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A comparison of single-cycle versus multiple-cycle proof testing strategiesAn evaluation of single-cycle and multiple-cycle proof testing (MCPT) strategies for SSME components is described. Data for initial sizes and shapes of actual SSME hardware defects are analyzed statistically. Closed-form estimates of the J-integral for surface flaws are derived with a modified reference stress method. The results of load- and displacement-controlled stable crack growth tests on thin IN-718 plates with deep surface flaws are summarized. A J-resistance curve for the surface-cracked configuration is developed and compared with data from thick compact tension specimens. The potential for further crack growth during large unload/reload cycles is discussed, highlighting conflicting data in the literature. A simple model for ductile crack growth during MCPT based on the J-resistance curve is used to study the potential effects of key variables. The projected changes in the crack size distribution during MCPT depend on the interactions between several key parameters, including the number of proof cycles, the nature of the resistance curve, the initial crack size distribution, the component boundary conditions (load vs. displacement control), and the magnitude of the applied load or displacement. The relative advantages of single-cycle and multiple-cycle proof testing appear to be specific, therefore, to individual component geometry, material, and loading.
Document ID
19900018799
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hudak, S. J., Jr.
(Southwest Research Inst. San Antonio, TX., United States)
Mcclung, R. C.
(Southwest Research Inst. San Antonio, TX., United States)
Bartlett, M. L.
(Southwest Research Inst. San Antonio, TX., United States)
Fitzgerald, J. H.
(Southwest Research Inst. San Antonio, TX., United States)
Russell, D. A.
(Rockwell International Corp. Canoga Park, CA., United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1990
Publication Information
Publisher: NASA
Subject Category
Structural Mechanics
Report/Patent Number
NASA-CR-4318
NAS 1.26:4318
Report Number: NASA-CR-4318
Report Number: NAS 1.26:4318
Accession Number
90N28115
Funding Number(s)
CONTRACT_GRANT: NAS8-37451
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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