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Residual stresses in welded platesThe purpose of this project was to develop a simple model which could be used to study residual stress. The mechanism that results in residual stresses in the welding process starts with the deposition of molten weld metal which heats the immediately adjacent material. After solidification of weld material, normal thermal shrinkage is resisted by the adjacent, cooler material. When the thermal strain exceeds the elastic strain corresponding to the yield point stress, the stress level is limited by this value, which decreases with increasing temperature. Cooling then causes elastic unloading which is restrained by the adjoining material. Permanent plastic strain occurs, and tension is caused in the region immediately adjacent to the weld material. Compression arises in the metal farther from the weld in order to maintain overall static equilibrium. Subsequent repair welds may add to the level of residual stresses. The level of residual stress is related to the onset of fracture during welding. Thus, it is of great importance to be able to predict the level of residual stresses remaining after a weld procedure, and to determine the factors, such as weld speed, temperature, direction, and number of passes, which may affect the magnitude of remaining residual stress. It was hoped to use traditional analytical modeling techniques so that it would be easier to comprehend the effect of these variables on the resulting stress. This approach was chosen in place of finite element methods so as to facilitate the understanding of the physical processes. The accuracy of the results was checked with some existing experimental studies giving residual stress levels found from x-ray diffraction measurements.
Document ID
19950012557
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bernstein, Edward L.
(Alabama A & M Univ. Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1994
Publication Information
Publication: Alabama Univ., Research Reports: 1994 NASA(ASEE Summer Faculty Fellowship Program
Subject Category
Structural Mechanics
Accession Number
95N18972
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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