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In-phase thermomechanical fatigue mechanisms in an unidirectional SCS-6/Ti 15-3 MMCThe objective of this investigation was to identify the inelastic deformation and damage mechanisms under in-phase (IP) thermomechanical fatigue (TMF) in a unidirectional SCS-6/Ti 15-3 metal matrix composite (MMC). Load-controlled IP TMF tests were conducted at 300-538 C at various stress ranges in high-purity argon. A major emphasis of this work was to identify damage mechanism well before final fracture of specimens, rather than to generate life diagrams, to aid development of a realistic deformation/damage and life model.
Document ID
19950022712
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Newaz, Golam M.
(Battelle Memorial Inst. Columbus, OH, United States)
Majumdar, Bhaskar S.
(Universal Energy Systems, Inc., Dayton OH., United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1995
Publication Information
Publisher: NASA
Subject Category
Composite Materials
Report/Patent Number
NASA-CR-195482
NAS 1.26:195482
E-9716
Report Number: NASA-CR-195482
Report Number: NAS 1.26:195482
Report Number: E-9716
Accession Number
95N29133
Funding Number(s)
CONTRACT_GRANT: NAS3-26822
PROJECT: RTOP 505-63-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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