caef 7 strain life

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    Explaining the differences from Stress-Life Fatigue

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    The Strain-Life Method

    (Local Strain, -N, or Crack Initiation)

    *Relates local strain to fatigue damage at that point

    *Useful when cycles have some plastic strain component

    *Suitable for predicting life in components which aresupposed to be defect free, i.e., not structural joints,sharp features, etc.

    (Low Cycle Fatigue LCF)

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    MSC Fatigue Features

    *Based on Local Strain Concepts

    *

    Mean Stress Correction*Elastic-Plastic Conversion

    *Statistical Confidence Parameters

    *Palmgren-Miner Linear Damage

    *

    User Defined Life

    *Cyclic Stress-Strain Modeling

    *Surface Conditions

    *Factor of Safety Analysis

    *Biaxiality Indicators

    *Multiple Loads

    Strain-Life (-N)

    1/2cycle

    1cycle

    1/2cycle

    1cycle

    1cycle

    1/2cycle

    Strain

    Time

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    Cyclic Testing - Hysteresis Loops and End Point Definition

    2Nf

    StabilizedHysteresis Loop

    Stress

    Strain

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    -NFatigue Tests*Specimens are subjected to constant

    amplitude strain using an

    extensometer in the servo loop

    *

    N test controls plastic strain, theparameter that governs fatigue

    *The number of cycles to crack

    initiation is plotted against the total

    strain on a log-log plot and the best fitcurve computed

    ( ) ( )cff

    b

    f

    f

    a NNE

    22`

    `+=

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    Elastic & Plastic Components(Due to Basquin, Coffin and Manson)

    (2Nf)b + f

    (2Nf)c

    f

    E

    2=

    Elastic

    (Basquin)

    Plastic

    (Coffin-Manson)

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    Neubers Rule

    The strain concentration factor,

    and the stress concentration factor,

    after plastic yielding.

    Neither are known but Neuber suggested that the square root of theproduct of the stress and strain concentration factors was equal to

    Kt . Hence Neubers Rule is simply:

    Re-arrangement of this Rule gives a useful equation:

    eK

    e

    =

    SK

    =

    ( )2.Te

    KKK =

    ( ) =SeKT

    2

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    Another re-arrangement gives:

    in which the LHS is known. This can be solved with the cyclic stress

    strain curve equation simultaneously to derive and

    Topper simply replaced Ktby Kf to make Neubers Rule applicable infatigue analysis for local stress strain tracking.

    Use of Kfin Neubers Rule

    ( ) =EeKT

    2

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    1

    2

    3

    Kf

    e

    s

    Cyclic Stress Strain Curve

    Neuber

    Equation

    Solution

    point

    Graphical Solution for Local and

    1

    K

    3yclic Stres

    Solution

    2

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    Morrow Life Plot

    StrainAmplitude(M/M)

    Life (Reversals)nCode nSoft

    STW Life Plot

    STWP

    arameter(MPa)

    Life (Reversals)nCode nSoft

    Morrow Smith-Topper-Watson

    ( ) ( )

    2

    2 2=

    +f mf

    bf f

    c'' ( ) ( )

    c+bfff

    2bf

    2f

    max 2''2'

    2

    +

    =

    Correcting for Mean Stress