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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

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    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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    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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