ce270 stress mohrs s10 purdue university

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  • 7/25/2019 CE270 Stress Mohrs S10 Purdue University

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    J. Liu CE270 Spring 2010

    CE270 Spring 2010

    Stress Transformations

    Often interested in maximum normal and

    shear stresses at a point and orientation on

    the element

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    Plane Stress

    Stress can be analyzed in a single plane (no

    load on surface)

    Typically on thin sections, such as a beamweb

    x

    y

    z

    x

    y

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    x

    x

    y

    y

    xy

    State of planestress for elementis unique to

    orientation

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    How do we transform the

    stress components when we

    change orientation?

    x

    xy

    Use equilibrium of

    FORCES!

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    First, Sign Convention

    Positive (+) if pointing in (+) direction on (+)

    face

    Positive (+) if pointing in (-) direction on (-)face

    x

    y

    OR normal stress

    (outward)

    shear stress (up on

    right-hand side)

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    x

    xy

    A x face

    Asin

    Acos

    y

    x

    xy

    yx

    )cos)(cos(

    )cos)(sin()sin)(sin()sin)(cos(0

    ''

    A

    AAAAF

    x

    xyy

    xyxx

    4/23/10 Fix! (had them backwards on

    Wednesday)

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    cossin22sin

    sincos2cos

    )cossin2(sincos

    22

    22' xyyxx

    Repeat for other stresses

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    Stress Transformations

    2sin2cos22

    2cos2sin2

    2sin2cos22

    '

    ''

    '

    xyyxyx

    y

    xyyx

    yx

    xyyxyx

    x

    Hibbeler Chp. 9

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    Example

    x

    z

    A

    L

    T=294.5 N-m

    wood grainGiven:

    Wooden shaft

    dia. = 100 mm

    Find:

    stresses parallel

    and perpendicular

    to the grain at

    point A ( to z

    axis)A

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    x

    z

    A

    L

    T=294.5 N-m

    wood grain

    JTcmax

    4)05.0(

    2

    )05.0)(5.294(

    m

    mNm

    Pax 6105.1

    BUT! (+) on (+) face, therefore (+) shear stress

    x

    y

    max

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    x

    z

    A

    L

    T=294.5 N-m

    wood grain

    x

    y

    max

    72

    72

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    x

    z

    A

    L

    T=294.5 N-m

    wood grain

    72

    Perpendicular to grain (could cause splitting)

    2sin2cos

    22

    ' xyyxyx

    y

    MPaPaxy 88.0))72(2(sin)105.1( 6'

    Compression perpendicular to grain

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    x

    z

    A

    L

    T=294.5 N-m

    wood grain

    72

    Parallel to grain (could shear along grain?)

    2cos2sin

    2

    '' xyyx

    yx

    MPaPaxyx 2.1144cos)105.1( 6

    ''

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    Parallel to grain (pulling on grain)

    2sin2cos22

    ' xyyxyx

    x

    MPax 88.0'

    0.88 MPa

    0.88 MPa

    1.2 MPa

    Final

    State ofStress

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    Principal Stresses

    Maximum and minimum normal stresses

    acting at a point

    Can differentiate with respect to and set=0,

    etc., or can use Mohrs Circle

    Equations for plane stress transformation can

    be put into a graphical format

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    Mohrs Circle

    22

    22''

    2'

    2

    2

    xyyx

    yxavg

    yxavgx

    R

    R

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    Sign Convention Mohrs Circle

    positive to the right

    clockwise above,counterclockwise below

    In the kitchen, the clock is above, and the counter is below.

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    General Procedure

    1. Plot C = avg

    2. Plot (x

    ,xy

    ), (y

    ,yx

    )

    3. Determine R

    4. Draw circle

    C

    ( x, xy)

    ( y, yx)x

    y

    avg

    Reference state

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    on element = 2 on Mohrs Circle

    ( x, xy)

    ( y, yx)

    x

    y

    ( y, yx)

    ( x, xy)

    x

    y

    90

    180

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    Principal Stresses

    ( x, xy)

    ( y, yx)

    p from

    reference

    state

    12

    p

    R

    R

    avg

    avg

    2

    1

    1

    2

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    Maximum Shear Stress

    Ryx max''

    ( x, xy)

    ( y, yx)

    s from

    referencestate

    xymax

    s

    45

    9022

    ps

    ps

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    Example

    x

    z

    A

    L

    T=294.5 N-m

    wood grain

    Given:

    Wooden shaft

    dia. = 100 mm

    Find:stresses parallel

    and perpendicular

    to the grain at

    point A ( to zaxis) using Mohrs

    Circle

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    Reference

    state

    x

    y

    max =1.5MPa = R (0, yx)

    (0, xy)

    2 =144

    144 -90 =54

    ( y, yx)

    ( x, xy)

    MPaRx 88.054cos'

    MPaRy 88.054cos'

    MPaRyx 2.154sin''

    C

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    0.88 MPa

    0.88 MPa

    1.2 MPa

    Final

    State of

    Stress

    MPaRx 88.054cos'

    MPaRy 88.054cos' MPaR

    yx

    2.154sin''