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Combined effects of weld-induced residual stresses and flaws on the fracture strength of Ti-5Al-2.5SnThe combined effects of weld-induced residual stresses and flaws on fracture strength were experimentally evaluated by testing Ti-5Al-2.5Sn surface flawed specimens at -320F (-195C) in liquid nitrogen. Flaws were located in weld metal with crack planes either parallel to or perpendicular to gas tungsten arc weld centerlines, and in base metal with the crack plane perpendicular to the rolling direction. Tests were conducted using two different flaw sizes to effect fracture stresses at two different levels including one level either at or near, and one level well below the tensile yield strength. Three different residual stress levels were generated, measured, and tested. Results were evaluated using modified linear elastic fracture mechanics theory.
Document ID
19740061593
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hall, L. R.
(Boeing Aerospace Co. Seattle, Wash., United States)
Date Acquired
August 7, 2013
Publication Date
October 1, 1973
Subject Category
Materials, Metallic
Meeting Information
Meeting: Meeting on Significance of Defects in Welded Structures
Location: Tokyo
Country: Japan
Start Date: October 15, 1973
End Date: October 19, 1973
Accession Number
74A44343
Funding Number(s)
CONTRACT_GRANT: NAS3-12016
Distribution Limits
Public
Copyright
Other

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