CEE 377 HW6 SOLUTION
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Mechanical Engineering
Date
Dec 6, 2023
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Homework 6
CEE 377 - Introduction to Structural Design
Problem 1
We have been asked to redesign the roof and add an additional level to a portion of our Seattle hotel. A
restaurant has been added to the top level around the elevator shaft, as shown below. The restaurant portion
has a gable-shaped roof with a slope of 4-on-12 that is supported by four roof trusses along the same grid
lines as the girders. The gable roof is constructed from 1/8-inch plywood and asphalt shingles.
The lower tier of the roof outside of the restaurant will be converted into an outdoor patio area enclosed
by a 3-foot-high parapet wall. The patio area and the restaurant will include a 1-inch cement finish floor,
and the roof slab thickness has been increased to 6 inches. Assume that all rainwater on the restaurant roof
is collected in gutters and deposited away from the building. For the patio, primary drainage is provided
by a single 6-inch drain pipe. Secondary drainage occurs through a 6-inch circular scupper located 2 inches
above the primary drainage system. The design 15-minute/100-year rainfall intensity for Seattle is
i
= 2.38
in./hr, and the ground snow load is
p
g
= 25 psf. Given the updated layout, determine
the rain load,
R
, on the lower portion of the roof.
all relevant snow loads,
S
, on both the lower and upper tier of the roof, including any snow drift.
the new live load for the restaurant and the new live roof load for the outdoor patio.
the updated demand on girder B and beam A supporting the roof level.
Use the tributary area
approach.
the demand on an internal roof truss (e.g., the truss along the line adjacent to girder B).
1
20
′
5
′
10
′
5
′
20
′
3 @ 9
′
= 27
′
(Typical)
Opening
Girders
(Typ.)
Beams
(Typ.)
Beam A
Girder B
Restaurant
Patio
Secondary Drainage
Primary Drainage
3 @ 15
′
= 45
′
15
′
3 @ 27
′
= 81
′
Ground Floor
First Story
Second Story
Restaurant
Patio
Rain Load
We assume that only the rain from the patio will accumulate and flow out through the drainage system.
The drainage area is
A
= (54 ft)(60 ft) = 3240 ft
2
, and the design rainfall intensity is
i
= 2
.
38 in./hr,
resulting in a flow rate of
Q
= 0
.
0104
Ai
= 0
.
0104(3240)(2
.
38) =
80.2 gal/min.
Using this data, for a 6-inch circular scupper, Table C8.3-5 allows us to interpolate between 3 inches
(55 gal/min) and 4 inches (90 gal/min). For
Q
= 80.2 gal/min, this gives us
d
h
= 3
.
72 inches. Since
2
the depth to the secondary drainage is
d
s
= 2 inches, the rain load is
R
=
5
.
2
(
2
+
3
.
72
) =
29
.
74
psf
Snow Loads
Here we will need to consider both the balanced and unbalanced loads on the restaurant roof as well
as the balanced and drift loads on the patio area. In both cases, we will start with a flat roof snow
load.
For a ground snow load of
p
g
= 25 psf, assuming
C
e
= 1
.
0 (Surface Roughness B, Partial
Exposure),
C
t
= 1
.
0 (No thermal modifications necessary), and
I
s
= 1
.
0 (Risk Category II), we have
p
f
= 0
.
7(1)(1)(1)(25) = 17
.
5 psf.
–
Restaurant Roof
Balanced Load:
p
f
= 17
.
5 psf
Unbalanced Load: For
p
g
= 25 psf and
W
= 13
.
5 ft, we have to use the special note in Figure
7.6-1 for low
W
. In this case,
W
is the minimum of 20 ft, so we have
h
d
= 1
.
45 in. Per the note,
h
d
cannot exceed
p
I
s
p
g
W/
4
γ
. The specific weight of the snow is
γ
= 0
.
13
p
g
+ 14 = 17
.
25
pcf, thus
h
d
= 1
.
45 in
<
q
I
s
p
g
W/
4
γ
=
p
1
.
0(25)(13
.
5)
/
(4
∗
17
.
25) = 2
.
21 in
⇐
✓
We can use
h
d
= 1
.
45 in. For a roof slope of 4 on 12, we have
S
= 3
.
0, thus the intensity of
the drift surcharge is
h
d
γ/
√
S
= 14
.
4 psf and the horizontal extent is 8
√
Sh
d
/
3 = 6
.
7 ft.
17
.
5 psf
13
.
5 ft
13
.
5 ft
Balanced Loading
Condition
4
12
5
.
25 psf
31
.
9 psf
14
.
4 psf
13.5’
6.7’
6.8’
Unbalanced Loading
Condition
4
12
–
Patio Roof
Balanced Load: We can use the same balanced snow load on the patio that we used on the
restaurant roof, as none of our factors need to be modified. Thus,
p
f
= 17
.
5 psf.
Drift Load: For a specific weight of 17.25 pcf, we have
h
b
=
p
f
/γ
= 1
.
01 ft,
h
c
= 15
−
1
.
01 =
13
.
99 ft,
h
c
/h
b
= 13
.
85
>
0
.
2, and drift loads must be considered. The drift height is then
the maximum of the leeward drift (
l
u
= 27 ft
, h
d
= 1
.
75 ft) and the windward drift (
l
u
=
54 ft
, h
d
= 0
.
75(2
.
4) = 1
.
8 ft). Windward drift controls, and we have
h
d
= 1
.
8 ft. Because
h
d
< h
c
, the extent of the drift is
w
= 4
h
d
= 7
.
2 ft, and we have
p
d
= 1
.
8(17
.
25) = 31
.
1 psf.
ASCE 7-16 Section 7.8 reminds us to calculate drift surcharges next to the 3-foot parapet
walls using the windward drift approach. For winds blowing right to left, we have
l
u
= 54 ft
and
h
d
= 0
.
75(2
.
4) = 1
.
8 ft.
For winds blow top to bottom or bottom to top, we have
l
u
= 60 ft, and given the nature of Figure 7.6-1 this will be close enough that we can also use
h
d
= 1
.
8 ft, corresponding to
p
d
= 31
.
1 psf.
3
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7
.
2
′
39
.
6
′
7
.
2
′
3
′
48
.
6 psf
17
.
5 psf
48
.
6 psf
Live and Live Roof Loads
The live and live roof loads are found in ASCE 7-16 Table 4.3-1
–
Restaurant:
Dining rooms and restaurants have a live load of
L = 100 psf
, which is nonre-
duceable. There is a roof live load associated with the restaurant, which has an ordinary pitched
roof live load of 20 psf. This can be reduced as well, with a tributary area of (27’)(20’) = 540
sq ft and roof slope of
F
= 4 inches of rise per foot of run. The corresponding live roof load is
L
r
= (1
.
2
−
0
.
001(540))(1
.
0)(20 psf) = 13
.
2 psf.
–
Patio: The patio area of the roof requires a bit of thought, since there is not an item specifically
calling out a patio. Looking at the roof loading, the most sensible option is to use ”Roof areas
used for occupants”, since the idea would be that the patio would host restaurant guests and
other visitors. In this case, we would again use
L
r
= 100 psf
. ASCE 7-16 Section 4.8.3 tells us
that occupiable roofs are allowed to use reduced live loads in the same way that we would do for
an interior floor load, but for values of 100 psf, we cannot reduce.
Dead Loads
While not explicitly stated, to determine the updated demands on girder B and beam
A, as well as the roof truss, we will need to calculated dead loads.
–
Restaurant Roof: 1/8-inch plywood = 0.4 psf, asphalt shingles = 2 psf
–
Patio: 1-inch cement floor finish = 32 psf, concrete roof slab = (138 pcf)(6”)(1/12) = 69 psf
For determining loads on beam A and girder B, we will have, in both cases, a simply supported beam
subjected to distributed loads. Both members are on the patio area, where the dead load is 32 + 69 = 101
psf, the live roof load is 100 psf, and the rain load is 29.7 psf.
Beam A has a tributary width of 9 feet,
and girder B has a tributary width of 20 feet, and the corresponding uniformly distributed loads are shown
below.
Load
Beam A
Girder B
Dead
0.909 k/ft
2.02 k/ft
Live Roof
0.900 k/ft
2.00 k/ft
Rain
0.267 k/ft
0.59 k/ft
It is evident that the live roof load will control over the rain load, but we have not considered the snow load.
That is because both members are situated within the drift surcharge, so we have to consider how we will
calculate and distribute the additional load.
Let’s start with Beam A. As shown below, a portion of the drift extends into the tributary width for
Beam A. The easiest way to handle that is to smooth the triangular portion across the entire tributary
width.
w
S
= 17
.
5 psf(9 ft) + 0
.
5(11
.
7 psf)(2
.
7 ft) = 0
.
173 k
/
ft
Beam A
Trib Width
9 ft
2.7 ft
17.5 psf
29.2 psf
4
So we have four load types (dead, live roof, rain, snow), which requires us to consider two load combina-
tions
1
.
4
w
D
=
1
.
4(0
.
909 k
/
ft) = 1
.
27 k
/
ft
1
.
2
w
D
+ 1
.
6(
w
L
r
or
w
R
or
w
S
)
=
1
.
2
w
D
+ 1
.
6
w
L
r
=
1
.
2(0
.
909 k
/
ft) + 1
.
6(0
.
900 k
/
ft) = 2
.
53 k
/
ft
⇐
CONTROLS
20 ft
2
.
60 k
/
ft
This results in shear and moment demands of
V
max
=
V
support
=
wL
2
= 25
.
3 kip
M
max
=
M
midspan
=
wL
2
8
= 127 k
·
ft
We can take a similar approach for Girder B, but we have to consider the nonuniformity of the snow load.
Our snow loading condition is distributed as shown below, including the 20-foot tributary width associated
with girder B.
7
.
2 ft
19
.
8 ft
0
.
972 k
/
ft
0
.
350 k
/
ft
We know that the maximum shear will still occur at a support, but the maximum moment no longer occurs
at midspan. In fact, a static analysis of this beam will find that
V
max
= 6
.
77 kip at the left support and
M
max
= 34
.
6 k
·
ft approximately 12.9 feet from the left support. In this case, we compare the snow load
demands with those of the live roof load (which we know will control over rain), and we find that the live
roof load of 100 psf gives
V
max
=
wL
2
=
100 psf(20 ft)(27 ft)
2
= 27 kip
M
max
=
wL
2
8
=
100 psf(20 ft)(27 ft)
2
8
= 182
.
25 k
·
ft
This is much higher than the maximum snow load, and occurs in the same location as the dead load demands,
where, for the 2.02 k/ft dead load calculated above, we have
V
max
= 27
.
3 kip and
M
max
= 184 k
·
ft.
Applying the appropriate load combination, we find:
V
max
=
1
.
2
V
D
+ 1
.
6
V
L
r
= 1
.
2(27
.
3 kip) + 1
.
6(27 kip) = 76
.
0 kip
M
max
=
1
.
2
M
D
+ 1
.
6
M
L
r
= 1
.
2(184 k
·
ft) + 1
.
6(182 k
·
ft) = 512 k
·
ft
Lastly, we look to determine the demands on an interior roof truss. In this case, we consider the interior
truss with a tributary width of 20 feet, similar to the girders. We can use a tributary area type approach
to carry the dead, live roof, and snow loads to the 5 joints along the two diagonals.
The dead load, live
load, and balanced snow load are all distributed evenly uniformly across the roof. For a distributed load of
1 psf, each interior node gets (20 ft)(6.75 ft)(1 psf) = 0.135 kip, and each exterior node sees (20 ft)(3.375
ft)(1 psf) = 0.0675 kip.
Loads at the exterior nodes go directly into the supports, so we only need the
interior nodal values which can be scaled from the 1 psf load. The corresponding internal nodal values are
P
D
= 0
.
125(2
.
4) = 0
.
30 kip,
P
L
r
= 0
.
125(13
.
2) = 1
.
65 kip, and
P
S
= 2
.
19 kip.
The corresponding truss
loads can then be found:
5
Dead Loads, Live Roof, and Balanced Snow Loads
P
P
P
4
.
5
P
4
.
5
P
4
.
5
P
4
.
5
P
−
1
.
5
√
10
P
0
−
0
.
5
√
10
P
−
√
10
P
P
−
1
.
5
√
10
P
0
−
0
.
5
√
10
P
−
√
10
P
1
.
5
P
1
.
5
P
For the unbalanced snow load, we will do a similar tributary area approach.
In this case, we split the
tributary areas as shown below and sum the total load within each 6.25-foot tributary width. Note that the
unbalanced snow load can be unbalanced in either direction and because the structure is symmetric, we can
simply flip the results about the center of the structure.
0
.
105 k
/
ft
0
.
638 k
/
ft
0
.
288 k
/
ft
13.5’
6.7’
6.8’
6.75’
6.75’
6.75’
Unbalanced Snow Loads
0
.
71 kip
3
.
11 kip
2
.
51 kip
7
.
69 kip
7
.
69 kip
11
.
3 kip
11
.
3 kip
−
8
.
11 kip
0
−
1
.
12 kip
−
6
.
99 kip
1
.
91 kip
−
11
.
9 kip
0
−
4
.
91 kip
−
6
.
99 kip
2
.
57 kip
3
.
77 kip
A
B
C
D
E
F
G
H
Let’s tabulate the results.
The values in the table below represents axial forces in the truss members
in kips, and the values in bold represent the maximum of the live roof and snow loads to use in the load
combinations. Because the dead load is so small, we will neglect the 1.4D load combination.
6
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Member
Dead
Live Roof
Snow, Balanced
Snow, Unbalanced (max)
1.2
D
+ 1.6(
L
r
or
S
)
AB
1.35
7.425
9.855
11.3
19.7
BC
1.35
7.425
9.855
11.3
19.7
CD
1.35
7.425
9.855
11.3
19.7
DE
1.35
7.425
9.855
11.3
19.7
AF
-1.42
-7.83
-10.4
-11.9
-20.7
BF
0
0
0
0
0
CF
-0.474
-2.61
-3.46
-4.91
-8.43
CG
0.3
1.65
2.19
1.91
3.86
CH
-0.474
-2.61
-3.46
-4.91
-8.43
DH
0
0
0
0
0
EH
-1.42
-7.83
-10.4
-11.9
-20.7
FG
-0.949
-5.22
-6.93
-6.99
-12.3
GH
-0.949
-5.22
-6.93
-6.99
-12.3
7
Problem 2
Using a derivation similar to what we did in lab and class, show that the effective length factor for a fixed-
pinned column is
K
= 0
.
7. Note: The math on this problem is a bit tedious, and you will end up with a
transcendental equation that must be solved graphically. Use your plotter of choice (Matlab, Mathematica,
etc.) to help find your answer
As always, we can start with the displacement equation and associated derivatives below.
v
(
x
)
=
A
sin
kx
+
B
cos
kx
+
Cx
+
D
v
′
(
x
)
=
kA
cos
kx
−
kB
sin
kx
+
C
v
′′
(
x
)
=
−
k
2
A
sin
kx
−
k
2
B
cos
kx
Let’s assume that the fixed end is located at
x
= 0.
The boundary conditions for this problem are
v
(0) =
v
′
(0) = 0 and
v
(
L
) =
EIv
′′
(
L
) = 0.
Because we know
EI
is not zero, the moment boundary
condition can also be considered to be zero curvature, or
v
′′
(
L
) = 0. We can apply each to solve our system.
v
′
(0) = 0
⇒
kA
+
C
= 0
→
C
=
−
kA
v
′′
(
L
) = 0
⇒
−
k
2
A
sin
kL
−
k
2
B
cos
kL
= 0
→
B
=
−
A
tan
kL
v
(0) = 0
⇒
B
+
D
= 0
→
D
=
−
B
=
A
tan
kL
v
(
L
) = 0
⇒
A
sin
kL
+
B
cos
kL
+
CL
+
D
→
A
sin
kL
−
A
tan
kL
cos
kL
−
AkL
+
A
tan
kL
=
A
(tan
kL
−
kL
) = 0
→
tan
kL
=
kL
This is a transcendental equation that should be solved graphically. One method would be to plot
kL
vs
f
(
kL
) for both sides of the function and find where they overlap, and another would be to plot tan(
kL
)
−
kL
and look find the points where the function crosses zero.
2
4
6
8
10
2
4
6
8
10
We see that the two equation are equal at
kL
= 4
.
49 and
kL
= 7
.
73. We are interested in the lowest
value, so we set
kL
=
r
P
EI
L
= 4
.
49
⇒
P
=
20
.
16
EI
L
2
=
π
2
EI
0
.
4896
L
2
=
π
2
EI
(0
.
700
L
)
2
Here we see that
K
= 0
.
7, as expected.
8
Problem 3
The small building below supports a dead load of 100 psf and a live load of 50 psf (NOTE: treat the live
load as a floor live load not a roof live load). It is supported by 6 columns, all having the cross-sectional
properties shown, a yield stress of 50 ksi and modulus of elasticity of 29000 ksi. The braces can resist both
tension and compression. Neglect other loads. Determine if the edge and corner columns are safe.
Let’s start with the capacities. In the east-west direction, the corner column is pinned at each end while
the edge column is pinned at both ends and the midpoint. In the north-south direction, both columns are
part of a moment frame with pinned supports, thus we can idealize the east-west direction as a pin-slider
connection.
K
= 1
.
0
K
= 1
.
0
K
= 1
.
0
K
= 2
.
0
Corner, E-W
Corner, E-W
Both, N-S
This lets us calculate the following critical loads:
9
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Corner Column, E-W (Weak Axis)
P
cr
=
π
2
EI
y
(
KL
)
2
=
π
2
(29000)(36
.
6)
(1
.
0(24)(12))
2
= 126
.
3 kip
←
CONTROLS
Edge Column, E-W (Weak Axis)
P
cr
=
π
2
EI
y
(
KL
)
2
=
π
2
(29000)(36
.
6)
(1
.
0(12)(12))
2
= 505
.
2 kip
Both Columns, N-S (Strong Axis)
P
cr
=
π
2
EI
x
(
KL
)
2
=
π
2
(29000)(171)
(2
.
0(24)(12))
2
= 147
.
5 kip
Then we need to determine the demands on the columns. We can tabulate our answers below. Remember
that, for columns, ASCE 7-16 Table 4.7-1 tells us
K
LL
= 4.
Member
A
T
A
I
D
L
P
D
P
L
P
u
= 1
.
2
P
D
+ 1
.
6
P
L
ϕP
cr
ft
2
ft
2
psf
psf
kip
kip
kip
kip
Corner Column
360
1440
100
32.3
36
11.6
61.8
113.7
Edge Column
720
2880
100
26.5
72
19.1
116.9
132.8
Here we see that both members have demands less than capacities and are thus safe.
10
Related Questions
Problem 4: A boat is shown in the figure below. Its geometry at the water line is the same as the top
surface. The hull is solid, Is the boat stable?
Top surface
5.5 m
0.3 m
2.4 m
Water surface
1.5 m
Cross section
0.6 m
6,773
FEB
23
rw
MacBook Air
80
888
DII
F1
F2
F3
F4
F5
F6
F7
F8
F9
!
@
$
&
*
1
2
3
4
5
6
7
8
w #
arrow_forward
Help!!! Please answer all Correctly!!! Please
arrow_forward
Learning Goal:
To calculate the normal and shear stresses at a point on the cross
section of a column.
A column with a wide-flange section has a flange width b = 250 mm , height k = 250 mm , web thickness to = 9 mm , and flange thickness t; = 14 mm (Figure 1).
Calculate the stresses at a point 65 mm above the neutral axis if the section supports a tensile normal force N = 2 kN at the centroid, shear force V = 5.8 kN , and
bending moment M = 3 kN - m as shown (Figure 2).
The state of stress at a point is a description of the normal and shear
stresses at that point. The normal stresses are generally due to both
internal normal force and internal bending moment. The net result can
be obtained using the principle of superposition as long as the
deflections remain small and the response is elastic.
Part A- Normal stress
Calculate the normal stress at the point due to the internal normal force on the section.
Express your answer with appropriate units to three significant figures.
• View…
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Help!!! Please answer all Correctly!!! Please
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Problem 1
Learning Goal:
To be able to find the center of gravity, the center of mass, and the centroid of a
composite body.
A centroid is an object's geometric center. For an object of uniform composition,
its centroid is also its center of mass. Often the centroid of a complex composite
body is found by, first, cutting the body into regular shaped segments, and then
by calculating the weighted average of the segments' centroids.
Figure
←d→
x
Part A
IVE ΑΣΦ | 4
T, 1.610,0.5075
Submit
An object is made from a uniform piece of sheet metal. The object has dimensions of a = 1.20 ft ,b= 3.74 ft, and c = 2.45 ft. A hole with diameter d = 0.600 ft is centered at (1.00, 0.600).
Find z, y, the coordinates of the body's centroid. (Figure 1)
Express your answers numerically in feet to three significant figures separated by a comma.
▸ View Available Hint(s)
Previous Answers
Provide Feedback
vec •
* Incorrect; Try Again; 4 attempts remaining
?
1 of 5
ft
Review
>
Next >
Activate Windows
Go to…
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Learning Goal:
A centroid is an object's geometric center. For an object of uniform composition, its centroid is also its
center of mass. Often the centroid of a complex composite body is found by, first, cutting the body into
regular shaped segments, and then by calculating the weighted average of the segments' centroids.An
object is made from a uniform piece of sheet metal. The object has dimensions of a = 1.45 ft, where a is
the diameter of the semi-circle, b = 3.24 ft, and c = 2.10 ft. A hole with diameter d = 0.500 ft is centered
at (1.13, 0.725).
Figure
X
1 of 2
Part A
Find the area of the body. (Figure 1)
Express your answer numerically in feet squared to three significant figures.
► View Available Hint(s)
VE ΑΣΦ41 | vec
A = 1.52
Submit
* Incorrect; Try Again; 5 attempts remaining
Part B
I=
Find I, the x-coordinate of the body's centroid. (Figure 1)
Express your answer numerically in feet to three significant figures.
► View Available Hint(s)
Submit
Previous Answers
Part C
y =…
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please find the solution
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solve all parts
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session.masteringengineering.com
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Writing Assignment 3
Grades for Sean E Stiner: (MA 244-02) (FA24) INTRO TO L...
M MasteringEngineering MasteringComputerScience: Homew...
(b) Success Confirmation of Question Submission | bartleby
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Learning Goal:
To calculate the maximum allowable stresses in pressure vessels,
compute the minimum allowable thickness of pressure vessels to
meet certain constraints, and observe and compare properties of
different pressure vessel shapes.
Engineers are considering two possible vessel shapes for storing
fuel. One shape is cylindrical and the other is spherical. Each
vessel would be constructed out of the same material such that its
hoop stresses and longitudinal stresses would be no greater than
120 MPa. The cylindrical pressure vessel has an inside diameter
of de = 800 mm and a thickness of te = 25.0 mm. The spherical
pressure vessel has an inside diameter of ds = 650 mm and a
thickness of t = 11.0 mm.
▼
Part A - Maximum allowable pressure in the cylindrical pressure vessel
Determine the maximum allowable pressure, pc,max, in the cylindrical pressure vessel.
Express your answer in N to three significant figures.
► View Available Hint(s)
Pc,max =
Submit
ΟΙ ΑΣΦ
↑ vec
Previous Answers…
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Please help me with this question. Thanks so much!
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The question and data are in pictures.
Please answer properly with each steps and explanation.
Best of luck.
Thank you so much in advance.
arrow_forward
Learning Goal:
To calculate the maximum allowable stresses in pressure vessels,
compute the minimum allowable thickness of pressure vessels to
meet certain constraints, and observe and compare properties of
different pressure vessel shapes.
Engineers are considering two possible vessel shapes for storing
fuel. One shape is cylindrical and the other is spherical. Each
vessel would be constructed out of the same material such that its
hoop stresses and longitudinal stresses would be no greater than
140 MPa. The cylindrical pressure vessel has an inside
diameter of dc = 635 mm and a thickness of t = 14 mm . The
spherical pressure vessel has an inside diameter of
de = 735 mm and a thickness of t = 8 mm.
Part A - Maximum allowable pressure in the cylindrical pressure vessel
Determine the maximum allowable pressure, pc,max, in the cylindrical pressure vessel.
Express your answer in MPa to three significant figures.
► View Available Hint(s)
Pc,max =
Submit
ΑΣΦ
Ps,max =
Request Answer
Submit…
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Cooling load computation
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Homework 6- Attempt 1
roblem 9.122
The concrete "gravity" dam is held in place by its own
weight (Figure 1). The density of concrete is
Pc = 2.5 Mg/m³, and water has a density of
P = 1.0 Mg/m³. Suppose that a = 1.5 m
h = 7.5 m.
igure
a
A
-d-a-
-d-
h
Part A
6 of 10
>
■Review
Determine the smallest dimension & that will prevent the dam from overturning
about its end A.
Express your answer to three significant figures and include the
appropriate units.
d= 3.77
A
m
Submit
Previous Answers Request Answer
?
Incorrect; Try Again; 17 attempts remaining
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Learning Goal:
To determine the effects of certain geometric shapes, namely fillets and circular cutouts, on the stress distributions inside a rigid body and to determine the maximum applicable axial force in the same rigid body
while considering these stress concentrations.
The member shown below is made of steel (oallow = 145 MPa ) that is 80 mm thick. The member is subjected to an axial force P that is applied at both ends. Let rf = 10 mm , w = 120 mm , h = 40 mm , and d
= 25 mm
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session.masteringengineering.com
Homework #4
MasteringEngineering MasteringComputerScience: Home...
b My Questions | bartleby
b Password Reset | bartleby
? Help
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Learning Goal:
A column with a wide-flange section has a flange width b = 200 mm , height h = 200 mm, web thickness tw = 8 mm , and flange
thickness tf = 12 mm (Figure 1). Calculate the stresses at a point 75 mm above the neutral axis if the section supports a tensile
To calculate the normal and shear stresses at a point
on the cross section of a column.
normal force N = 2.9 kN at the centroid, shear force V = 4.6 kN, and bending moment M = 4.8 kN • m as shown (Figure 2).
The state of stress at a point is a description of the
normal and shear stresses at that point. The normal
stresses are generally due to both internal normal
force and internal bending moment. The net result can
be obtained using the principle of superposition as
long as the deflections remain small and the response
is elastic.
Part A - Normal stress
Calculate the normal stress at the point due to the internal normal force on the section.
Express your answer with appropriate units to three significant figures.
> View…
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Please help me this question. Need all the answers in detail. Thanks!
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No gpt,solve in paper sheet.
Free body diagram is must and should.
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Help!!! Please answer it correctly
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Please do Asap
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ools
Fundamental of bio.. x
57 (73 of 286)
e cdlaims compliance with the PDF/A standard and has been opened read-only to
4.13 Exercise Problems
Problem 43 The uniform, horizontal beam shown in
Fig. 4.51 is hinged to the wall at point A and supported by ar
a cable attached to the beam at point C. Point C also
th
represents the center of gravity of the beam. At the other
end, the cable is attached to the wall so that it makes an angle
0=68° with the horizontal. If the length of the beam is / =
4 m and the weight of the beam is W = 400 N, calculate the
tension T in the cable and components of the reaction force
on the beam at point A.
Answers: T = 431 N, RAr
= 162 N(→), RAy
= 0
A
Fie
Fig. 4.51 Problem 4.3
Pr
be
4.4 Using two different cable-pulley arrangements
Problem
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You have been contracted by a company to design a system for them. The system requires that you use a very elastic material but the materials available to you are
Material A which has a Young’s Modulus of 210,000 N/mm2 and
Material B which has a Young’s modulus of 12,500 N/mm2
Using the deflection and stiffness equation, which material will best suit the job?
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