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Evaluation of Stress Corrosion Cracking Susceptibility Using Fracture Mechanics Techniques, Part 1Stress corrosion cracking (SSC) tests were performed on 13 aluminum alloys, 13 precipitation hardening stainless steels, and two titanium 6Al-4V alloy forgings to compare fracture mechanics techniques with the conventional smooth specimen procedures. Commercially fabricated plate and rolled or forged bars 2 to 2.5-in. thick were tested. Exposures were conducted outdoors in a seacoast atmosphere and in an inland industrial atmosphere to relate the accelerated tests with service type environments. With the fracture mechanics technique tests were made chiefly on bolt loaded fatigue precracked compact tension specimens of the type used for plane-strain fracture toughness tests. Additional tests of the aluminum alloy were performed on ring loaded compact tension specimens and on bolt loaded double cantilever beams. For the smooth specimen procedure 0.125-in. dia. tensile specimens were loaded axially in constant deformation type frames. For both aluminum and steel alloys comparative SCC growth rates obtained from tests of precracked specimens provide an additional useful characterization of the SCC behavior of an alloy.
Document ID
19740002722
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sprowls, D. O.
(Aluminum Co. of America Pittsburgh, PA, United States)
Shumaker, M. B.
(Aluminum Co. of America Pittsburgh, PA, United States)
Walsh, J. D.
(Aluminum Co. of America Pittsburgh, PA, United States)
Coursen, J. W.
(Aluminum Co. of America Pittsburgh, PA, United States)
Date Acquired
September 3, 2013
Publication Date
May 31, 1973
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-124469
Report Number: NASA-CR-124469
Accession Number
74N10835
Funding Number(s)
CONTRACT_GRANT: NAS8-21487
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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