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Thermal stress-relief treatments for 2219 aluminum alloy are evaluatedEvaluation of three thermal stress relief treatments for 2219 aluminum alloy in terms of their effect on residual stress, mechanical properties, and stress corrosion resistance. The treatments are post aging and stress relieving fullscale and subscale parts formed in the aged T81 condition, and aging subscale parts formed in the unaged T31 condition.
Document ID
19660000447
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Date Acquired
August 3, 2013
Publication Date
October 1, 1966
Subject Category
Materials
Report/Patent Number
MFS-1213
Report Number: MFS-1213
Accession Number
66B10448
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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