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Fatique crack growth behavior of a single crystal alloy as observed through an in situ fatigue loading stageAn in situ fatigue loading stage inside a scanning electron microscope (SEM) was used to determine the fatigue crack growth behavior of a PWA 1480 single-crystal nickel-based superalloy. The loading stage permits real-time viewing of the fatigue damage processes at high magnification. The PWA 1480 single-crystal, single-edge notch specimens were tested with the load axis parallel to the (100) orientation. Two distinct fatigue failure mechanisms were identified. The crack growth rate differed substantially when the failure occurred on a single slip system in comparison to multislip system failure. Two processes by which crack branching is produced were identified and are discussed. Also discussed are the observed crack closure mechanisms.
Document ID
19880013602
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Telesman, Jack
(NASA Lewis Research Center Cleveland, OH, United States)
Kantzos, Peter
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Metallic Materials
Report/Patent Number
NAS 1.15:100863
E-4080
NASA-TM-100863
Report Number: NAS 1.15:100863
Report Number: E-4080
Report Number: NASA-TM-100863
Accession Number
88N22986
Funding Number(s)
PROJECT: RTOP 505-63-1B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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