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Flaw growth of 7075, 7475, 7050 and 7049 aluminum alloy plate in stress corrosion environmentsMarine atmosphere and laboratory stress corrosion test results on smooth and precracked specimens from 7075, 7475, 7050, and 7049 alloy plates (1.25 and 3.0-in. thick) are presented. It is shown that for a given strength level, alloys 7050-T7X and 7049-T7X have superior short-transverse stress corrosion resistance (SCR) to 7X75-T7X. At typical strength levels above the minimum, for example, SCR of these alloys is considerably better than that of 7075-T76, and approaches that of 7075-T73. Alloy 7475 maintains an advantage in the area of fracture toughness, however, because it can be thermally processed to give particularly clean microstructures. Results from precracked specimens are in good qualitative agreement with those obtained from smooth specimens. Although both specimen types are capable of distinguishing between -T6, -T76 and -T73 tempers in relatively short time periods the precracked specimen provides more information about crack growth rates.
Document ID
19770019328
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dorward, R. C.
(Kaiser Aluminum and Chemical Corp. Pleasanton, CA, United States)
Hasse, K. R.
(Kaiser Aluminum and Chemical Corp. Pleasanton, CA, United States)
Date Acquired
September 3, 2013
Publication Date
October 15, 1976
Subject Category
Metallic Materials
Report/Patent Number
CFT-RR-76-32
NASA-CR-150313
Report Number: CFT-RR-76-32
Report Number: NASA-CR-150313
Accession Number
77N26272
Funding Number(s)
CONTRACT_GRANT: NAS8-30890
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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