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    Chapter 9 : Failure

    This presentation includes figures and images from Callister text and instructor materials.

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    Brittle fracture surface

    transgranular intergranular

    160mm 4 mm

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    Intergranular

    (betweengrains)

    Intragranular

    (within grains)316 S. Steel

    (metal)Reprinted w/

    permission from

    "Metals Handbook",9th ed, Fig. 650, p.

    357. Copyright 1985,ASM International,

    Materials Park, OH.(Micrograph by D.R.

    Diercks, ArgonneNational Lab.)

    304 S. Steel

    (metal)Reprinted w/permission

    from "Metals Handbook",9th ed, Fig. 633, p. 650.

    Copyright 1985, ASMInternational, Materials

    Park, OH. (Micrograph byJ.R. Keiser and A.R. Olsen,

    Oak Ridge National Lab.)

    4 mm 160mm

    BRITTLE FRACTURE

    Initiation point

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    Evolution to failure:

    neckingvoidnucleation

    void growth

    and linkageshearingat surface fracture

    Resulting

    fracture

    surfaces(steel)

    50 mm

    particles

    serve as void

    nucleation

    sites.

    50 mm

    100 mm

    From V.J. Colangelo and F.A. Heiser,Analysis of Metallurgical Failures(2nd

    ed.), Fig. 11.28, p. 294, John Wiley andSons, Inc., 1987. (Orig. source: P.

    Thornton, J. Mater. Sci., Vol. 6, 1971,pp. 347-56.)

    Fracture surface of tire cord wire

    loaded in tension. Courtesy of F.Roehrig, CC Technologies, Dublin, OH.

    Used with permission.

    MODERATELY DUCTILE FAILURE

    Cup and cone ductile fracture

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    Ductile Fracture surface

    From center of specimen From shear edge of specimen

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    Fracture Modevariation in load

    direction

    Mode I

    Tension

    Mode II

    sliding

    Mode III

    Tearing

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    Stress conc. factor:

    Large Ktpromotes failure:

    FLAWS ARE STRESS CONCENTRATORS

    Stress distributionin front of a hole:

    Kt = 2(a/t)1/2

    2/1

    02

    t

    m

    a

    OR

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    Stress intensity factor and Fracture toughness

    -Stress intensity near crack isdistributed throughout the

    volume, decreasing further away.

    - The stress intensity depends on

    stress applied and flaw location

    andsize.

    -For the given geometry

    aYK

    Compare to stress

    concentration factor:

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    Stress intensity factor - Fracture toughness

    Note axes orientation: stress applied in y-direction

    Plane-stress: Very thin (plate)sample, (stress developed in z

    direction is small compared to

    that in y and x)

    Plane-strain: Thick plate, (strain

    developed in z direction is small

    compared to that in y and x)

    Stress does develop in z direction.

    - most constrained configuration.

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    Fracture toughness

    aYK aYK

    cc

    Critical applied stress

    for fracture

    aYK cIc

    Plane strain conditionsmost constrained,so brittle fracture occurs at lower stress for

    same crack length.

    Material property, just like yield strength or

    elastic modulus, for crack opening mode, plane

    strain, for this geometry

    FromMechanical Metallurgy, Dieter

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    Crack growth condition:

    Y a

    Largest, moststressed cracks grow first!

    --Result 1: Max flaw size

    dictates design stress.

    --Result 2: Design stress

    dictates max. flaw size.

    design Kc

    Y amax

    amax 1

    Kc

    Ydesign

    2

    K Kc

    DESIGN AGAINST CRACK GROWTH

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    Increasing temperature...

    --increases %EL and Kc

    Ductile-to-brittle transition temperature (DBTT)...

    Impact test/temperature effect

    DBTT

    initial heightfinal height

    sample

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    Crazing in polystyrene

    Crazeoccurs in polymers

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    Slip bands withingrains formed by

    fatigue

    Surface notches

    formed by fatigue

    Images from Schaffer, 1999