Introduction to Aircraft Structural Analysis (Elsevier Aerospace Engineering)

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348 CHAPTER 10 Materials


Fig.10.20


Alternating stress in fatigue loading.


Fig.10.21


Stress–endurance curves.


Inmanypracticalsituations,theamplitudeofthealternatingstressvariesandisfrequentlyrandom
innature.TheS–ncurvedoesnot,therefore,applydirectlyandanalternativemeansofpredictingfailure
isrequired.Miner’scumulativedamagetheorysuggeststhatfailureoccurswhen


n 1
N 1

+

n 2
N 2

+···+

nr
Nr

= 1 (10.1)

wheren 1 ,n 2 ,...,nrare the number of applications of stressesσalt,σmean,andN 1 ,N 2 ,...,Nrare the
numberofcyclestofailureofstressesσalt,σmean.
WeshallexaminefatigueanditseffectonaircraftdesigninmuchgreaterdetailinChapter14.

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