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8/3/2019 Lecture-02 Introduction to Shearing, Bearing and Maximum Stresses
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STRESS ANALYSISDR. MUHAMMAD ABID
ASSOCIATE PROFESSOR - FME
TOPIC
GIK Institute of Engineering Sciences and Technology
LECTURE
1Introduction
Stress StrainConcepts2
8/3/2019 Lecture-02 Introduction to Shearing, Bearing and Maximum Stresses
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GIK Institute of Engineering Sciences and Technology. L2 - 2
Shearing Stress
Under applied Forces are applied transverse forces P and
Pto the memberAB, Corresponding internal forces act inthe plane of section Cand are called shearing forces.
A
Pave
The corresponding average shear stress is,
The resultant of the internal shear force distribution is
defined as the shearof the section and is equal to the load P.
A
F
A
P
ave
Single ShearA
F
A
P
2ave
Double Shear
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Bearing Stress in Connections
Bolts, rivets, and pins create
stresses on the points of contact
or bearing surfaces of the
members they connect.
dt
P
A
Pb
Corresponding average force
intensity is called the bearing
stress,
The resultant of the force
distribution on the surface isequal and opposite to the force
exerted on the pin.
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Determine the stresses in the
members and connections of
the structure shown.
Stress Analysis & Design Example
Normal stresses:
Rod is in tension
Boom is in compression
Shearing stresses:
Pin C is in single shear
Pin A is in double shear
Pin B is in _______ shear
Bearing stress
At A in the boom AB, 53.3
MPa
At C in Bracket 32 MPa
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cossin
cos
sin
cos
cos
cos
00
2
00
A
P
A
P
A
V
A
P
A
P
A
F
The average normal and shear stresses on
the oblique plane are
Stress on an Oblique Plane
sincos PVPF
Resolve P into components normal and
tangential to the oblique section,
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The maximum normal stress occurs when the
reference plane is perpendicular to the memberaxis,
0
0
m A
P
The maximum shear stress occurs for a plane at
+ 45o with respect to the axis,
00 2
45cos45sinA
P
A
Pm
Maximum Stresses
cossincos0
2
0 A
P
A
P
Normal and shearing stresses on an oblique
plane
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Normal Strain and Stress-Strain Diagram
strainnormal
stress
L
A
P
Brittle Materials
Ductile Materials
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Hookes Law: Modulus of Elasticity
Below the yield stress
ElasticityofModulus
orModulusYoungs
E
E
Strength is affected by alloying,
heat treating, and manufacturing
process but stiffness (Modulus of
Elasticity) is not.
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Elastic vs. Plastic Behavior
If the strain disappears when the
stress is removed, the material is
said to behave elastically.
When the strain does not return
to zero after the stress is
removed, the material is said tobehaveplastically.
The largest stress for which this
occurs is called the elastic limit.
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Fatigue
Fatigue properties are shown onS-N diagrams.
When the stress is reduced below
the endurance limit, fatiguefailures do not occur for any
number of cycles.
A member may fail due tofatigue
at stress levels significantly below
the ultimate strength if subjected
to many loading cycles.
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Deformations Under Axial Loading
AE
P
EE
From Hookes Law:
From the definition of strain:
L
Equating and solving for the deformation,
AE
PL
With variations in loading, cross-section ormaterial properties,
i ii
ii
EA
LP
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221
21
in9.0
in.12
AA
LL
23
3
in3.0
in.16
A
L
Apply free-body analysis to each
component to determine internal forces,
lb1030
lb1015
lb1060
33
32
31
P
P
P
Evaluate total deflection,
in.109.75
3.0
161030
9.0
121015
9.0
121060
1029
1
1
3
333
6
3
33
2
22
1
11
A
LP
A
LP
A
LP
EEA
LP
i ii
ii
in.109.753
in.618.0in.07.1
psi1029 6
dD
EDetermine the deformation of the
steel rod shown under given loads.
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13/29GIK Institute of Engineering Sciences and Technology.
Stresses in Vessels
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Stresses in Vessels
Membrane stress pattern is totally changed for any variation in geometry as shown
in Figure above, i.e.
At Nozzle-cylinder
Flat End of Cylinder
Sphere-cylinder
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Factor of Safety
stressallowablestressultimate
safetyofFactor
all
u
FS
FS
Structural members or machines
must be designed such that theworking stresses are less than the
ultimate strength of the material.
Factor of safety considerations:
uncertainty in material properties
uncertainty of loadings
uncertainty of analyses
number of loading cycles
types of failure
maintenance requirements and
deterioration effects
importance of member to structures
integrity
risk to life and property
influence on machine function
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Stresses in Thin-Walled Pressure Vessels
Cylindrical vessel with principal stresses
1 = hoop stress
2 = longitudinal stress
t
pr
xrpxtFz
1
1 220
Hoop stress:
21
2
22
2
2
20
t
pr
rprtFx
Longitudinal stress:
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Stresses in Thin-Walled Pressure Vessels
PointsA andB correspond to hoop stress, 1,
and longitudinal stress, 2
Maximum in-plane shearing stress:
t
pr
42
12)planeinmax(
Maximum out-of-plane shearing stress
corresponds to a 45o rotation of the plane
stress element around a longitudinal axis
t
pr
22max
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Stresses in Thin-Walled Pressure Vessels
Spherical pressure vessel:
t
pr
221
Mohrs circle for in-plane
transformations reduces to a point
0
constant
plane)-max(in
21
Maximum out-of-plane shearing
stress
t
pr
412
1max
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Stresses in Vessels
Stresses in
Cylindrical Vessel
Stresses in Spherical Vessel
Stresses in Thick
Cylinders
Hoop Stress =
Axial stress =
Hoop = Axial =
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Basic concepts for stress analysis
Equilibrium: external and internal
loading
Strain displacement compatibility
Constitutive relationships (for
material behavior, v,E)
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Stresses in Vessels
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Stresses in Vessels
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Stresses in Vessels
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Stresses in Vessels
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Stresses in Vessels
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Stresses in Vessels
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Stresses in Vessels
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Stresses in Vessels
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Stresses in Vessels
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