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Accommodating and cracking mechanisms in low-cycle fatigueThe three main stages of fatigue life (accommodation, crack initiation and crack growth) are briefly reviewed. The cyclic behavior of annealed or predeformed face-centered cubic metals is described. Moreover, two types of alloys (Al-4-Cu and WASPALOY) are examined regarding the influence of the interactions between the precipitates and the dislocations on the cyclic behavior. Data on the percent of life to crack initiation (for a microcrack smaller than about 100 microns) are also given. Finally, experimental and theoretical results on crack growth rates in lowcycle fatigue are described.
Document ID
19780018549
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Pineau, A.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1978
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-75227
Report Number: NASA-TM-75227
Accession Number
78N26492
Funding Number(s)
CONTRACT_GRANT: NASW-2791
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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