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Elevated temperature fracture of RS/PM aluminum alloy 8009The fracture behavior of advanced powder metallurgy Al-Fe-V-Si alloy 8009 (previously called FVS0812) is being characterized under monotonic loads, as a function of temperature. Particular attention is focused on contributions to the fracture mechanism from the fine grained dispersoid strengthened microstructure, dissolved solute from rapid solidification, and the moist air environment. Time-dependent crack growth is characterized in advanced aluminum alloys at elevated temperatures with the fracture mechanics approach, and cracking mechanisms are examined with a metallurgical approach. Specific tasks were to obtain standard load crack growth experimental information from a refined testing system; to correlate crack growth kinetics with the j-integral and time dependent C(sub t)(t); and to investigate the intermediate temperature embrittlement of 8009 alloy in order to understand crack growth mechanisms.
Document ID
19910017973
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Porr, William C., Jr.
(Virginia Univ. Charlottesville, VA, United States)
Yang, Leng
(Virginia Univ. Charlottesville, VA, United States)
Gangloff, Richard P.
(Virginia Univ. Charlottesville, VA, United States)
Date Acquired
September 6, 2013
Publication Date
June 30, 1991
Publication Information
Publication: NASA-UVA Light Aerospace Alloy and Structures Technology Program (LA2ST)
Subject Category
Metallic Materials
Accession Number
91N27287
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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