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Aluminum U-groove weld enhancement based on experimental stress analysesThough butt-welds are among the most preferred joining methods in aerostructures because of their sealing and assembly integrity and general elastic performance; their inelastic mechanics are generally the least understood. This study investigated experimental strain distributions across a thick aluminum U-grooved weld and identified two weld process considerations for improving the multipass weld strength. The extreme thermal expansion and contraction gradient of the fusion heat input across the tab thickness between the grooves produce severe peaking, which induces bending moment under uniaxial loading. The filler strain hardening decreased with increasing filler pass sequence. These combined effects reduce the weld strength, and a depeaking index model was developed to select filler pass thicknesses, pass numbers, and sequences to improve the welding process results over the current normal weld schedule.
Document ID
19960000864
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Verderaime, V.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Vaughan, R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Launch Vehicles And Space Vehicles
Report/Patent Number
NAS 1.60:3581
M-789
NASA-TP-3581
Accession Number
96N10864
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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