Failure Theory for piping material

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    Thermal Strains and Element of the

    Theory of Plasticity

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    Thermal Strains

    Thermal strain is a special class of Elastic strain that

    results fromexpansion with increasing temperature, or

    contraction with decreasing temperature

    Increased temperature causes the atoms to vibrateby

    large amount. In isotropic materials, the effect is the

    same in all directions.

    !er a limited range of temperatures, the thermal

    strains at a gi!en temperature T, can be assumed to beproportional to the change, T.

    ( ) ( )TTT == " #$%&'(

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    where T"is the reference temperature #) " at T"(. The

    coefficient of thermal expansion, , is seen to be in units

    of '*o

    +, thus maing strain dimensionless. Since uniform thermal strains occur in all directions in

    isotropic material, -ooes law for /&0 can be

    generali1ed to include thermal effects.

    ( )[ ] ( )TE

    zyxx ++= '

    ( )[ ] ( )TE zxyy ++=

    '

    ( )[ ] ( )TE

    yxzz ++= '

    #$%&2(

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    The theory of plasticity is concerned with a number of

    different types of problems. It deals with the beha!ior

    of metals at strains where -ooes law is no longer!alid.

    3rom the !iewpoint of design, plasticity is concerned

    with predictingthe safe limitsfor use of a materialunder combined stresses. i.e., the maximum loadwhich

    can be applied to a body without causing4

    Excessi!e 5ielding

    3low 3racture

    Plasticity is also concerned with understanding the

    mechanism of plastic deformation of metals.

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    Plastic deformation is not a re!ersible process, and

    depends on the loading path by which the final state is

    achie!ed. In plastic deformation, there is no easily measured

    constant relating stress to strain as with 5oungs modulus

    for elastic deformation.

    The phenomena of strain hardening, plastic

    anisotropy, elastic hysteresis, and Bauschinger effect

    can not be treated easily without introducing

    considerable mathematical complexity.

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    3igure %&'#a(. Typical true stress&strain cur!es for a ductile metal.

    -ooes law is followed up to the yield stress ", and beyond ",

    the metal deforms plastically.

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    3igure %&'b. Same cur!e as %&'a, except that it shows what happensduring unloading and reloading & -ysteresis. The cur!e will not be

    exactly linear and parallel to the elastic portion of the cur!e.

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    3igure %&'c. Same cur!e as %&'a, but showing 6auschinger effect.

    It is found that the yield stress in tension is greater than the yield

    stress in compression.

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    3igure %&2. Ideali1ed flow cur!es. #a( 7igid ideal plastic material

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    3igure %&2b. Ideal plastic material with elastic region

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    3igure %&2c. Piecewise linear # strain&hardening( material.

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    $ true stress&strain cur!e is fre8uently called a flow

    cur!e, because it gi!es the stress re8uired to cause the

    metal to flow plastically to any gi!en strain. The mathematical e8uation used to describe the stress&

    strain relationship is a power expression of the form4

    where 9 is the stress at ) '." and n, the strain&

    hardening coefficient, is the slope of a log&log of

    E8. %&'

    That is,

    n

    k = #%&'(

    logloglog nK += #%&2(

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    3$I:;7E +7ITE7I$4 3:

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    In applying a yielding criterion, the resistance of a

    material is gi!en by its yield strength.

    In applying a fracture criterion, the ultimate tensilestrength is usually used.

    3ailure criterion for isotropic materials can be

    expressed in the following mathematical form4

    where failure #yielding or fracture( is predicted to occur

    when a specific mathematical functionf of the principal

    normal stresses is e8ual to the failure strength of the

    material, c, from a uniaxial tension test.

    ( ) cf =/2' ,,#%&/(

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    The failure strength is either the yield strength o, or the

    ultimate strength u, depending on whether yielding or

    fracture is of interest.

    :et us define an effecti!e stress, , which is a single

    numerical !alue that characteri1es the state of applied

    stress. If

    where cis a nown material property

    3ailure is not expected if

    The safety factoragainst failure is gi!en as4

    That is the applied stress can be increased by a factor of

    = before failure occurs.

    (#>

    occursfailurec =

    (#>

    failurenoc

    c

    X =

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    Maximum Normal Stress Criterion (Rankine

    5ielding #Plastic flow( taes place when the greatest

    principal stress in a complex state of stress reachestheflow stress in a uniaxial tension.

    Since '? 2? /, 3low occurs when

    "#tension( ) '

    +ompressi!e strength is usually greater than tensile

    strength.

    3low stress in uniaxial tension

    @aximum normal stress in a

    complex stress state.

    #%&A(

    ( ) ( )ncompressiotension "'"

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    Experiment to determine the yield stress of the shrimp

    #defined as the stress at which the amplitude of the tail

    wiggling would ha!e becomes less than a critical !alue(

    when crushed between two fingers showed that it occurredat a stress of about '"&CD*m&2#'A.C psi(.

    -ence,

    7anines criterion predicts that shrimp failure would occur at

    This corresponds to a depth of only '"m. 3ortunately for all

    lo!ers of crustaceans, this is not the case, and hydrostatic

    stresses do not contribute to plastic flow.

    2C

    " *'" mN=

    2C" *'" mNp =

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    Maximum!Shear!Stress or Tresca Criterion

    This yield criterion assumes that yielding occurswhen

    the maximum shear stress in a complex state of stresse8uals the maximum shear stress at the onset of flow in

    uniaxial&tension.

    3rom E8,#2.2'(, the maximum shear stress is gi!en by4

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    3or uniaxial tension, , and the maximum

    shearing yield stress is gi!en by4

    Substituting in E8. #%./(, we ha!e

    Therefore, the maximum&shear&stress criterion is gi!en by4

    "/2,"' === "

    2"

    "

    =

    22"

    "/'

    max

    ==

    =

    "/' = #%.G(

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    This criterion corresponds to taing the differences

    between '

    and /

    and maing it e8ual to the flow stressin uniaxial tension.

    This criterion does not predict failure under hydrostatic

    stress, because we would ha!e ') /) p and no

    resulting shear stress.

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    von Mises" or #istortion!$nergy Criterion

    This criterion is usually applied to ductile material !on @ises proposed that yielding would occur when the

    second in!ariant of the stress de!iator H2exceeds some

    critical !alue.

    where

    for yielding in uniaxial tension

    22 kJ =( ) ( ) ( )[ ]2'/

    2

    2'

    2

    /22G

    ' ++=J

    "B /2"' ===

    22"

    2" Gk=+

    #%.F(

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    Substituting E8. %&% into %&F, we obtain the usual form of

    !on @ises yield criterion.

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    %dditional &ailure Criteria

    ctahedral Shear Stress 5ield +riteria4 This is another

    yield criteria often used for ductile metals. It states thatyielding occurs when the shear stress on the octahedral

    planes reaches a critical !alue.

    @ohr&+oulomb 3ailure +riterion4 This is used for

    brittle metals, and is a modified Tresca criterion.

    Jriffith 3ailure +riterion4 $nother criterion used forbrittle metals. It simply states that failure will occur

    when the tensile stress tangential to an ellipsoidal ca!ity

    and at the ca!ity surface reaches a critical le!el ".

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    @c+lintoc&

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    $xample

    $ region on the surface of a G"G'&TA aluminum alloy

    component has strain gage attached, which indicate thefollowing stresses4

    '' ) F" @Pa

    22 ) '2" @Pa

    '2 ) G" @Pa

    0etermine the yielding for both Trescas and !on @ises

    criteria, gi!en that " ) 'C" @Pa #the yield stress(.

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    Solution

    Since we were gi!en the !alue of '2, we must therefore

    first establish the principal stresses. In!oe E8. A&/F.

    -ence,

    ' ) 'G" @PaB 2 ) /" @PaB ' ) "

    $ccording to Tresca, max ) #'G" & "(*2 ) %" @Pa

    3or yielding in uniaxial tension4

    "*2 ) FC @Pa

    Since the %" @Pa ? FC @Pa, Tresca criterion would be

    unsafe.

    +

    += 2'2

    222''22''

    2'22

    ,

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    The !on @ises criterion can be in!oed from E8. %&.

    The :.-.S. of the abo!e E8. gi!es a !alue of 'FC @Pa.

    This criterion predicts that the material will not fail #flow(,unlie the Tresca criterion, which predicts that the material

    will flow.

    Therefore, the Tresca criterion is more conser!ati!e than

    the !on @ises criterion in predicting failure.

    [ ] 2*'2'/

    2

    /2

    2

    2' (#(#(#

    2

    '

    ++=o