Stress Strain Relationship for Mild Steel

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    13-1Mechanics of MaterialsStress-Strain Curve for Mild Steel

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    13-2aMechanics of MaterialsDefinitions

    Hookes Law

    Shear Modulus:

    Stress:

    Strain:

    Poissons Ratio:

    Normal stress or strain =

    Shear stress = || to the surface

    " to the surface

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    13-2bMechanics of MaterialsDefinitions

    Uniaxial Load and Deformation

    Thermal Deformation

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    13-3aMechanics of MaterialsStress and Strain

    Thin-Walled Tanks

    Hoop Stress:

    Axial Stress:

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    13-3bMechanics of MaterialsStress and Strain

    Transformation of Axes

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    13-3cMechanics of MaterialsStress and Strain

    Five simplified steps to construct Mohrs circle

    1. Determine the applied stresses (x, y, xy).2. Draw a set of - axes.

    3. Locate the center:

    4. Find the radius (ormax):

    5. Draw Mohrs circle.

    "c =1

    2("

    x+"

    y).

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    13-3d1Mechanics of MaterialsStress and Strain

    For examples 1 and 2, use the following illustration.

    Example 1 (FEIM)The principal stresses (2, 1) are most nearly

    (A) 62400 kPa and 14400 kPa

    (B) 84000 kPa and 28000 kPa

    (C) 70000 kPa and 14000 kPa

    (D) 112000 kPa and 28000 kPa

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    13-3d2Mechanics of MaterialsStress and Strain

    The center of Mohrs circle is at

    "max = (30000 kPa)2+ (24000 kPa)2 = 38419 kPa

    "

    1

    = "c

    # $max

    = (#24000 kPa # 38419 kPa)= #62419 kPa

    "2 = "c+ #max = ($24000 kPa+38419 kPa)=14418 kPa

    Therefore, (D) is correct.

    Using the Pythagorean theorem, the radius of Mohrs circle (max) is:"c =

    1

    2("

    x+"

    y) = 1

    2(#48000 kPa+0)= #24000 kPa

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    13-3d3Mechanics of MaterialsStress and Strain

    Example 2 (FEIM):

    The maximum shear stress is most nearly

    (A) 24000 kPa

    (B) 33500 kPa

    (C) 38400 kPa

    (D) 218000 kPa

    Therefore, (C) is correct.

    In the previous example problem, the radius of Mohrs circle (max) was

    "max = (30000 kPa)2+ (24000 kPa)2

    = 38419 kPa (38400 kPa)

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    13-3eMechanics of MaterialsStress and Strain

    General Strain

    Note that "x is no longer proportional to #x.

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    13-3fMechanics of MaterialsStress and Strain

    Static Loading Failure Theory

    Maximum Normal Stress: A material fails if

    Or

    " # St

    " # Sc

    This is true of brittle materials.

    For ductile materials:

    Maximum Shear

    Distortion Energy (von Mises Stress)

    Tmax

    =max"1 # "2

    2,

    "1 # "3

    2,

    "2 # "3

    2

    $

    %

    &&

    '

    (

    ))>Syt

    2

    "# = 12

    #1

    $ #2( )

    2

    + #1

    $ #3( )

    2

    + #2

    $ #3( )

    2%&' (

    )*>S

    yt

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    13-3gMechanics of MaterialsStress and Strain

    Torsion

    For a body with radius rbeingstrained to an angle , the shear

    strain and stress are:

    " = r

    d#

    dz " =G# =Gr

    d$

    dz

    For a body with polar moment of

    inertia (J), the torque (T) is:

    T=G

    d"

    dzr

    2dA

    A# =GJ

    d"

    dz

    The shear stress is:

    "#z=Gr T

    GJ= Tr

    J

    For a body, the general angulardisplacement () is:

    " =

    T

    GJdz

    0

    L

    #

    For a shaft of length (L), the totalangular displacement () is:

    Torsional stiffness:

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    13-3hMechanics of MaterialsStress and Strain

    Hollow, Thin-Walled Shafts

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    13-4aMechanics of MaterialsBeams

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    13-4bMechanics of MaterialsBeams

    Load, Shear, and Moment Relations

    Load:

    Shear:

    For a beam deflected to a radius of curvature (), the axial strain at a

    distance (y) from the neutral axis is "x = #y/$.

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    13-4c1Mechanics of MaterialsBeams

    Shear and Bending Moment Diagrams

    Example 1 (FEIM):

    Draw the shear and bending moment diagrams for the following beam.

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    13-4c2Mechanics of MaterialsBeams

    Shear is undefined at concentrated force points, but just short ofx= 12 m

    Rl+Rr = 100 Nm

    "

    #$

    %

    &'16 m( ) =1600 N

    Rl= (8)(R

    r(4)= 0

    Therefore, Rl= 533.3 N and Rr= 1066.7 N

    So the shear diagram is:

    From 0 m to 12 m, V= Rl" 100

    N

    m

    #

    $

    %&

    '

    (x= 533.3 N" 100N

    m

    #

    $

    %&

    '

    (x; 0 m < x < 12 m

    V(12") = 533.3 N" 100N

    m

    #

    $%

    &

    '((12 m) = "666.7 N

    V=1600 N" 100N

    m

    #

    $%

    &

    '(x; 12 < x ) 16 m

    From 12 m to 16 m, V=V(12")+R

    r" (100 N)(x"12)

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    13-4c3Mechanics of MaterialsBeams

    The bending moment is the integral of the shear.

    M= Sdx0

    12

    " + Sdx12

    x

    " = #800+ 1600 N#100N

    mx

    $

    %&

    '

    ()

    0

    12

    " dx

    = "800 N #m+ 1600 N( )x" 50N

    m

    $

    %

    &'

    (

    )x2

    $

    %

    &'

    (

    )

    12

    x

    M= 533.3x 50x2; 0 m < x< 12 m

    M= "800 N #m+ 1600 N( )x" 50N

    m

    $

    %&

    '

    ()x

    2 " 1600 N( ) 12 m( )+ 50N

    m

    $

    %&

    '

    ()12 m( )

    2

    M= "12800 N #m+ 1600 N( )x" 50N

    m

    $

    %&

    '

    ()x

    2

    12 m

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    13-4c4Mechanics of MaterialsBeams

    The bending moment diagram is:

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    13-4d1Mechanics of MaterialsBeams

    Example 2 (FEIM):The vertical shear for the section at the midpoint of the beam shown is

    (A) 0

    (B)

    (C) P

    (D) none of these

    Drawing the force diagram and the shear diagram,

    Therefore, (A) is correct.

    1

    2P

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    13-4d2Mechanics of MaterialsBeams

    Example 3 (FEIM):For the shear diagram shown, what is the maximum bending moment? The

    bending moment at the ends is zero, and there are no concentrated couples.

    (A) 8 kNm

    (B) 16 kNm

    (C) 18 kNm

    (D) 26 kN

    m

    Starting from the left end of the beam, areas begin to cancel after 2 m. Starting

    from the right end of the beam, areas begin to cancel after 4 m. The rectangle on

    the right has an area of 16 kNm. The trapezoid on the left has an area of

    (1/2)(12 kN + 14 kN) (2 m) = 26 kNm. The trapezoid has the largest bending

    moment.

    Therefore, (A) is correct.

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    13-4eMechanics of MaterialsBeams

    Bending Stress

    Deflection

    Shear Stress

    Note: Beam deflection formulas are given in the NCEES Handbook for

    any situation that might be on the exam.

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    13-4fMechanics of MaterialsBeams

    Example (FEIM):

    Find the tip deflection of the beam shown. EI is 3.47 106 Nm2, the

    load is 11379 N/m, and the beam is 3.7 m long.

    From the NCEES Handbook:

    " =w

    oL

    4

    8EI=

    11379N

    m

    #

    $%

    &

    '(3.7 m( )

    4

    8( ) 3.47)106 N *m2( )= 0.077 m

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    13-5aMechanics of MaterialsColumns

    Beam-Columns (Axially Loaded Beams)

    Maximum and minimum stresses in an eccentrically loaded column:

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    13-5cMechanics of MaterialsColumns

    Elastic Strain Energy:

    Strain energy per unit volume for tension: