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Preloading To Accelerate Slow-Crack-Growth TestingAn accelerated-testing methodology has been developed for measuring the slow-crack-growth (SCG) behavior of brittle materials. Like the prior methodology, the accelerated-testing methodology involves dynamic fatigue ( constant stress-rate) testing, in which a load or a displacement is applied to a specimen at a constant rate. SCG parameters or life prediction parameters needed for designing components made of the same material as that of the specimen are calculated from the relationship between (1) the strength of the material as measured in the test and (2) the applied stress rate used in the test. Despite its simplicity and convenience, dynamic fatigue testing as practiced heretofore has one major drawback: it is extremely time-consuming, especially at low stress rates. The present accelerated methodology reduces the time needed to test a specimen at a given rate of applied load, stress, or displacement. Instead of starting the test from zero applied load or displacement as in the prior methodology, one preloads the specimen and increases the applied load at the specified rate (see Figure 1). One might expect the preload to alter the results of the test and indeed it does, but fortunately, it is possible to account for the effect of the preload in interpreting the results. The accounting is done by calculating the normalized strength (defined as the strength in the presence of preload the strength in the absence of preload) as a function of (1) the preloading factor (defined as the preload stress the strength in the absence of preload) and (2) a SCG parameter, denoted n, that is used in a power-law crack-speed formulation. Figure 2 presents numerical results from this theoretical calculation.
Document ID
20110016575
Acquisition Source
Glenn Research Center
Document Type
Other - NASA Tech Brief
Authors
Gyekenyesi, John P.
(NASA Glenn Research Center Cleveland, OH, United States)
Choi, Sung R.
(Cleveland State Univ. Cleveland, OH, United States)
Pawlik, Ralph J.
(Ohio Aerospace Inst. Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2004
Publication Information
Publication: NASA Tech Briefs, January 2004
Subject Category
Man/System Technology And Life Support
Report/Patent Number
LEW-17409-1
Distribution Limits
Public
Copyright
Public Use Permitted.
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