficient h that must be maintained at the outer surface of the disk in order to satisfy the prescribed conditions.
a problem existed at the stocking stations of a mini-load AS/RS (automated storage and retrieval system) of a leading electronics manufacturer (Fig.1). At these stations, operators fill the bin delivered by the crane with material arriving in a tote over a roller conveyor. The conveyor was designed at such a height that it was impossible to reach the hooks comfortably even with the tote extended. Furthermore, cost consideration came into the picture and the conveyor height was not reduced. Instead, a step stool was considered to enable the stocker to reach the moving hooks comfortably. The height of the hooks from the floor is 280.2 cm (AD). The tote length is 54.9 cm. The projection of tote length and arm reach, CB = 66.1 cm. a) What anthropometric design principles would you follow to respectively calculate height, length, and width of the step to make it usable to a large number of people? b) What is the minimum height (EF) of the step with no shoe allowance? c) What is the minimum…
Qu. 5 Composite materials are becoming more widely used in aircraft industry due to their high strength, low weight and excellent corrosion resistant properties. As an engineer who is given task to design the I beam section of an aircraft (see Figure 7) please, answer the following questions given the material properties in Table 3.
Determine the Moduli of Elasticity of Carbon/Epoxy, Aramid/Epoxy, and Boron /Epoxy composites in the longitudinal direction, given that the composites consist of 25 vol% epoxy and 75 vol% fiber.
What are the specific moduli of each of these composites?
What are the specific strengths (i.e. specific UTS) of each of these composites?
What is the final cost of each of these composites?please show all work step by step problems make sure to see formula material science
Mueh
Battery operated train
Coll
160,000kg 0.0005 0.15 5m² 1.2kg/m³
CD
Af Pair
19
пре neng
0.98 0.9
0.88
Tesla Prated
Tesla Trated "wheel ng
Joxle
270 kW
440NM
0,45m 20
8.5kg m2
the middle
Consider a drive cycle of a 500km trip with 3 stops in
Other than the acceleration and deceleration
associated with the three stops, the tran maintains
constat cruise speed velocity of 324 km/hr. The
tran will fast charge at each stop for 15 min at a
rate Peharge = 350 kW
ΟΙ
15MIN
Stop
w charging
(350kW)
(ผม
τ
(AN
GMIJ
t
6M
1) HOW MUCH DISTANCE dace is covered DURING THE
ACCELERATION TO 324 km/hr?
2)
DETERMINE HOW LONG (IN seconds) the tran will
BE TRAVELING AT FULL SPEED
2
?
3) CALCULATE THE NET ENERGY GAW PER STOP
ete
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