Week 6_ Principal Stresses and Strains

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    ENEM 14012 Principal stresses andstrains

    Ref Beer 2012

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    Introduction

    In 3D case, stressat a point has sico!ponents

    x y z

    xy yz zx

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    Introduction

    "o# theco!ponents of

    stresses aretransfor!ed undera rotation of aes

    $a!e is the case#ith strains

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    %ransfor!ation of stress plane

    stress

    2D casex

    y xy

    xy

    xy

    xy

    y

    x

    0z zx yz = = =

    , ,x y xy

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    Plane stress

    & thin plate

    %hic'ness is s!allco!pared to other

    di!ension Plane stress(

    independent of )and unifor! o*erthic'ness

    , ,x y xy

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    Plane stress

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    %ransfor!ation of Planestress

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    %ransfor!ation of Planestress

    E+uiliriu! e+uations(2 2

    2 2

    2 2

    2

    2

    0 : cos sin 2 sin cos

    0 : ( ) sin cos (cos sin )

    sin 2 2 sin cos

    cos 2 cos sin

    1 cos 2cos2

    1 cos 2sin

    2

    x x x y xy

    y x y x y xy

    F

    F

    = = + +

    = = +

    =

    =

    +=

    =

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    %ransfor!ation of Planestress

    Puttin- tri-ono!etric relations

    cos 2 sin 22 2

    sin 2 cos 22

    cos 2 sin 2 , 902 2

    x y x y

    x xy

    x y

    x y xy

    x y x y o

    y xy

    x y x y C

    +

    = + +

    = +

    + = = +

    + = + =

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    Principal stresses and !a shearin-

    stress

    It is a circle

    2 2 2 2

    2 2

    2 2 2

    ( ) ( )2 2

    ( )2 2

    ( )

    x y x y

    x x y xy

    x y x y

    ave xy

    x ave x y

    if and R

    R

    +

    + = +

    + = = +

    + =

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    Principal stresses

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    Principal stresses

    Ma *alue of nor!alstress

    sin 2 cos 2 02

    2tan2

    x y

    x y xy

    xy

    P

    x y

    = + =

    =

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    Principal stresses

    %he e+uation de.nest#o an-les that areapart

    /or , apart

    Principal stresses

    Principal planes, no

    shear stress in thisplane

    180o

    P 90o

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    Principal stresses

    Ma and !innor!al stresses

    max min

    2 2

    max,min ( )2 2

    ave ave

    x y x y

    xy

    R and R

    = + =

    + = +

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    Ma shearin- stress

    Point D and E

    rdinate is !ashearin- stress

    &scissa is

    2

    x y

    ave

    +=

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    Ma shearin- stress

    2

    cos 2 sin 22 2

    x yx

    x y x y

    x xy

    +=

    + = + +

    2

    x y

    ave

    +

    =

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    Ma shearin- stress

    2 2

    max

    cos 2 sin 2 02

    tan2

    2

    ( )2

    ,

    2

    x y

    S xy S

    x y

    S

    xy

    x y

    xy

    x y

    ave

    R

    normal stress

    + =

    =

    = = +

    + = =

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    rientation of ele!ent

    /or !a shear and!a nor!al stress

    tan 2

    2

    x y

    Sxy

    =

    2tan 2

    xy

    P

    x y

    =

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    rientation of ele!ent

    Relati*e orientation

    1tan 2

    tan 2

    sin 2 cos20

    cos 2 sin 2

    sin 2 sin 2 cos 2 cos 2 0

    cos(2 2 ) 0

    2 2 90

    45

    S

    P

    s P

    s P

    s P s P

    s P

    o

    s P

    o

    S P

    =

    + =

    + =

    =

    =

    =

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    Mohrs circle( plane stress

    %he circle #e sa# is Mohr circle

    er!an en-ineer tto Mohr 13561718

    %he circle can e used as analternati*e solution of prole!

    Is ased on -eo!etric consideration,not re+uired the use of !an9for!ulas

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    Mohrs circle( plane stress

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    Principal stress and !ai!u! shear

    stress

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    %hin6#alled pressure *essels

    &pplication of planestress

    :all o;ers little

    resistance to endin- Internal forces on the

    #all are tan-ent tothe #all surface

    %9pes( c9lindrical andspherical pressure*essels

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    %hin6#alled pressure *essels

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    $tresses on the #all

    Hoop stress Longitudinal stress

    1

    1

    0 : (2 ) (2 ) 0ZF t x p r x

    pr

    t

    = =

    =

    22

    2

    1 2

    0 : (2 ) 0

    2

    2

    x

    F rt p r

    pr

    t

    = =

    =

    =

    r10

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    $phere

    1 2

    1

    max

    2

    2 4

    pr

    tpr

    t

    = =

    = =