Page 428. Sample Problem 6.1.Solve this problem completely;but replace theapplied point-forceon the rightfrom 1.5 kN to 2 kN.Let the one on the left remain unchanged.At the same time, instead of computing the averageshearing stress in each joint at the provided sectionn-n, please find the average shearing stress in each jointfortheworst section of the beamwherever it is(and state/show where it is), not necessarily at the providedlocation ofsectionn-n.Keep in mind that this change will result in many other changes across the board.Discuss all practicalissues in your findings.For example, where is the system likelyto fail in terms of the glued parts, and why?

Elements Of Electromagnetics
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ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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Page 428. Sample Problem 6.1.Solve this problem completely;but replace theapplied point-forceon the rightfrom 1.5 kN to 2 kN.Let the one on the left remain unchanged.At the same time, instead of computing the averageshearing stress in each joint at the provided sectionn-n, please find the average shearing stress in each jointfortheworst section of the beamwherever it is(and state/show where it is), not necessarily at the providedlocation ofsectionn-n.Keep in mind that this change will result in many other changes across the board.Discuss all practicalissues in your findings.For example, where is the system likelyto fail in terms of the glued parts, and why?

A
1.5 KN |
171
¡n
0.4m-
1.5 kN
40.4 m
0.2 m
B
Sample Problem 6.1
Beam AB is made of three plates glued together and is subjected, in its
plane of symmetry, to the loading shown. Knowing that the width of each
glued joint is 20 mm, determine the average shearing stress in each joint
at section n-n of the beam. The location of the centroid of the section
is given in Fig. 1 and the centroidal moment of inertia is known to be
I= 8.63 x 10 m².
20 mm
80 mm
In
20 mm
20 mm
100 mm
1.5 KN
Joint a
-Joint b
60 mm
Fig. 1 Cross-section dimensions with
location of centroid.
STRATEGY: A free-body diagram is first used to determine the shear at
the required section. Eq. (6.7) is then used to determine the average shearing
stress in each joint.
MODELING:
1.5 kN
Vertical Shear at Section n-n. As shown in the free-body diagram in
Fig. 2, the beam and loading are both symmetric with respect to the center
of the beam. Thus, we have A = B = 1.5 kN †.
68.3 mm
A = 1.5 KN
B = 1.5 KN
A = 1.5 KN
Fig. 2 Free-body diagram of beam and segment of beam to left of
section n-n.
Drawing the free-body diagram of the portion of the beam to the left of
section n-n (Fig. 2), we write
+1 EF, = 0:
1.5 kN - V = 0
V = 1.5 kN
Transcribed Image Text:A 1.5 KN | 171 ¡n 0.4m- 1.5 kN 40.4 m 0.2 m B Sample Problem 6.1 Beam AB is made of three plates glued together and is subjected, in its plane of symmetry, to the loading shown. Knowing that the width of each glued joint is 20 mm, determine the average shearing stress in each joint at section n-n of the beam. The location of the centroid of the section is given in Fig. 1 and the centroidal moment of inertia is known to be I= 8.63 x 10 m². 20 mm 80 mm In 20 mm 20 mm 100 mm 1.5 KN Joint a -Joint b 60 mm Fig. 1 Cross-section dimensions with location of centroid. STRATEGY: A free-body diagram is first used to determine the shear at the required section. Eq. (6.7) is then used to determine the average shearing stress in each joint. MODELING: 1.5 kN Vertical Shear at Section n-n. As shown in the free-body diagram in Fig. 2, the beam and loading are both symmetric with respect to the center of the beam. Thus, we have A = B = 1.5 kN †. 68.3 mm A = 1.5 KN B = 1.5 KN A = 1.5 KN Fig. 2 Free-body diagram of beam and segment of beam to left of section n-n. Drawing the free-body diagram of the portion of the beam to the left of section n-n (Fig. 2), we write +1 EF, = 0: 1.5 kN - V = 0 V = 1.5 kN
0.020 m
Neutral axis
Neutral axis
0.100 m-
Fig. 3 Using area above section a-a to
find Q.
0.020 m
= 0.0417 m
₂= 0.0583 m
0.060 m
Fig. 4 Using area below section b-b to
find Q.
ANALYSIS:
Shearing Stress in Joint a. Using Fig. 3, pass the section a-a through
the glued joint and separate the cross-sectional area into two parts. We
choose to determine Q by computing the first moment with respect to the
neutral axis of the area above section a-a.
Q=Ay₁ = [(0.100 m) (0.020 m)] (0.0417 m) = 83.4 x 10m³
Recalling that the width of the glued joint is t = 0.020 m, we use Eq. (6.7)
to determine the average shearing stress in the joint.
Tave =
Tave =
VQ
It
VO
It
=
Shearing Stress in Joint b. Using Fig. 4, now pass section b-b and
compute Q by using the area below the section.
=
(1500 N) (83.4 x 10 m³)
(8.63 x 10
m²) (0.020 m)
Q = Ay₂ = [(0.060 m)(0.020 m)] (0.0583 m) = 70.0 x 10-6; m³
(1500 N) (70.0 x 10 m²)
(8.63 x 10 m²) (0.020 m)
Tave = 725 kPa
Tave = 608 kPa
Transcribed Image Text:0.020 m Neutral axis Neutral axis 0.100 m- Fig. 3 Using area above section a-a to find Q. 0.020 m = 0.0417 m ₂= 0.0583 m 0.060 m Fig. 4 Using area below section b-b to find Q. ANALYSIS: Shearing Stress in Joint a. Using Fig. 3, pass the section a-a through the glued joint and separate the cross-sectional area into two parts. We choose to determine Q by computing the first moment with respect to the neutral axis of the area above section a-a. Q=Ay₁ = [(0.100 m) (0.020 m)] (0.0417 m) = 83.4 x 10m³ Recalling that the width of the glued joint is t = 0.020 m, we use Eq. (6.7) to determine the average shearing stress in the joint. Tave = Tave = VQ It VO It = Shearing Stress in Joint b. Using Fig. 4, now pass section b-b and compute Q by using the area below the section. = (1500 N) (83.4 x 10 m³) (8.63 x 10 m²) (0.020 m) Q = Ay₂ = [(0.060 m)(0.020 m)] (0.0583 m) = 70.0 x 10-6; m³ (1500 N) (70.0 x 10 m²) (8.63 x 10 m²) (0.020 m) Tave = 725 kPa Tave = 608 kPa
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