3. Fatigue failure

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Last updated 9:17 PM on 2/1/26
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18 Terms

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Definition of fatigue failure

Failure of material under cyclical load (load that varies over time)

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Stress level fatigue occur

can occur below yield stress

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Dangers of fatigue stress

  • no warning →no deformation, necking

  • sudden, catastrophic fracture

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4 Methods where crack appear

  • manufacturing defects

  • fatigue processes

  • corrosion

  • creep

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Types of fatigue failure (in terms of cycle and presence of cracks)

Cycle:

  1. Low cycle fatigue

  • low no. of cycle

  • occur above σy

  1. High cycle fatigue

  • million cycles to fail

  • occur below σy

Crack:
1. Crack-free

  1. Pre-existing cracks - non destructive testing method used to spot cracks)

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<p>High cycle load cyclic stress-no. of cycle relationship (Stress-number (SN) curve)</p>

High cycle load cyclic stress-no. of cycle relationship (Stress-number (SN) curve)

for crack-free specimen

  • for any cyclic load, follow SN curve of σm (mean stress)

<p>for crack-free specimen</p><ul><li><p>for any cyclic load, follow SN curve of σ<sub>m</sub> (mean stress)</p></li></ul><p></p>
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Benefit for SN curve

  • material comparison

  • early design estimate

  • high cycle fatigue regime

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Limitations of SN curve

  • remaining life of cracked component

  • crack growth behaviour

  • high scatter in experiemental data

  • long test required

  • most of lifetime used to initate defect

  • IGNORES CRACK SIZE

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Method to solve limitation of SN curve

find one curve for certain stress value

shift curve up and down for different stress

estimate but useful

<p>find one curve for certain stress value</p><p>shift curve up and down for different stress</p><p>estimate but useful</p>
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**

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Calculation of fatigue life (by number of cycle)

Ni: crack initiation

Np: crack propagation

  • depends on crack size & stress intensity range

<p>N<sub>i</sub>: crack initiation</p><p></p><p>N<sub>p</sub>: crack propagation</p><ul><li><p>depends on crack size &amp; stress intensity range</p></li></ul><p></p><p></p>
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Definition of Paris Law

rate of fatigue crack growth

relate crack growth to range of stress intensity factor

occur AFTER crack propagation

<p>rate of fatigue crack growth</p><p>relate crack growth to range of stress intensity factor</p><p>occur AFTER crack propagation</p>
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Methods to form defect(crack initiation) (Low vs high cycle)

Low:

  • plasticity causes slip steps on surface

  • act as stress concetrator to start fatigue

High:

  • no gross plasticity but homogeneties in atomic level raise local stress and initiate fatigue

<p>Low:</p><ul><li><p>plasticity causes slip steps on surface</p></li><li><p>act as stress concetrator to start fatigue</p></li></ul><p>High:</p><ul><li><p>no gross plasticity but homogeneties in atomic level raise local stress and initiate fatigue</p></li></ul><p></p>
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Design method to reduce fatigue

  • reduce section stress (raise cross-section)

  • remove stress concentrators(add fillers, welding)

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Environmental method to cope with fatigue

  • consider corrosion-fatigue relationship

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Surface treatment to cope with fatigue

  • locally harden surface as crack usually initates there

  • case hardening, work hardening, shot peening (locally inducing elastic compressive stresses)

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3 ways material is used to cope with fatigue

  • remove porosity ( at source or via hot working)

  • employ 2 phases (to deflect crack path)

  • employ composites(blunt crack as it propagates)

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Maintenance method to cope with fatigue

  • employ non-destructive method(NDE) to detect cracking

  • repair, remove replace or review