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Residual Stress Reversal in Highly Strained Shot Peened Structural ElementsThe purpose of this research was to further the understanding of a crack initiation problem in a highly strained pressure containment housing. Finite Element Analysis methods were used to model the behavior of shot peened materials undergoing plastic deformation. Analytical results are in agreement with laboratory tensile tests that simulated the actual housing load conditions. These results further validate the original investigation finding that the shot peened residual stress had reversed, changing from compressive to tensile, and demonstrate that analytical finite element methods can be used to predict this behavior.
Document ID
20020048530
Acquisition Source
Marshall Space Flight Center
Document Type
Thesis/Dissertation
Authors
Mitchell, William S.
(Pratt and Whitney Aircraft West Palm Beach, FL United States)
Throckmorton, David
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Structural Mechanics
Funding Number(s)
PROJECT: RTOP 376-20-20
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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