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Analyses of Fatigue Crack Growth and Closure Near Threshold Conditions for Large-Crack BehaviorA plasticity-induced crack-closure model was used to study fatigue crack growth and closure in thin 2024-T3 aluminum alloy under constant-R and constant-K(sub max) threshold testing procedures. Two methods of calculating crack-opening stresses were compared. One method was based on a contact-K analyses and the other on crack-opening-displacement (COD) analyses. These methods gave nearly identical results under constant-amplitude loading, but under threshold simulations the contact-K analyses gave lower opening stresses than the contact COD method. Crack-growth predictions tend to support the use of contact-K analyses. Crack-growth simulations showed that remote closure can cause a rapid rise in opening stresses in the near threshold regime for low-constraint and high applied stress levels. Under low applied stress levels and high constraint, a rise in opening stresses was not observed near threshold conditions. But crack-tip-opening displacement (CTOD) were of the order of measured oxide thicknesses in the 2024 alloy under constant-R simulations. In contrast, under constant-K(sub max) testing the CTOD near threshold conditions were an order-of-magnitude larger than measured oxide thicknesses. Residual-plastic deformations under both constant-R and constant-K(sub max) threshold simulations were several times larger than the expected oxide thicknesses. Thus, residual-plastic deformations, in addition to oxide and roughness, play an integral part in threshold development.
Document ID
19990041101
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Newman, J. C., Jr.
(NASA Langley Research Center Hampton,VA United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1999
Subject Category
Composite Materials
Report/Patent Number
L-17842
NAS 1.15:209133
NASA/TM-1999-209133
Report Number: L-17842
Report Number: NAS 1.15:209133
Report Number: NASA/TM-1999-209133
Meeting Information
Meeting: Fatigue Crack Growth Thresholds, Endurance Limits, and Design (ASTM STP-1372)
Location: Norfolk, VA
Country: United States
Start Date: November 4, 1998
End Date: November 5, 1998
Sponsors: American Society for Testing and Materials
Funding Number(s)
PROJECT: RTOP 522-18-11-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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