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Corrosion Embrittlement of Duralumin I Practical Aspects of the ProblemSince aircraft design is tending toward all-metal construction, the strong heat-treatable light aluminum alloy, duralumin (a generic name for a class of heat-treatable alloys containing Cu, Mg, Mn, and Si), is finding increasing application. Doubt has been expressed concerning the reliability and permanence of these materials. Information is given on the effect of corrosion on the tensile properties of 14-gauge sheet duralumin, heat treated by quenching in hot water after being heated for 15 minutes in a fused nitrate bath at 500 to 510 C. Intercrystalline corrosion and practical aspects of intercrystalline embrittlement are discussed with respect to duralumin.
Document ID
19930081096
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Rawdon, Henry S
(Bureau of Standards)
Date Acquired
September 6, 2013
Publication Date
April 1, 1928
Report/Patent Number
NACA-TN-282
Report Number: NACA-TN-282
Accession Number
93R10386
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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